US20060124018A1 - Explosive-activated safe-arm device - Google Patents
Explosive-activated safe-arm device Download PDFInfo
- Publication number
- US20060124018A1 US20060124018A1 US10/525,916 US52591605A US2006124018A1 US 20060124018 A1 US20060124018 A1 US 20060124018A1 US 52591605 A US52591605 A US 52591605A US 2006124018 A1 US2006124018 A1 US 2006124018A1
- Authority
- US
- United States
- Prior art keywords
- signal
- housing
- barrier
- initiation
- fixture
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000002360 explosive Substances 0.000 title description 19
- 230000004888 barrier function Effects 0.000 claims abstract description 141
- 230000000977 initiatory effect Effects 0.000 claims abstract description 99
- 230000003111 delayed effect Effects 0.000 claims abstract description 86
- 230000004044 response Effects 0.000 claims description 15
- 230000001681 protective effect Effects 0.000 abstract 2
- 239000007789 gas Substances 0.000 description 82
- 241000283216 Phocidae Species 0.000 description 13
- 239000000463 material Substances 0.000 description 9
- 230000033001 locomotion Effects 0.000 description 6
- 238000009527 percussion Methods 0.000 description 6
- 230000007246 mechanism Effects 0.000 description 4
- 239000008188 pellet Substances 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- 230000006378 damage Effects 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 241000283139 Pusa sibirica Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000000586 desensitisation Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/34—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by a blocking-member in the pyrotechnic or explosive train between primer and main charge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/28—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
- F42C15/31—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids generated by the combustion of a pyrotechnic or explosive charge within the fuze
Definitions
- This invention relates to an explosive-activated safe-arm device for conveying non-electric initiation signals.
- the external initiation source comprises a signal transfer line that is connected to the device in a manner that permits the release of an explosive initiation signal from the signal line to the device.
- the signal line may comprise detonating cord, which inherently transmits an explosive output signal at all points along its length, but which is typically equipped with a coupling fixture to facilitate the connection of the signal line and the transfer of the explosive initiation signal to a target device.
- the signal line may comprise a signal tube, such as shock tube, having an end fixture coupled thereto, e.g., a detonator or pyrotechnic initiator, that is configured to generate a brisant output from the signal in the signal tube.
- a delay member typically comprise means for generating an explosive output signal at the end of the delay interval following the receipt of an initiation signal.
- the explosively initiated device or “target device” further comprises a direct-initiation fixture designed to receive the explosive output signal from the delay member and to function in response thereto, typically without delay.
- Some delay members are liable to initiation apart from receipt of the external explosive initiation signal, and may then cause unintended functioning of the target device. Avoidance of such unintentional functioning is generally recognized as an important design goal, especially when there is a high cost associated with the functioning of the target device (e.g., target devices such as warheads and rocket motors).
- the device is mounted within the explosive or propulsive charge in the projectile casing.
- the device includes a housing within which is disposed a delay powder train 31 with an associated output charge, detonator 29 .
- the output charge must initiate a booster charge 32 via explosive pellets 42 and 43 in order to initiate self destruction of the projectile.
- the intervening pellets 42 and 43 are mounted on rotatable plates which, when the projectile rotates as a result of being fired, move in response to the rotation by aligning the pellets.
- the output charge 29 will initiate the booster charge 32 by initiating, in sequence, the aligned intervening pellets 43 and 42 .
- the plates 17 are eccentrically-mounted rotors which are moved by centrifugal force when the projectile is in flight.
- U.S. Pat. No. 4,328,754 to Goodman, dated May 11, 1982 and entitled “Time Delay Device”, discloses a mechanism for the delayed release of a spring-driven firing pin.
- the operation of the release depends upon the movement of a release piston under the force of a spring.
- the action of the spring is resisted by a reservoir of gas which must be dissipated through a narrow aperture to permit the piston to move.
- the gas controls the speed of the piston and thus determines a delay interval between the activation of the delay device and the release of the firing pin.
- U.S. Pat. No. 4,660,473 to Bender et al, dated Apr. 28, 1987, entitled “Compressed Gas-Actuated Mechanical Power Element”, discloses a housing containing a pair of movable pistons that can be extended from the housing under the force of compressed gas introduced into the housing.
- U.S. Pat. No. 4,932,325 to Wilson, dated Jun. 12, 1990, entitled “Safety Device For An Aerodynamic Body Fuse”, discloses a device for an aerodynamic body, in which functional parts are mounted on a slide that can be moved from a safe position within the contour of the body to an armed position beyond the contour of the body.
- the slide defines two air passages that face in opposite directions, so that when the slide is disposed in a moving air stream, a different air pressure is created in each perforation.
- the perforations communicate with a piston chamber and the difference in pressure is employed to move a piston from a safe position to an armed position.
- U.S. Pat. No. 3,938,443 to Wolski discloses a mechanical logic module for a missile fuse device.
- the logic module makes use of the passage of air through a conduit to create a pressure differential to operate a piston.
- the piston rotates a cam which constitutes part of a safe-arm device.
- FIG. 4 A prior art safing mechanism employed on aerospace devices is illustrated schematically in FIG. 4 .
- an input fixture 116 and an output (receiving) fixture 114 are mounted for signal transfer from one to the other in a housing 112 .
- the housing 112 defines a piston chamber 112 b within which a barrier piston 124 resides.
- Barrier piston 124 includes a shield portion 124 a that can be disposed between fixture 116 and 114 to prevent signal transfer from one to the other.
- Barrier piston 124 is initially in an “armed” position, in which shield portion 124 a does not obstruct signal transfer from fixture 116 to fixture 114 .
- Safing device 110 includes a cap 113 that is configured to receive a safing fixture 111 .
- Each of fixtures 116 , 114 and 111 comprises a threaded stainless steel ferrule that can be secured to housing 112 or cap 113 , respectively, and which is secured to a signal transmission device (detonating cord) that terminates in an explosive-filled cup that protrudes through the ferrule into housing 112 .
- a signal transmission device detonating cord
- an input signal received on the signal line connected to input fixture 116 causes an initiation signal to be released into housing 112 to initiate a signal in the output fixture 114 .
- safing fixture 111 receive a safing signal, it will release gas into the top portion of chamber 112 b that will impel barrier piston 124 downward (as sensed in FIG.
- the signal that initiates safing fixture 111 may be generated in response to an external condition that would make the initiation of a signal in output fixture 114 undesirable.
- This invention provides a safe-arm device comprising a housing defining at least one inlet aperture, an outlet aperture, and a barrier chamber.
- a barrier member in the barrier chamber that is movable therein from a safe position to an armed position in response to impelling gas introduced into the housing.
- the delayed output component is responsive to an input signal, for generating a delayed initiation signal.
- the barrier member when in the safe position, is situated to inhibit initiation of an output device in the outlet aperture by the delayed output component and, when in the armed position, is situated to permit the delayed output component to initiate such output device.
- the barrier member when in the safe position, may be situated between the delayed output component and the outlet aperture.
- the device may be configured to admit impelling gas from an input device in the inlet aperture into the barrier chamber to move the barrier member.
- the device may comprise an impelling gas source that is responsive to a signal from an input device.
- the device may comprise a signal transfer device that comprises first and second signal transfer fixtures joined by a signal line.
- the first signal transfer fixture may be secured in the housing and configured for initiation by an input device in the inlet aperture and the second signal transfer fixture may comprise an arming fixture comprising the impelling gas source, and may be secured in the housing to release gas into the barrier chamber in response to a signal from the first signal transfer fixture.
- the first signal transfer fixture may comprise an arming fixture comprising the impelling gas source and may be secured in the housing to release gas into the barrier chamber in response to a signal from an input fixture, and the second signal transfer fixture may be secured in the housing and configured to initiate the delayed output component in response to a signal from the first signal transfer fixture.
- the device may be combined with an input device secured in each inlet aperture for initiating the delayed output component and introducing impelling gas into the housing, and with an output device secured in the outlet aperture for initiation by the delayed output component.
- the housing is preferably sealed against the escape of impelling gas.
- one input device may introduce the impelling gas and another may initiate the delayed output component.
- the barrier chamber may comprise a piston chamber portion and an output initiation portion.
- the barrier member may comprise a piston segment in the piston chamber portion, and a middle segment and a shield segment in the output initiation portion of the barrier chamber, wherein the middle segment of the barrier member is configured to substantially isolate the outlet aperture from impelling gas introduced into the piston chamber portion.
- FIG. 1 is a schematic cross-sectional view of a safe-arm device according to a first embodiment of the invention
- FIG. 2A is a schematic cross-sectional view of a safe-arm device according to a second embodiment of the invention.
- FIG. 2B is a view of a device similar to FIG. 2A except that it comprises two input devices, one of which is a gas-generating fixture which is independent of i.e., not responsive to, the other input fixture;
- FIG. 3A is a schematic cross-sectional view of a safe-arm device according to a third embodiment of the invention.
- FIG. 3B is a schematic cross-sectional view of a portion of the barrier member in a portion of the barrier chamber of the device of FIG. 3A ;
- FIG. 4 is a schematic cross-sectional view of a prior art safing device.
- the safe-arm device of this invention finds utility in various fields, including aerospace and military applications, for reliably transferring a non-electric initiation signal through a housing from an input device to an output device.
- the safe-arm device includes a delayed output component which generates an initiation signal for an output device coupled to the housing after a delay interval following the receipt of a signal from the input device (the input signal).
- a movable barrier member in the housing that is initially positioned to inhibit the transfer of a delayed initiation signal from the delayed output component to an output device, i.e., it is initially in a “safe” position between the delayed output component and the output device.
