US1758170A - Parachute container - Google Patents
Parachute container Download PDFInfo
- Publication number
- US1758170A US1758170A US385819A US38581929A US1758170A US 1758170 A US1758170 A US 1758170A US 385819 A US385819 A US 385819A US 38581929 A US38581929 A US 38581929A US 1758170 A US1758170 A US 1758170A
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- Prior art keywords
- casing
- parachute
- container
- lid
- members
- 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.)
- Expired - Lifetime
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- 239000000463 material Substances 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000007799 cork Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000000994 depressogenic effect Effects 0.000 description 1
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012729 immediate-release (IR) formulation Substances 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
Definitions
- This invention relates to a parachute container, and it is an object of the invention to provide a device of this kind which is especially adapted for use in connection with an aeroplane and which serves to effectively house the parachute when not in use, yet readily permitting said parachute to become effective when desired.
- Another object. of the invention is to provide a container of this kind which is supported for swinging movement in a vertical i direction and which is normally in substan ⁇ tially a horizontal position, together with closure members or lids associated with the opposite ends of the body of the container whereby the parachute housed within the container is effectively protected against outside elements.
- a further object of the invention is to provide a device of this kind wherein the ends of the body of the container are closed by members or lids which automatically assume an open position, together with a releasable means for maintaining said lids in closed 0- sition, said lids when released automaticalll moving into open position so that substantia ly' instantaneous release will be effected of the parachute housed within the container.
- a container of this kind which is provided with an interior casin' suitably spaced from the peripheral wall o the body of the container to provide a chamber in which the major portion of the parachute is adapted to be received, said inside casing being open from end to end and affording effective means to assurea substantially immediate release of the parachute when desired;
- the invention consists in the details of construction and in the combination and arrangement ofthe several parts of my improved parachute container whereby certain important advantages are attained and the device rendered simpler, less expensive and otherwise more convenient and advantageous for use, as will be hereinafter more fully set forth.
- Figure 1 is a view partly in section and partly in elevation of a parachute container constructed in accordance with an embodiment of my invention
- Figure 2 is a sectional view taken substantially on the line 2-2 of Figure 1 looking in the direction of the arrow;
- Figure 3 is a fragmentary sectional view taken substantially on the same line as Figure 2 but looking in the opposite direction;
- Figure 4 is a view in elevation of my container in release position and with the parachute extended or projected;
- Figure 5 is a view in plan of one of the paper washers as herein disclosed.
- Figure 6 is a. fragmentary view partly in elevation and partly in section particularly illustrating the means for holding one of the lidy members normally closed;
- Figure 7 is a fragmentar detailed view partly in elevation and part y i.; section illustrating an anti-friction means for one of the release rods as herein employed;
- Figure 8 is a fragmentary view partly in section and partly in elevation of one of the mountings for the outer casing
- Figure 9 is a fragmentary view partly in 80 front elevation arid artl in section of the structure illustrated 1h F lgure 8.
- C denotes an outer casing of desired dimensions and which has its open end de- 35 fined b an outstanding flange 1 to which is secure by an adhesive or otherwise as may be preferred a gasketl 2 of cork or other suitable material with which is adapted to have direct contact a marginal portion of the lid 9 member L for the forward end of the casing C.
- the marginal portion of this lid member L is defined by a flange 3 which, when the lid member L 1s closed as illustrated in Fig-' ure 1, surrounds the liange 1 of the casing C 95 and thus provides effective means to prevent water, dust or the like from having ingress within the casing C through the front end thereof when the lid member L is closed.
- the opposite or rear end portion of the casing C 10 is defined by an angular flange 4 providing a seat for a gasket 5 which also may be of oo rk or other desired material and which is maintained in applied position by an adhesive or otherwise as may be preferred.
- the marginal portion of the lid member M for said rear end of the casing C has direct contact with this gasket 5 when infull closed position.
- Each of the lid members L and M is connected to the adjacent end portion of the casing C by a hinge 6 of a conventional spring type which operates to constantly urge the lid member L or M into full open position and which also operates to provide automatic' means for moving said member L or M into fullopen position upon release from closed position.
- Each of the lid members L and M carries an outstanding headed lug or male member 7 which, when said lid member is in full open position, is received within an expansible socket or female member 8, thus providing additional means for effectively maintaining the lid member L or M in desired full open position.
- the socket or female members 8 are preferably placed exteriorly of the casing C at the top thereof.
- each of the rods 10 carries a block or arm 15 xed thereto.
- each of the blocks or arms 15 is provided with a groove 16 which, upon requisite rocking movelnent of the head or arm 15, is adapted to receive therein a portion of the flange 1 or 4 of the casing C and the adjacent peripheral portion of the lid member L or M whereby said lid member will be effectively locked in full closed position, yet readily released upon suflicient swinging movement of the block or arm 15 in a direction away from the casingC.
- Each of the rods 