- the barrier member is movable to a non-inhibiting position, i.e., to an “armed” position, in which it permits the delayed output component to initiate the output device.
- the delayed output component may function solely to postpone the initiation of the output device for an interval sufficient to permit movement of the barrier member, or it may serve additional functions (such as the initiation of other devices) during the delay interval as well.
- the safe-arm device may include a retainer (e.g., a shear pin) for releasably retaining the barrier in the safe position until the receipt of the input signal, and may also include a locking mechanism (e.g., locking tabs and grooves) to keep the barrier in the armed position thereafter.
- a retainer e.g., a shear pin
- a locking mechanism e.g., locking tabs and grooves
- the barrier member is movable in response to the introduction of impelling gas into the housing when the input signal is received.
- the housing defines a barrier chamber in which a piston portion of the barrier member resides. A pressure difference from one side of the piston portion to the other will cause the barrier member to move.
- the impelling gas which may be highly energetic (i.e., hot and highly pressurized)
- the housing and barrier member are configured so that the output device is substantially isolated from the impelling gas.
- the barrier member will prevent the delayed output component from initiating the output device by blocking the debris, heat and shock of the delayed initiation signal from the output device. Gas produced by the delayed output component may also move the barrier from the safe position, but such movement would occur after the delayed initiation signal has been blocked from the output device.
- the impelling gas is obtained at least in part from an input device that has been secured to the housing.
- the input device comprises a gas-generating fixture which introduces impelling gas into the housing, and the housing is configured so that the impelling gas can flow into an impelling region in the barrier chamber from the input device.
- the safe-arm device of this invention comprises a gas-generating fixture that is distinct from, but responsive to, the input device, and the input device need not contribute impelling gas.
- the impelling gas is provided by the input device together with gas from a gas-generating fixture responsive to it.
- the distinct gas-generating fixture may constitute an input device that is distinct from the input device that initiates the delayed output component.
- all devices mounted in the housing e.g., the at least one input device, output device and the optional signal transfer device and gas-generating fixture, etc., form a seal with the housing so that the impelling gas is not subject to loss in pressure due to leakage from the housing, and to prevent the introduction of gas into the housing from the environment.
- the maximum efficacy of impelling gas introduced into the device will be obtained and the need for an external power source for moving the barrier member can be avoided, i.e., the device can be self-contained.
- Safe-arm device 10 comprises a housing 12 which includes a fixture seat 13 a.
- Fixture seat 13 a defines an inlet aperture 13 b which includes an expansion chamber 13 a
- Housing 12 encloses a delayed output component 17 in a component chamber 12 a.
- An input device 16 is secured in inlet aperture 13 b and an output device 14 is secured in outlet aperture 12 g and housing 12 is otherwise sealed such that gas cannot enter or escape housing 12 .
- the input device 16 is capable of emitting a signal that can initiate the delayed output component 17 . It also introduces impelling gas into the housing to move the barrier member 24 , as described below.
- input device 16 comprises an input fixture 16 a secured to a signal line 18 such as detonating cord.
- Input device 16 may optionally comprise an FCDCA (flexible confined detonating cord assembly), a type of signal-transfer apparatus well known in the art.
- FCDCA flexible confined detonating cord assembly
- the end tip of an FCDCA When initiated, the end tip of an FCDCA generates a brisant output signal and a flyer plate derived from the cup.
- FCDCA flexible confined detonating cord assembly
- input fixture 16 a is a signal transfer fixture comprising a longitudinal bore therethrough where a signal transfer line comprising a flexible, confined detonating cord (e.g., a length of 2.7 grains per foot HNS-IIA Aluminum Mild detonating fuse, surrounded by flexible shielding (which my included braided stainless steel with moisture barrier therein)) is received.
- a signal transfer line comprising a flexible, confined detonating cord (e.g., a length of 2.7 grains per foot HNS-IIA Aluminum Mild detonating fuse, surrounded by flexible shielding (which my included braided stainless steel with moisture barrier therein)) is received.
- An end tip 16 b comprising a transfer charge of reactive (i.e., pyrotechnic or explosive) material such as HNS disposed in a cup is secured on the end of the signal transfer line and protrudes from the fixture 16 a
- Input fixture 16 a is configured so that it can easily be secured to the housing (e.g., it may have screw threads that mate with threads in the housing) with end tip 16 b in position for signal transfer with another device (e.g., for initiation of a delay device or signal transfer device).
- Delayed output component 17 includes a delay member 20 and a ferrule 26 which carries a percussion cap 28 .
- Delay member 20 comprises a sleeve 20 b filled with a pyrotechnic delay material 20 d.
- Sleeve 20 b carries an annular flange 20 a disposed concentrically about delay member 20 .
- the input end of sleeve 20 b is disposed within ferrule 26 , which is secured to flange 20 a.
- Ferrule 26 defines an expansion chamber around delay member 20 to permit the expansion of gas generated by delay material 20 d.
- Ferrule 26 carries percussion cap 28 at a position where the cap 28 can be initiated by an input device secured in the inlet aperture of the housing, and where, upon initiation, cap 28 will initiate the delay material 20 d from across a short spacing gap.
- a seal 27 on the end of ferrule 26 covers over percussion cap 28 to protect the cap against desensitization by environmental factors, e.g., moisture. Seal 27 is sufficiently thin and input device 16 is sufficiently powerful that seal 27 does not prevent input device 16 from initiating cap 28 .
- Ferrule 26 is configured so that it leaves an annular gas-flow passage about its exterior, between itself and the interior surface of component chamber 12 a, for reasons discussed below.
- delayed initiation charge 22 which contains a charge of reactive material, e.g., an explosive material such as HNS, in a cup and which is sensitive to initiation by pyrotechnic delay material 20 d.
- delayed initiation charge 22 has access to barrier chamber 12 b from component chamber 12 a via an initiation aperture (unnumbered) in the housing.
- delayed initiation charge 22 releases a delayed initiation signal that may include a flyer and that is sufficiently energetic to initiate an output device.
- Housing 12 defines a barrier chamber 12 b within which barrier member 24 resides.
- barrier chamber 12 b One portion of barrier chamber 12 b, which is closed by barrier plug 12 c, is referred to herein as a piston chamber 12 d, and another portion of barrier chamber 12 b is an output transfer portion 12 e.
- a piston segment 24 b of barrier member 24 is configured to closely match the walls of piston chamber 12 d and a middle segment 24 c of barrier member 24 is configured for a substantially sealing fit within output transfer portion 12 e.
- Barrier chamber 12 b and barrier member 24 are configured to prevent barrier member 24 from rotating within chamber 12 b, e.g., they may comprise a groove and slot engagement between them.
- High-pressure impelling gas can be introduced into piston chamber 12 d at a point below piston segment 24 b (as sensed in FIG. 1 ) (referred to herein as the impelling region 12 h ), where the impelling gas is blocked from direct entry into output transfer portion 12 e by middle segment 24 c of barrier member 24 .
- the high pressure in the impelling region 12 h will cause barrier member 24 to move as indicated by the upward-pointing arrow in FIG. 1 .
- a longitudinal pressure relief aperture 24 e extends from the top of the piston segment 24 b of barrier member 24 to the bottom of the shield segment 24 d. At least some of the non-impelling gas in the upper portion of barrier chamber 12 b (as sensed in FIG. 1 ) that would otherwise be compressed by the motion of barrier member 24 to its armed position may therefore be displaced into the output transfer portion 12 e of barrier chamber 12 b. Thus, resistance against the movement of barrier member 24 to the armed position due to the compression of non-impelling gas in the housing is significantly reduced. Nevertheless, middle segment 24 c of barrier member 24 substantially establishes a seal with barrier chamber 12 b to prevent the entry of impelling gas from the piston chamber 12 d into output transfer portion 12 e.
- barrier member 24 is configured to isolate the outlet aperture, and an output device mounted therein, from impelling gas.
- the seals established by piston segment 24 b and middle segment 24 c may be facilitated by the use of ring seals, as shown in device 10 ′′, FIG. 3A .
- Delayed initiation charge 22 of delayed output component 17 is positioned so that when initiated, it releases a signal, optionally including a flyer, into output transfer portion 12 e, for initiating an output device.
- Barrier member 24 includes a shield segment 24 d extending from middle segment 24 c. Shield segment 24 d is configured to be interposed between the delayed initiation charge 22 and an output device when barrier member 24 is in the safe position.
- the shield segment 24 d may be designed to simulate a fixed, simply-supported beam, rather than a fixed-free beam.
- barrier member 24 may be held in the safe position by retaining means such as a shear pin in a double-shear configuration (not shown), designed to prevent barrier 24 from moving in chamber 12 b in response to non-initiating stimuli, such as vibrations, but which permits the barrier to move to the armed position under the influence of impelling gas.
- retaining means such as a shear pin in a double-shear configuration (not shown), designed to prevent barrier 24 from moving in chamber 12 b in response to non-initiating stimuli, such as vibrations, but which permits the barrier to move to the armed position under the influence of impelling gas.
- the delayed initiation charge 22 is positioned for initiation of an output device disposed in the output transfer portion 12 e of the housing.
- an output device comprises an output initiating charge mounted within output transfer portion 12 e at the outlet aperture of the housing, so the delayed initiation charge 22 is preferably positioned close to the outlet aperture 12 g.
- output device 14 comprises an FCDCA, just as does input device 16 , and the end tip thereof (which contains the HNS initiation transfer charge) protrudes into output transfer portion 12 e of barrier chamber 12 b from the outlet aperture 12 g of the housing. There is a gap between the output device 14 and the delayed initiation charge 22 within which the shield segment 24 d of barrier member 24 can reside when it is in the safe position.
- the delayed initiation signal from delayed initiation charge 22 can initiate the output device 14 , which initiates the attached signal line 15 , which in turn can then initiate the principal functioning charge of the target device, e.g., a warhead, rocket motor, etc.
- the shield segment 24 d When in the safe position, the shield segment 24 d is physically disposed between delayed initiation charge 22 and output device 14 , and so shields the output device 14 from the debris, heat and shock of the signal generated by delayed initiation charge 22 , thus preventing the initiation of a signal in output device 14 .
- impelling gas is introduced into the barrier chamber 12 b to create a pressure difference from one side of piston segment 24 b to the other, with the greater pressure being in the impelling region 12 h below piston segment 24 b (as sensed in FIG. 1 ).
- the impelling gas may be obtained from input device 16 , i.e., from the function of the end tip thereof.
- fixture seat 13 is preferably configured to avoid forming a seal with delayed output component 17 (which would prevent gas flow beyond inlet aperture 13 b ).
- ferrule 26 is configured to leave a gas flow opening between its exterior surface and the interior surface of component chamber 12 a and a conduit 30 is provided to accommodate the flow of gas from component chamber 12 a to the impelling region 12 h of piston chamber 12 d.
- Conduit 30 may be provided by drilling a hole through housing 12 , through component chamber 12 a to barrier chamber 12 b and then plugging the hole with a plug 32 .
- a seal 20 c e.g., a ring seal or o-ring bushing, between ferrule 26 and the interior surface of component chamber 12 a prevents impelling gas from entering output transfer portion 12 e via the initiation aperture by which delayed initiation charge 22 has access to barrier chamber 12 b.
- Seal 20 c is positioned so that it does not impede the flow of impelling gas from input device 16 into conduit 30 , i.e., it is between the initiation aperture and the opening of conduit 30 to the component chamber 12 a.
- barrier member 24 is responsive to the flow of high pressure impelling gases generated by input device 16 into impelling region 12 a of barrier chamber 12 b via conduit 30 .
- the pressure beneath piston segment 24 b impels barrier member 24 upward (as sensed in FIG. 1 ), to the “armed” position, in which the shield segment 24 d of barrier member 24 is no longer disposed between delayed initiation charge 22 and output device 14 , so the delayed initiation signal from delayed initiation charge 22 can initiate output device 14 .
- the safe-arm device 10 comprises a retainer for holding barrier member 24 in the safe position, the retainer is designed so that it yields to the force imposed by the impelling gas.
- the shear pin is designed to shear under the force produced by the impelling gas. This occurs within a shorter time interval than the delay interval provided by delayed output component 17 between its initiation by input device 16 and the initiation of charge 22 .
- the impelling gas moves the barrier member from the safe position to the armed position within about 1 millisecond, whereas the delayed output component provides a delay of about 350 milliseconds.
- Cap 12 c is configured to withstand the impact of barrier member 24 when it moves to the armed position.
- the pressure of the gases in barrier chamber 12 b may keep barrier member 24 in the armed position for long enough to permit the initiation of the output device.
- a locking mechanism may be incorporated into safe-arm device 10 .
- the illustrated embodiment comprises locking means that include a spring-loaded locking pin 34 that bears on barrier member 24 , which includes a pin recess 24 a.
- pin 34 is received within pin recess 24 a, thus preventing barrier member 24 from returning to the safe position.
- the housing 12 is sealed by input device 16 , output device 14 , cap 12 c and plug 32 against the escape of gas from the housing. This helps assure that the impelling gas generates and maintains sufficient pressure to move barrier member 24 from the safe position to the armed position.
- safe-arm device 10 is initially configured as shown in FIG. 1 , with barrier member 24 in the safe position.
- input device 16 Upon receipt of an initiation signal from the external initiation signal line 18 , input device 16 emits an explosive signal which includes high pressure gases and a flyer plate (not shown). The flyer plate traverses expansion chamber 13 a and strikes percussion cap 28 which, in turn, initiates the delay composition in delay member 20 . Meanwhile, the expanding gases of input device 16 flow from inlet aperture 13 b through conduit 30 to the impelling region 12 h of barrier chamber 12 b to move barrier member 24 from the safe position to the armed position as indicated by the arrow (unnumbered).
- the delay member 20 after the pyrotechnic material 20 d is consumed, releases an explosive delayed initiation signal from delayed initiation charge 22 which initiates output device 14 .
- input device 16 directly initiates delayed output component 17 and also directly provides impelling gas to the barrier chamber 12 b.
- Pyrotechnic delay members such as delay member 20 are well-known in the art.
- the delayed output component 17 may comprise an electronic delay unit instead of a pyrotechnic delay member.
- An electronic delay unit that may be used with a non-electric input device may comprise a transducer for converting the non-electric input signal to an electrical signal, storage means for storing the converted input signal, an electrically initiated delayed initiation charge 22 and a timer-controlled switching circuit for releasing the stored input signal to the delayed initiation charge 22 after the desired interval.
- Electronic delay units of this kind are well-known in the art, as seen, e.g., in U.S. Pat. Nos. 5,377,592 and 6,079,332, both of which are hereby incorporated herein by reference as background information.
- impelling gas can be provided by an impelling gas source that is part of the safe-arm device itself and distinct from, but is responsive to, the input device, so the input device indirectly introduces the impelling gas into the housing.
- an impelling gas source that is part of the safe-arm device itself and distinct from, but is responsive to, the input device, so the input device indirectly introduces the impelling gas into the housing.
- safe-arm device 10 ′ comprises a housing 12 ′ within which direct initiation output device 14 and a delayed output component 17 are disposed. Housing 12 ′ defines a barrier chamber 12 b where barrier member 24 ′ is situated.
- Barrier member 24 ′ is movable between a safe position and an armed position to prevent or permit signal transfer from the delayed output component 17 to an output device 14 following receipt of an input signal from an input device 16 . All of these structures function in substantially the same way as their corresponding structures in safe-arm device 10 ( FIG. 1 ), except as indicated by the following description.
- Device 10 ′ comprises a signal transfer device 35 such as an FCDCA having a signal transfer fixture on each end of the signal line.
- the signal transfer device 35 may comprise any other kind of signal line such as shock tube, low velocity signal tube, etc., with suitable signal transfer fixtures (e.g., initiation caps or squibs) at opposite ends thereof.)
- the signal transfer device 35 comprises an arming fixture 36 that is secured in housing 12 ′ and which comprises an end tip configured and positioned to release the energized impelling gas into the impelling region 12 h of barrier chamber 12 b.
- Arming fixture 36 ′ functions in response to a signal received via signal transfer line 40 from input signal transfer fixture 38 , which is secured in housing 12 for initiation by input device 16 .
- Transfer fixture 38 transfers an initiation signal to arming fixture 36 within a time interval that is shorter than the delay interval provided by delay member 20 . Since safe-arm device 10 ′ thus comprises its own source of impelling gas (arming fixture 36 ), the input device need not be one that generates such gas. Further, since arming fixture 36 introduces impelling gas directly into the piston chamber, it is not necessary for housing 12 ′ to have a channel such as conduit 30 ( FIG. 1 ) to provide gas flow communication from input device 16 to barrier chamber 12 b.
- an initiation signal received via signal line 18 causes input device 16 to release an explosive initiation signal into housing 12 ′, which initiates transfer fixture 38 and percussion cap 28 .
- Transfer fixture 38 generates an initiation signal that is transferred via transfer line 40 to arming fixture 36 .
- the gases released from arming fixture 36 cause barrier member 24 ′ to move to the armed position.
- percussion cap 28 initiates delay member 20 .
- delay member 20 After passage of a delay interval imposed by the controlled burning of pyrotechnic delay material 20 d, by which time barrier member 24 ′ has moved to the armed position, delay member 20 generates an initiation signal from delayed initiation charge 22 .
- the output signal from delayed initiation charge 22 can initiate output device 14 .
- input fixture 16 has introduced impelling ‘gas into housing 12 ’ (albeit indirectly), and also initiated the delayed output component 17 .
- Device 10 a′ is shown as device 10 a′ in FIG. 2B .
- Device 10 a′ is generally similar in construction and function to device 10 ′, and corresponding structures there are labeled with corresponding reference numerals. Accordingly, the description of device 10 ′ of FIG. 2A will convey an understanding of device 10 a′ with the following additional explanation.
- Safe-arm device 10 a′ makes use of an input device that is situated to initiate the delayed output component upon receipt of an input signal from line 18 a, and is isolated (for purposes of providing impelling gas) from barrier chamber 12 b.
- Safe-arm device 10 a′ also comprises a gas-generating input device 36 a which is configured and situated in an inlet aperture to barrier chamber 12 b to release impelling gas into barrier chamber 12 b upon receipt of an input signal on line 18 b.
- the gas-generating input device 36 a is not responsive to the output from input device 16 .
- input device 36 a receives an initiating signal from line 18 b, which may obtain its input signal from a different source from the signal source for line 18 a, and the function of the different sources may be subject to different safety conditions from each other.
- the introduction of impelling gas into the housing is independent of the initiation of the delayed output component.
- safe-arm device 10 ′′ shown in FIG. 3A comprises a housing 12 ′′ that defines an inlet aperture 13 b that is connected via gas flow conduit 30 ′ to impelling region 12 h of barrier chamber 12 b. Housing 12 ′′ also defines a first transfer aperture 13 c in which a signal transfer device can be secured for communication with input device 16 .
- Housing 12 ′′ contains a barrier member 24 ′ which is movably disposed within barrier chamber 12 b.
- Barrier chamber 12 b and barrier member 24 ′ are similar to the corresponding barrier member 24 and barrier chamber 12 b of the embodiments of FIGS. 1 and 2 , except that barrier member 24 ′′ does not have a pressure relief aperture, such as aperture 24 e of piston 24 ( FIG.
- Barrier member 24 ′ is equipped with ring seal 24 k in piston segment 24 b′ and ring seals 24 m in middle segment 24 c′ to facilitate the achievement of the seals described above.
- the delayed output component is isolated from input device 16 by housing 12 ′′. Accordingly, signal transfer device 37 is provided to transfer an initiation signal from input device 16 to the delayed output component 17 .
- Transfer device 37 comprises a transfer fixture 38 that is positioned for initiation by input fixture 16 , and to convey the signal to a signal line 18 and, in turn, to fixture 36 .
- Fixture 36 is similar in configuration to input fixture 16 of FIG. 1 or FIG. 2A , and is configured and situated to be able to initiate the delayed output component 17 .
- Delayed output component 17 of safe-arm device 10 ′′ has the same as configuration and function as delayed output component 17 of device 10 ′ ( FIG. 2A ).
- Safe-arm device 10 ′′ is generally similar to safe-arm device 10 ′ ( FIG. 2A ) with the following exceptions.
- a gas flow conduit 30 ′ permits gas flow from two fixtures, input fixture 16 and transfer fixture 38 , to the impelling region 12 h of barrier chamber 12 b′, thus approximately doubling the pressure of the impelling gas that drives barrier member 24 ′ relative to devices 10 and 10 ′.
- transfer fixture 38 constitutes a gas-generating fixture of device 10 ′′.
- inlet aperture 13 b is isolated from delayed output component 17 , so impelling gas will not be introduced into output region 12 e via the initiation aperture by which delayed output component 17 is open to barrier chamber 12 b.
- the increased pressure of the impelling gas in impelling region 12 h relative to devices 10 and 10 ′ makes it unnecessary to provide barrier member 24 ′ with a pressure relief aperture such as aperture 24 e ( FIG. 1 ), since the impelling gas will have sufficient pressure to move barrier member 24 ′ to an armed position despite the compression of gases in the upper portion of barrier chamber 12 b′.
- device 10 ′′ comprises a shear pin to provide a retainer to keep barrier member 24 ′ in the safe position until an input signal is received.
- barrier member 24 ′ comprises tabs 24 f ( FIG. 3B ) on an upward-extending blade 24 g on piston segment 24 b. Tabs 24 f are configured to engage vertical slots (not shown) in barrier chamber 12 b to prevent barrier member 24 ′ from rotating as it moves to its armed position.
- Barrier chamber 12 b defines flared shoulders 12 f adjacent cap 12 c, and tabs 24 f are deformable so that when impelling gas causes barrier member 24 ′ to strike cap 12 c, tabs 24 f are deformed by the contact with cap 12 c and engage shoulders 12 f, thus preventing barrier member 24 ′ from reversing direction and moving downward, towards the safe position.
- delayed output component 17 initiates output fixture 14 as previously described for devices 10 and 10 ′.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Manipulator (AREA)
- Automotive Seat Belt Assembly (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
This invention provides a protective safe-arm device (10) for use with a delayed output component (17) that can be coupled to an input device (16) and to an output device (14) to interpose a delay between the receipt of an initiation signal from the input device (16) and the issuance of the signal to an output device (14), which may communicate with, or be part of, an explosively-activated target device, e.g., a rocket motor, warhead, etc. The safe-arm device (10) is configured so that before the output device (14) is intended to function, a barrier member (24) resides between the output device (14) and the delayed output component (17) therein. Thus, should the delayed output component (17) function inadvertently, I will fail to initiate the output device (14). However, a signal received from the input device (16) causes the introduction into the housing of an impelling gas which moves the barrier member (24) away from its protective position, thus permitting the delayed output component (17) to initiate the output device (14).
Description
- This application claims the benefit of U.S. provisional application serial No. 60/424,988, filed Nov. 8, 2002.
- 1. Field of the Invention
- This invention relates to an explosive-activated safe-arm device for conveying non-electric initiation signals.
- Various kinds of devices are designed to function in response to a non-electric, e.g., explosive, initiation signal from an external initiation source. Often, the external initiation source comprises a signal transfer line that is connected to the device in a manner that permits the release of an explosive initiation signal from the signal line to the device. The signal line may comprise detonating cord, which inherently transmits an explosive output signal at all points along its length, but which is typically equipped with a coupling fixture to facilitate the connection of the signal line and the transfer of the explosive initiation signal to a target device. Alternatively, the signal line may comprise a signal tube, such as shock tube, having an end fixture coupled thereto, e.g., a detonator or pyrotechnic initiator, that is configured to generate a brisant output from the signal in the signal tube. For some devices it is necessary to include a delay member to interpose a time delay between the receipt of the explosive signal from the external initiation source and the transfer of the initiation signal to the explosively initiated device. Delay members typically comprise means for generating an explosive output signal at the end of the delay interval following the receipt of an initiation signal. The explosively initiated device or “target device” further comprises a direct-initiation fixture designed to receive the explosive output signal from the delay member and to function in response thereto, typically without delay.
- Some delay members are liable to initiation apart from receipt of the external explosive initiation signal, and may then cause unintended functioning of the target device. Avoidance of such unintentional functioning is generally recognized as an important design goal, especially when there is a high cost associated with the functioning of the target device (e.g., target devices such as warheads and rocket motors).
- 2. Related Art
- U.S. Pat. No. 2,737,892 to Dalton et al, entitled “On-Off Self Destruction Base Fuze”, dated Mar. 13, 1956, discloses a fuze for the self destruction of a projectile that fails to function normally. The device is mounted within the explosive or propulsive charge in the projectile casing. The device includes a housing within which is disposed a delay powder train 31 with an associated output charge, detonator 29. The output charge must initiate a
booster charge 32 via explosive pellets 42 and 43 in order to initiate self destruction of the projectile. The intervening pellets 42 and 43 are mounted on rotatable plates which, when the projectile rotates as a result of being fired, move in response to the rotation by aligning the pellets. Should the projectile still be rotating in flight by the time the delay train has been consumed, the output charge 29 will initiate thebooster charge 32 by initiating, in sequence, the aligned intervening pellets 43 and 42. Theplates 17 are eccentrically-mounted rotors which are moved by centrifugal force when the projectile is in flight. - U.S. Pat. No. 4,328,754 to Goodman, dated May 11, 1982 and entitled “Time Delay Device”, discloses a mechanism for the delayed release of a spring-driven firing pin. The operation of the release depends upon the movement of a release piston under the force of a spring. The action of the spring, however, is resisted by a reservoir of gas which must be dissipated through a narrow aperture to permit the piston to move. Thus, the gas controls the speed of the piston and thus determines a delay interval between the activation of the delay device and the release of the firing pin.
- U.S. Pat. No. 4,660,473 to Bender et al, dated Apr. 28, 1987, entitled “Compressed Gas-Actuated Mechanical Power Element”, discloses a housing containing a pair of movable pistons that can be extended from the housing under the force of compressed gas introduced into the housing.
- U.S. Pat. No. 4,932,325 to Hütter, dated Jun. 12, 1990, entitled “Safety Device For An Aerodynamic Body Fuse”, discloses a device for an aerodynamic body, in which functional parts are mounted on a slide that can be moved from a safe position within the contour of the body to an armed position beyond the contour of the body. The slide defines two air passages that face in opposite directions, so that when the slide is disposed in a moving air stream, a different air pressure is created in each perforation. The perforations communicate with a piston chamber and the difference in pressure is employed to move a piston from a safe position to an armed position.
- U.S. Pat. No. 3,938,443 to Wolski, dated Feb. 17, 1976, entitled “Logic Module”, discloses a mechanical logic module for a missile fuse device. The logic module makes use of the passage of air through a conduit to create a pressure differential to operate a piston. The piston rotates a cam which constitutes part of a safe-arm device.
- A prior art safing mechanism employed on aerospace devices is illustrated schematically in
FIG. 4 . In this device, aninput fixture 116 and an output (receiving)fixture 114 are mounted for signal transfer from one to the other in ahousing 112. Thehousing 112 defines a piston chamber 112 b within which abarrier piston 124 resides.Barrier piston 124 includes ashield portion 124 a that can be disposed between 116 and 114 to prevent signal transfer from one to the other. Barrierfixture piston 124 is initially in an “armed” position, in whichshield portion 124 a does not obstruct signal transfer fromfixture 116 tofixture 114.Safing device 110 includes acap 113 that is configured to receive a safing fixture 111. Each of 116, 114 and 111 comprises a threaded stainless steel ferrule that can be secured tofixtures housing 112 orcap 113, respectively, and which is secured to a signal transmission device (detonating cord) that terminates in an explosive-filled cup that protrudes through the ferrule intohousing 112. In normal use, an input signal received on the signal line connected toinput fixture 116 causes an initiation signal to be released intohousing 112 to initiate a signal in theoutput fixture 114. However, should safing fixture 111 receive a safing signal, it will release gas into the top portion of chamber 112 b that will impelbarrier piston 124 downward (as sensed inFIG. 4 ) so that theshield portion 124 a will obstruct the transfer of a signal fromfixture 116 tofixture 114. The signal that initiates safing fixture 111 may be generated in response to an external condition that would make the initiation of a signal inoutput fixture 114 undesirable. - This invention provides a safe-arm device comprising a housing defining at least one inlet aperture, an outlet aperture, and a barrier chamber. There is a barrier member in the barrier chamber that is movable therein from a safe position to an armed position in response to impelling gas introduced into the housing. There is also a delayed output component in the housing. The delayed output component is responsive to an input signal, for generating a delayed initiation signal. The barrier member, when in the safe position, is situated to inhibit initiation of an output device in the outlet aperture by the delayed output component and, when in the armed position, is situated to permit the delayed output component to initiate such output device.
- According to one aspect of the invention, the barrier member, when in the safe position, may be situated between the delayed output component and the outlet aperture.
- According to another aspect of the invention, the device may be configured to admit impelling gas from an input device in the inlet aperture into the barrier chamber to move the barrier member.
- Optionally, the device may comprise an impelling gas source that is responsive to a signal from an input device. For example, the device may comprise a signal transfer device that comprises first and second signal transfer fixtures joined by a signal line. The first signal transfer fixture may be secured in the housing and configured for initiation by an input device in the inlet aperture and the second signal transfer fixture may comprise an arming fixture comprising the impelling gas source, and may be secured in the housing to release gas into the barrier chamber in response to a signal from the first signal transfer fixture. Alternatively, the first signal transfer fixture may comprise an arming fixture comprising the impelling gas source and may be secured in the housing to release gas into the barrier chamber in response to a signal from an input fixture, and the second signal transfer fixture may be secured in the housing and configured to initiate the delayed output component in response to a signal from the first signal transfer fixture.
- According to various other aspects of the invention, the device may be combined with an input device secured in each inlet aperture for initiating the delayed output component and introducing impelling gas into the housing, and with an output device secured in the outlet aperture for initiation by the delayed output component. In such case, the housing is preferably sealed against the escape of impelling gas.
- Optionally, there may be a single input device for both introducing impelling gas into the housing and initiating the delayed output component. Alternatively, one input device may introduce the impelling gas and another may initiate the delayed output component.
- The barrier chamber may comprise a piston chamber portion and an output initiation portion. The barrier member may comprise a piston segment in the piston chamber portion, and a middle segment and a shield segment in the output initiation portion of the barrier chamber, wherein the middle segment of the barrier member is configured to substantially isolate the outlet aperture from impelling gas introduced into the piston chamber portion.
-
FIG. 1 is a schematic cross-sectional view of a safe-arm device according to a first embodiment of the invention; -
FIG. 2A is a schematic cross-sectional view of a safe-arm device according to a second embodiment of the invention; -
FIG. 2B is a view of a device similar toFIG. 2A except that it comprises two input devices, one of which is a gas-generating fixture which is independent of i.e., not responsive to, the other input fixture; -
FIG. 3A is a schematic cross-sectional view of a safe-arm device according to a third embodiment of the invention; -
FIG. 3B is a schematic cross-sectional view of a portion of the barrier member in a portion of the barrier chamber of the device ofFIG. 3A ; and -
FIG. 4 is a schematic cross-sectional view of a prior art safing device. - The safe-arm device of this invention finds utility in various fields, including aerospace and military applications, for reliably transferring a non-electric initiation signal through a housing from an input device to an output device. The safe-arm device includes a delayed output component which generates an initiation signal for an output device coupled to the housing after a delay interval following the receipt of a signal from the input device (the input signal). To prevent the delayed output component from inadvertently initiating the output device in the absence of an input signal from an input device, there is a movable barrier member in the housing that is initially positioned to inhibit the transfer of a delayed initiation signal from the delayed output component to an output device, i.e., it is initially in a “safe” position between the delayed output component and the output device. However, the barrier member is movable to a non-inhibiting position, i.e., to an “armed” position, in which it permits the delayed output component to initiate the output device. The delayed output component may function solely to postpone the initiation of the output device for an interval sufficient to permit movement of the barrier member, or it may serve additional functions (such as the initiation of other devices) during the delay interval as well.
- The safe-arm device may include a retainer (e.g., a shear pin) for releasably retaining the barrier in the safe position until the receipt of the input signal, and may also include a locking mechanism (e.g., locking tabs and grooves) to keep the barrier in the armed position thereafter.
- Preferably, the barrier member is movable in response to the introduction of impelling gas into the housing when the input signal is received. In such embodiments, the housing defines a barrier chamber in which a piston portion of the barrier member resides. A pressure difference from one side of the piston portion to the other will cause the barrier member to move. To assure that the impelling gas, which may be highly energetic (i.e., hot and highly pressurized), moves the barrier member but does not initiate the output device, the housing and barrier member are configured so that the output device is substantially isolated from the impelling gas.
- Should the delayed output component function inadvertently, i.e., without the receipt of an input signal to generate impelling gas, the barrier member will prevent the delayed output component from initiating the output device by blocking the debris, heat and shock of the delayed initiation signal from the output device. Gas produced by the delayed output component may also move the barrier from the safe position, but such movement would occur after the delayed initiation signal has been blocked from the output device.
- In some embodiments of this invention, the impelling gas is obtained at least in part from an input device that has been secured to the housing. In such embodiment, the input device comprises a gas-generating fixture which introduces impelling gas into the housing, and the housing is configured so that the impelling gas can flow into an impelling region in the barrier chamber from the input device. In other embodiments, the safe-arm device of this invention comprises a gas-generating fixture that is distinct from, but responsive to, the input device, and the input device need not contribute impelling gas. In still other embodiments, the impelling gas is provided by the input device together with gas from a gas-generating fixture responsive to it. Optionally, there may be an intervening signal transfer device to convey an initiation signal from an input device to the delayed output component, or from the input device to a gas-generating fixture for the generation of impelling gas. According to still other embodiments, the distinct gas-generating fixture may constitute an input device that is distinct from the input device that initiates the delayed output component.
- Preferably, all devices mounted in the housing, e.g., the at least one input device, output device and the optional signal transfer device and gas-generating fixture, etc., form a seal with the housing so that the impelling gas is not subject to loss in pressure due to leakage from the housing, and to prevent the introduction of gas into the housing from the environment. By sealing the safe-arm device against gas leaks, the maximum efficacy of impelling gas introduced into the device will be obtained and the need for an external power source for moving the barrier member can be avoided, i.e., the device can be self-contained.
- One embodiment of an explosive safe-arm device in accordance with this invention is seen in
FIG. 1 together with aninput device 16 and anoutput device 14. Safe-arm device 10 comprises ahousing 12 which includes afixture seat 13 a.Fixture seat 13 a defines aninlet aperture 13 b which includes anexpansion chamber 13 aHousing 12 encloses a delayedoutput component 17 in acomponent chamber 12 a. There is abarrier chamber 12 b inhousing 12 and abarrier member 24 movably disposed therein, and anoutlet aperture 12 g. Aninput device 16 is secured ininlet aperture 13 b and anoutput device 14 is secured inoutlet aperture 12 g andhousing 12 is otherwise sealed such that gas cannot enter or escapehousing 12. Theinput device 16 is capable of emitting a signal that can initiate the delayedoutput component 17. It also introduces impelling gas into the housing to move thebarrier member 24, as described below. - In the illustrated embodiment,
input device 16 comprises aninput fixture 16 a secured to asignal line 18 such as detonating cord.Input device 16 may optionally comprise an FCDCA (flexible confined detonating cord assembly), a type of signal-transfer apparatus well known in the art. When initiated, the end tip of an FCDCA generates a brisant output signal and a flyer plate derived from the cup. (An FCDCA can also be used to receive a signal and transfer the signal to the detonating cord thereof, as occurs with theoutput device 14. Accordingly, the end fixture of an FCDCA is referred to herein generically as a signal transfer fixture.) Accordingly,input fixture 16 a is a signal transfer fixture comprising a longitudinal bore therethrough where a signal transfer line comprising a flexible, confined detonating cord (e.g., a length of 2.7 grains per foot HNS-IIA Aluminum Mild detonating fuse, surrounded by flexible shielding (which my included braided stainless steel with moisture barrier therein)) is received. Anend tip 16 b comprising a transfer charge of reactive (i.e., pyrotechnic or explosive) material such as HNS disposed in a cup is secured on the end of the signal transfer line and protrudes from thefixture 16 aInput fixture 16 a is configured so that it can easily be secured to the housing (e.g., it may have screw threads that mate with threads in the housing) withend tip 16 b in position for signal transfer with another device (e.g., for initiation of a delay device or signal transfer device). -
Delayed output component 17 includes adelay member 20 and aferrule 26 which carries apercussion cap 28.Delay member 20 comprises asleeve 20 b filled with apyrotechnic delay material 20 d.Sleeve 20 b carries anannular flange 20 a disposed concentrically aboutdelay member 20. The input end ofsleeve 20 b is disposed withinferrule 26, which is secured to flange 20 a.Ferrule 26 defines an expansion chamber arounddelay member 20 to permit the expansion of gas generated bydelay material 20 d.Ferrule 26 carriespercussion cap 28 at a position where thecap 28 can be initiated by an input device secured in the inlet aperture of the housing, and where, upon initiation,cap 28 will initiate thedelay material 20 d from across a short spacing gap. Aseal 27 on the end offerrule 26 covers overpercussion cap 28 to protect the cap against desensitization by environmental factors, e.g., moisture.Seal 27 is sufficiently thin andinput device 16 is sufficiently powerful thatseal 27 does not preventinput device 16 from initiatingcap 28.Ferrule 26 is configured so that it leaves an annular gas-flow passage about its exterior, between itself and the interior surface ofcomponent chamber 12 a, for reasons discussed below. - The output end of
sleeve 20 b carries a delayedinitiation charge 22 which contains a charge of reactive material, e.g., an explosive material such as HNS, in a cup and which is sensitive to initiation bypyrotechnic delay material 20 d. As shown, delayedinitiation charge 22 has access tobarrier chamber 12 b fromcomponent chamber 12 a via an initiation aperture (unnumbered) in the housing. When initiated, delayedinitiation charge 22 releases a delayed initiation signal that may include a flyer and that is sufficiently energetic to initiate an output device. -
Housing 12 defines abarrier chamber 12 b within whichbarrier member 24 resides. One portion ofbarrier chamber 12 b, which is closed bybarrier plug 12 c, is referred to herein as apiston chamber 12 d, and another portion ofbarrier chamber 12 b is anoutput transfer portion 12 e. Apiston segment 24 b ofbarrier member 24 is configured to closely match the walls ofpiston chamber 12 d and amiddle segment 24 c ofbarrier member 24 is configured for a substantially sealing fit withinoutput transfer portion 12 e.Barrier chamber 12 b andbarrier member 24 are configured to preventbarrier member 24 from rotating withinchamber 12 b, e.g., they may comprise a groove and slot engagement between them. - High-pressure impelling gas can be introduced into
piston chamber 12 d at a point belowpiston segment 24 b (as sensed inFIG. 1 ) (referred to herein as the impellingregion 12 h), where the impelling gas is blocked from direct entry intooutput transfer portion 12 e bymiddle segment 24 c ofbarrier member 24. The high pressure in the impellingregion 12 h will causebarrier member 24 to move as indicated by the upward-pointing arrow inFIG. 1 . - A longitudinal
pressure relief aperture 24 e extends from the top of thepiston segment 24 b ofbarrier member 24 to the bottom of theshield segment 24 d. At least some of the non-impelling gas in the upper portion ofbarrier chamber 12 b (as sensed inFIG. 1 ) that would otherwise be compressed by the motion ofbarrier member 24 to its armed position may therefore be displaced into theoutput transfer portion 12 e ofbarrier chamber 12 b. Thus, resistance against the movement ofbarrier member 24 to the armed position due to the compression of non-impelling gas in the housing is significantly reduced. Nevertheless,middle segment 24 c ofbarrier member 24 substantially establishes a seal withbarrier chamber 12 b to prevent the entry of impelling gas from thepiston chamber 12 d intooutput transfer portion 12 e. Thus,barrier member 24 is configured to isolate the outlet aperture, and an output device mounted therein, from impelling gas. The seals established bypiston segment 24 b andmiddle segment 24 c may be facilitated by the use of ring seals, as shown indevice 10″,FIG. 3A . -
Delayed initiation charge 22 ofdelayed output component 17 is positioned so that when initiated, it releases a signal, optionally including a flyer, intooutput transfer portion 12 e, for initiating an output device.Barrier member 24 includes ashield segment 24 d extending frommiddle segment 24 c.Shield segment 24 d is configured to be interposed between the delayedinitiation charge 22 and an output device whenbarrier member 24 is in the safe position. Optionally, theshield segment 24 d may be designed to simulate a fixed, simply-supported beam, rather than a fixed-free beam. - Optionally,
barrier member 24 may be held in the safe position by retaining means such as a shear pin in a double-shear configuration (not shown), designed to preventbarrier 24 from moving inchamber 12 b in response to non-initiating stimuli, such as vibrations, but which permits the barrier to move to the armed position under the influence of impelling gas. - As indicated above, the delayed
initiation charge 22 is positioned for initiation of an output device disposed in theoutput transfer portion 12 e of the housing. Typically, an output device comprises an output initiating charge mounted withinoutput transfer portion 12 e at the outlet aperture of the housing, so the delayedinitiation charge 22 is preferably positioned close to theoutlet aperture 12 g. In the illustrated embodiment,output device 14 comprises an FCDCA, just as doesinput device 16, and the end tip thereof (which contains the HNS initiation transfer charge) protrudes intooutput transfer portion 12 e ofbarrier chamber 12 b from theoutlet aperture 12 g of the housing. There is a gap between theoutput device 14 and the delayedinitiation charge 22 within which theshield segment 24 d ofbarrier member 24 can reside when it is in the safe position. Absent the interveningshield segment 24 d, the delayed initiation signal from delayedinitiation charge 22 can initiate theoutput device 14, which initiates the attachedsignal line 15, which in turn can then initiate the principal functioning charge of the target device, e.g., a warhead, rocket motor, etc. When in the safe position, theshield segment 24 d is physically disposed between delayedinitiation charge 22 andoutput device 14, and so shields theoutput device 14 from the debris, heat and shock of the signal generated by delayedinitiation charge 22, thus preventing the initiation of a signal inoutput device 14. - To move
barrier member 24 from the safe position to the armed position, impelling gas is introduced into thebarrier chamber 12 b to create a pressure difference from one side ofpiston segment 24 b to the other, with the greater pressure being in the impellingregion 12 h belowpiston segment 24 b (as sensed inFIG. 1 ). Optionally, as in the embodiment of FIG. 1, the impelling gas may be obtained frominput device 16, i.e., from the function of the end tip thereof. Accordingly,fixture seat 13 is preferably configured to avoid forming a seal with delayed output component 17 (which would prevent gas flow beyondinlet aperture 13 b). In addition,ferrule 26 is configured to leave a gas flow opening between its exterior surface and the interior surface ofcomponent chamber 12 a and aconduit 30 is provided to accommodate the flow of gas fromcomponent chamber 12 a to the impellingregion 12 h ofpiston chamber 12 d. (Conduit 30 may be provided by drilling a hole throughhousing 12, throughcomponent chamber 12 a tobarrier chamber 12 b and then plugging the hole with aplug 32.) Aseal 20 c, e.g., a ring seal or o-ring bushing, betweenferrule 26 and the interior surface ofcomponent chamber 12 a prevents impelling gas from enteringoutput transfer portion 12 e via the initiation aperture by which delayedinitiation charge 22 has access tobarrier chamber 12 b.Seal 20 c is positioned so that it does not impede the flow of impelling gas frominput device 16 intoconduit 30, i.e., it is between the initiation aperture and the opening ofconduit 30 to thecomponent chamber 12 a. - The movement of
barrier member 24 is responsive to the flow of high pressure impelling gases generated byinput device 16 into impellingregion 12 a ofbarrier chamber 12 b viaconduit 30. The pressure beneathpiston segment 24 b impelsbarrier member 24 upward (as sensed inFIG. 1 ), to the “armed” position, in which theshield segment 24 d ofbarrier member 24 is no longer disposed between delayedinitiation charge 22 andoutput device 14, so the delayed initiation signal from delayedinitiation charge 22 can initiateoutput device 14. If the safe-arm device 10 comprises a retainer for holdingbarrier member 24 in the safe position, the retainer is designed so that it yields to the force imposed by the impelling gas. For example, if the retainer comprises a shear pin, the shear pin is designed to shear under the force produced by the impelling gas. This occurs within a shorter time interval than the delay interval provided bydelayed output component 17 between its initiation byinput device 16 and the initiation ofcharge 22. In a particular embodiment, the impelling gas moves the barrier member from the safe position to the armed position within about 1 millisecond, whereas the delayed output component provides a delay of about 350 milliseconds.Cap 12 c is configured to withstand the impact ofbarrier member 24 when it moves to the armed position. In some embodiments, the pressure of the gases inbarrier chamber 12 b may keepbarrier member 24 in the armed position for long enough to permit the initiation of the output device. Preferably, to assure thatbarrier member 24 remains in the armed position, a locking mechanism may be incorporated into safe-arm device 10. The illustrated embodiment comprises locking means that include a spring-loadedlocking pin 34 that bears onbarrier member 24, which includes apin recess 24 a. Whenbarrier member 24 reaches its armed position, pin 34 is received withinpin recess 24 a, thus preventingbarrier member 24 from returning to the safe position. - In the illustrated embodiment, the
housing 12 is sealed byinput device 16,output device 14,cap 12 c and plug 32 against the escape of gas from the housing. This helps assure that the impelling gas generates and maintains sufficient pressure to movebarrier member 24 from the safe position to the armed position. - In operation, safe-
arm device 10 is initially configured as shown inFIG. 1 , withbarrier member 24 in the safe position. Upon receipt of an initiation signal from the externalinitiation signal line 18,input device 16 emits an explosive signal which includes high pressure gases and a flyer plate (not shown). The flyer plate traversesexpansion chamber 13 a and strikespercussion cap 28 which, in turn, initiates the delay composition indelay member 20. Meanwhile, the expanding gases ofinput device 16 flow frominlet aperture 13 b throughconduit 30 to the impellingregion 12 h ofbarrier chamber 12 b to movebarrier member 24 from the safe position to the armed position as indicated by the arrow (unnumbered). Thedelay member 20, after thepyrotechnic material 20 d is consumed, releases an explosive delayed initiation signal from delayedinitiation charge 22 which initiatesoutput device 14. Thus,input device 16 directly initiates delayedoutput component 17 and also directly provides impelling gas to thebarrier chamber 12 b. - Pyrotechnic delay members such as
delay member 20 are well-known in the art. In alternative embodiments, the delayedoutput component 17 may comprise an electronic delay unit instead of a pyrotechnic delay member. An electronic delay unit that may be used with a non-electric input device may comprise a transducer for converting the non-electric input signal to an electrical signal, storage means for storing the converted input signal, an electrically initiated delayedinitiation charge 22 and a timer-controlled switching circuit for releasing the stored input signal to the delayedinitiation charge 22 after the desired interval. Electronic delay units of this kind are well-known in the art, as seen, e.g., in U.S. Pat. Nos. 5,377,592 and 6,079,332, both of which are hereby incorporated herein by reference as background information. - As mentioned above, it is not necessary that the impelling gas come directly from an input device. Optionally, impelling gas can be provided by an impelling gas source that is part of the safe-arm device itself and distinct from, but is responsive to, the input device, so the input device indirectly introduces the impelling gas into the housing. For example, in the embodiment of
FIG. 2A , safe-arm device 10′ comprises ahousing 12′ within which directinitiation output device 14 and adelayed output component 17 are disposed.Housing 12′ defines abarrier chamber 12 b wherebarrier member 24′ is situated.Barrier member 24′ is movable between a safe position and an armed position to prevent or permit signal transfer from the delayedoutput component 17 to anoutput device 14 following receipt of an input signal from aninput device 16. All of these structures function in substantially the same way as their corresponding structures in safe-arm device 10 (FIG. 1 ), except as indicated by the following description. -
Device 10′ comprises asignal transfer device 35 such as an FCDCA having a signal transfer fixture on each end of the signal line. (Alternatively, thesignal transfer device 35 may comprise any other kind of signal line such as shock tube, low velocity signal tube, etc., with suitable signal transfer fixtures (e.g., initiation caps or squibs) at opposite ends thereof.) Thesignal transfer device 35 comprises an armingfixture 36 that is secured inhousing 12′ and which comprises an end tip configured and positioned to release the energized impelling gas into the impellingregion 12 h ofbarrier chamber 12 b. Armingfixture 36′ functions in response to a signal received viasignal transfer line 40 from inputsignal transfer fixture 38, which is secured inhousing 12 for initiation byinput device 16.Transfer fixture 38 transfers an initiation signal to armingfixture 36 within a time interval that is shorter than the delay interval provided bydelay member 20. Since safe-arm device 10′ thus comprises its own source of impelling gas (arming fixture 36), the input device need not be one that generates such gas. Further, since armingfixture 36 introduces impelling gas directly into the piston chamber, it is not necessary forhousing 12′ to have a channel such as conduit 30 (FIG. 1 ) to provide gas flow communication frominput device 16 tobarrier chamber 12 b. - In use, an initiation signal received via
signal line 18 causesinput device 16 to release an explosive initiation signal intohousing 12′, which initiatestransfer fixture 38 andpercussion cap 28.Transfer fixture 38 generates an initiation signal that is transferred viatransfer line 40 to armingfixture 36. The gases released from armingfixture 36cause barrier member 24′ to move to the armed position. Meanwhile,percussion cap 28 initiates delaymember 20. After passage of a delay interval imposed by the controlled burning ofpyrotechnic delay material 20 d, by whichtime barrier member 24′ has moved to the armed position,delay member 20 generates an initiation signal from delayedinitiation charge 22. Withbarrier member 24′ in the armed position, the output signal from delayedinitiation charge 22 can initiateoutput device 14. Thus,input fixture 16 has introduced impelling ‘gas into housing 12’ (albeit indirectly), and also initiated the delayedoutput component 17. - Another embodiment of this invention is shown as device 10 a′ in
FIG. 2B . Device 10 a′ is generally similar in construction and function todevice 10′, and corresponding structures there are labeled with corresponding reference numerals. Accordingly, the description ofdevice 10′ ofFIG. 2A will convey an understanding of device 10 a′ with the following additional explanation. - Safe-arm device 10 a′, like safe-
arm device 10′ ofFIG. 2A , makes use of an input device that is situated to initiate the delayed output component upon receipt of an input signal from line 18 a, and is isolated (for purposes of providing impelling gas) frombarrier chamber 12 b. Safe-arm device 10 a′ also comprises a gas-generating input device 36 a which is configured and situated in an inlet aperture tobarrier chamber 12 b to release impelling gas intobarrier chamber 12 b upon receipt of an input signal on line 18 b. However, unlikefixture 36 ofdevice 10′ (FIG. 2A ), the gas-generating input device 36 a is not responsive to the output frominput device 16. Instead, input device 36 a receives an initiating signal from line 18 b, which may obtain its input signal from a different source from the signal source for line 18 a, and the function of the different sources may be subject to different safety conditions from each other. Thus, the introduction of impelling gas into the housing is independent of the initiation of the delayed output component. - In yet another embodiment of this invention, safe-
arm device 10″ shown inFIG. 3A comprises ahousing 12″ that defines aninlet aperture 13 b that is connected viagas flow conduit 30′ to impellingregion 12 h ofbarrier chamber 12 b.Housing 12″ also defines afirst transfer aperture 13 c in which a signal transfer device can be secured for communication withinput device 16.Housing 12″ contains abarrier member 24′ which is movably disposed withinbarrier chamber 12 b.Barrier chamber 12 b andbarrier member 24′ are similar to thecorresponding barrier member 24 andbarrier chamber 12 b of the embodiments ofFIGS. 1 and 2 , except thatbarrier member 24″ does not have a pressure relief aperture, such asaperture 24 e of piston 24 (FIG. 2A ), which is unnecessary in safe-arm device 10″, for reasons discussed below.Barrier member 24′ is equipped with ring seal 24 k inpiston segment 24 b′ and ring seals 24 m inmiddle segment 24 c′ to facilitate the achievement of the seals described above. - In safe-
arm device 10″, the delayed output component is isolated frominput device 16 byhousing 12″. Accordingly, signal transfer device 37 is provided to transfer an initiation signal frominput device 16 to the delayedoutput component 17. Transfer device 37 comprises atransfer fixture 38 that is positioned for initiation byinput fixture 16, and to convey the signal to asignal line 18 and, in turn, tofixture 36.Fixture 36 is similar in configuration to inputfixture 16 ofFIG. 1 orFIG. 2A , and is configured and situated to be able to initiate the delayedoutput component 17. -
Delayed output component 17 of safe-arm device 10″ has the same as configuration and function asdelayed output component 17 ofdevice 10′ (FIG. 2A ). - Safe-
arm device 10″ is generally similar to safe-arm device 10′ (FIG. 2A ) with the following exceptions. First, agas flow conduit 30′ permits gas flow from two fixtures,input fixture 16 andtransfer fixture 38, to the impellingregion 12 h ofbarrier chamber 12 b′, thus approximately doubling the pressure of the impelling gas that drivesbarrier member 24′ relative to 10 and 10′. Accordingly,devices transfer fixture 38 constitutes a gas-generating fixture ofdevice 10″. In addition,inlet aperture 13 b is isolated fromdelayed output component 17, so impelling gas will not be introduced intooutput region 12 e via the initiation aperture by which delayedoutput component 17 is open tobarrier chamber 12 b. Further, the increased pressure of the impelling gas in impellingregion 12 h relative to 10 and 10′ makes it unnecessary to providedevices barrier member 24′ with a pressure relief aperture such asaperture 24 e (FIG. 1 ), since the impelling gas will have sufficient pressure to movebarrier member 24′ to an armed position despite the compression of gases in the upper portion ofbarrier chamber 12 b′. - Furthermore,
device 10″ comprises a shear pin to provide a retainer to keepbarrier member 24′ in the safe position until an input signal is received. Also,barrier member 24′ comprisestabs 24 f (FIG. 3B ) on an upward-extendingblade 24 g onpiston segment 24 b.Tabs 24 f are configured to engage vertical slots (not shown) inbarrier chamber 12 b to preventbarrier member 24′ from rotating as it moves to its armed position.Barrier chamber 12 b defines flaredshoulders 12 fadjacent cap 12 c, andtabs 24 f are deformable so that when impelling gas causesbarrier member 24′ to strikecap 12 c,tabs 24 f are deformed by the contact withcap 12 c and engageshoulders 12 f, thus preventingbarrier member 24′ from reversing direction and moving downward, towards the safe position. Whenbarrier member 24′ is in the armed position,delayed output component 17 initiatesoutput fixture 14 as previously described for 10 and 10′.devices - Although the invention has been described with reference to particular embodiments thereof, it will be understood by one of ordinary skill in the art, upon a reading of the foregoing disclosure, that various alterations to the described embodiments fall within the scope and spirit of the invention.
Claims (12)
1. A safe-arm device comprising:
a housing defining at least one inlet aperture, an outlet aperture, and a barrier chamber,
a barrier member in the barrier chamber that is movable therein from a safe position to an armed position in response to impelling gas introduced into the housing; and
a delayed output component in the housing, the delayed output component being responsive to an input signal for generating a delayed initiation signal;
wherein the barrier member, when in the safe position, is situated to inhibit initiation of an output device in the outlet aperture by the delayed output component and, when in the armed position, is situated to permit the delayed output component to initiate such output device.
2. The device of claim 1 wherein the barrier member, when in the safe position, is situated between the delayed output component and the outlet aperture.
3. The device of claim 1 configured to admit impelling gas from an input device secured in the inlet aperture into the barrier chamber to move the barrier member.
4. The device of claim 1 further comprising an impelling gas source that is responsive to a signal from an input device.
5. The device of claim 4 comprising a signal transfer device that comprises first and second signal transfer fixtures joined by a signal line, wherein the first signal transfer fixture is secured in the housing and configured for initiation by an input device in the inlet aperture and wherein the second signal transfer fixture comprises an arming fixture comprising the impelling gas source and is secured in the housing to release gas into the barrier chamber in response to a signal from the first signal transfer fixture.
6. The device of claim 4 comprising a signal transfer device that comprises first and second signal transfer fixtures joined by a signal line, wherein the first signal transfer fixture comprises an arming fixture comprising the impelling gas source and is secured in the housing to release gas into the barrier chamber in response to a signal from an input fixture, and wherein the second signal transfer fixture is secured in the housing and configured to initiate the delayed output component in response to a signal from the first signal transfer fixture.
7. The device of claim 1 , claim 5 or claim 6 in combination with an input device secured in each inlet aperture for initiating the delayed output component and introducing impelling gas into the housing, and further in combination with an output device secured in the outlet aperture for initiation by the delayed output component.
8. The device of claim 7 wherein the housing is sealed against the escape of impelling gas.
9. The device of claim 7 having a single input device which both initiates the delayed output component and introduces the initiating gas into the housing.
10. The device of claim 7 having one input device for initiating the delayed output component and a second input device for introducing initiating gas into the housing independently of the first input device.
11. The device of any one of claims 1-6 wherein the barrier chamber comprises a piston chamber portion and an output initiation portion, wherein the barrier member comprises a piston segment in the piston chamber portion, and a middle segment and a shield segment in the output initiation portion of the barrier chamber, wherein the middle segment of the barrier member is configured to substantially isolate the outlet aperture from impelling gas introduced into the piston chamber portion.
12. The device of claim 7 wherein the barrier chamber comprises a piston chamber portion and an output initiation portion, wherein the barrier member comprises a piston segment in the piston chamber portion, and a middle segment and a shield segment in the output initiation portion of the barrier chamber, wherein the middle segment of the barrier member is configured to substantially isolate the outlet aperture from impelling gas introduced into the piston chamber portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/525,916 US20060124018A1 (en) | 2002-11-08 | 2005-08-04 | Explosive-activated safe-arm device |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US42498802P | 2002-11-08 | 2002-11-08 | |
| PCT/US2003/035419 WO2004111568A2 (en) | 2002-11-08 | 2003-11-07 | Explosive-activated safe-arm device |
| US10/525,916 US20060124018A1 (en) | 2002-11-08 | 2005-08-04 | Explosive-activated safe-arm device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20060124018A1 true US20060124018A1 (en) | 2006-06-15 |
Family
ID=33551206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/525,916 Abandoned US20060124018A1 (en) | 2002-11-08 | 2005-08-04 | Explosive-activated safe-arm device |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20060124018A1 (en) |
| AU (1) | AU2003304212A1 (en) |
| WO (1) | WO2004111568A2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7497164B1 (en) * | 2003-12-03 | 2009-03-03 | The United States Of America As Represented By The Secretary Of The Navy | Integrated thin film explosive micro-detonator |
| US7798064B1 (en) | 2007-04-26 | 2010-09-21 | Dse, Inc. | Command and arm fuze assembly having small piston actuator |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8191477B1 (en) | 2005-12-15 | 2012-06-05 | Sandia Corporation | Microelectromechanical safe arm device |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2737892A (en) * | 1948-12-14 | 1956-03-13 | Patrick J Dalton | On-off self destruction base fuze |
| US3889598A (en) * | 1968-06-18 | 1975-06-17 | Us Navy | Arming system |
| US3938443A (en) * | 1974-06-17 | 1976-02-17 | The United States Of America As Represented By The Secretary Of The Navy | Logic module |
| US4006689A (en) * | 1974-08-01 | 1977-02-08 | Etat Francais | Pyrotechnical safety relay |
| US4328754A (en) * | 1979-03-26 | 1982-05-11 | Commonwealth Of Australia | Time delay device |
| US4380197A (en) * | 1978-05-26 | 1983-04-19 | The United States Of America As Represented By The Secretary Of The Navy | Safety and arming device/contact fuze |
| US4455940A (en) * | 1982-06-28 | 1984-06-26 | The United States Of America As Represented By The Secretary Of The Army | Random time delay fuze |
| US4660473A (en) * | 1983-12-30 | 1987-04-28 | Dynamit Nobel Aktiengesellschaft | Compressed gas-actuated mechanical power element |
| US4730559A (en) * | 1987-01-08 | 1988-03-15 | The State Of Israel, Ministry Of Defence, Israel Military Industry | Safetied demolition charge fuze |
| US4932325A (en) * | 1988-08-26 | 1990-06-12 | Messerschmitt-Bolkow-Blohm Gmbh | Safety device for an aerodynamic body fuse |
| US5212340A (en) * | 1990-10-01 | 1993-05-18 | The United States Of America As Represented By The Secretary Of The Navy | Safe and arm device using liquid explosive |
| US5377592A (en) * | 1991-07-09 | 1995-01-03 | The Ensign-Bickford Company | Impulse signal delay unit |
| US6079332A (en) * | 1996-11-01 | 2000-06-27 | The Ensign-Bickford Company | Shock-resistant electronic circuit assembly |
| US6415717B1 (en) * | 2001-02-16 | 2002-07-09 | The United States Of America As Represented By The Secretary Of The Navy | Line charge assembly and system for use in shallow-water clearing operations |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3765332A (en) * | 1972-03-27 | 1973-10-16 | Us Navy | Water armed air safetied detonator |
-
2003
- 2003-11-07 AU AU2003304212A patent/AU2003304212A1/en not_active Abandoned
- 2003-11-07 WO PCT/US2003/035419 patent/WO2004111568A2/en not_active Ceased
-
2005
- 2005-08-04 US US10/525,916 patent/US20060124018A1/en not_active Abandoned
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2737892A (en) * | 1948-12-14 | 1956-03-13 | Patrick J Dalton | On-off self destruction base fuze |
| US3889598A (en) * | 1968-06-18 | 1975-06-17 | Us Navy | Arming system |
| US3938443A (en) * | 1974-06-17 | 1976-02-17 | The United States Of America As Represented By The Secretary Of The Navy | Logic module |
| US4006689A (en) * | 1974-08-01 | 1977-02-08 | Etat Francais | Pyrotechnical safety relay |
| US4380197A (en) * | 1978-05-26 | 1983-04-19 | The United States Of America As Represented By The Secretary Of The Navy | Safety and arming device/contact fuze |
| US4328754A (en) * | 1979-03-26 | 1982-05-11 | Commonwealth Of Australia | Time delay device |
| US4455940A (en) * | 1982-06-28 | 1984-06-26 | The United States Of America As Represented By The Secretary Of The Army | Random time delay fuze |
| US4660473A (en) * | 1983-12-30 | 1987-04-28 | Dynamit Nobel Aktiengesellschaft | Compressed gas-actuated mechanical power element |
| US4730559A (en) * | 1987-01-08 | 1988-03-15 | The State Of Israel, Ministry Of Defence, Israel Military Industry | Safetied demolition charge fuze |
| US4932325A (en) * | 1988-08-26 | 1990-06-12 | Messerschmitt-Bolkow-Blohm Gmbh | Safety device for an aerodynamic body fuse |
| US5212340A (en) * | 1990-10-01 | 1993-05-18 | The United States Of America As Represented By The Secretary Of The Navy | Safe and arm device using liquid explosive |
| US5377592A (en) * | 1991-07-09 | 1995-01-03 | The Ensign-Bickford Company | Impulse signal delay unit |
| US6079332A (en) * | 1996-11-01 | 2000-06-27 | The Ensign-Bickford Company | Shock-resistant electronic circuit assembly |
| US6415717B1 (en) * | 2001-02-16 | 2002-07-09 | The United States Of America As Represented By The Secretary Of The Navy | Line charge assembly and system for use in shallow-water clearing operations |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7497164B1 (en) * | 2003-12-03 | 2009-03-03 | The United States Of America As Represented By The Secretary Of The Navy | Integrated thin film explosive micro-detonator |
| US7798064B1 (en) | 2007-04-26 | 2010-09-21 | Dse, Inc. | Command and arm fuze assembly having small piston actuator |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2004111568A2 (en) | 2004-12-23 |
| AU2003304212A1 (en) | 2005-01-04 |
| AU2003304212A8 (en) | 2005-01-04 |
| WO2004111568A3 (en) | 2005-07-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5485788A (en) | Combination explosive primer and electro-explosive device | |
| GB827120A (en) | Improvements in and relating to a percussion fuze | |
| US9562755B2 (en) | Safe and arm mechanisms and methods for explosive devices | |
| KR102644113B1 (en) | High explosive firing mechanism | |
| US7216589B2 (en) | Fuse for projected ordnance | |
| US5092243A (en) | Propellant pressure-initiated piezoelectric power supply for an impact-delay projectile base-mounted fuze assembly | |
| US5040463A (en) | Pressure activated power supply | |
| US3490373A (en) | Self-destructing rocket propelled grenade | |
| US2728296A (en) | Instantaneous detonator for hollow charge projectiles | |
| US2457839A (en) | Rocket | |
| US7430964B1 (en) | Safe and arm device and method of using the same | |
| US4099465A (en) | Ignition device for missile motors | |
| US20060124018A1 (en) | Explosive-activated safe-arm device | |
| EP1210563B1 (en) | Detonator | |
| US5591935A (en) | Shock sensing dual mode warhead | |
| US4047484A (en) | Fuze with bimetallic spring delay module | |
| US4244386A (en) | Valve having pyrotechnic separation device | |
| US3107618A (en) | De-arming device | |
| US3641938A (en) | Percussion or vibration fuse for explosive charge | |
| US3962974A (en) | Pressure-armed ordnance fuze | |
| US6131516A (en) | Air-safed underwater fuze system for launched munitions | |
| US4938141A (en) | Shock initiator device for initiating a percussion primer | |
| US3177810A (en) | Impact fuze | |
| US3707912A (en) | Mechanical fuze with self-destruct mechanism | |
| US5524543A (en) | Safety priming system for an explosive charge |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY, CONNE Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GRAHAM, JOHN A.;MALLERY, CARL F.;KEZERIAN, JEFFREY M.;AND OTHERS;REEL/FRAME:017531/0106;SIGNING DATES FROM 20050623 TO 20050801 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |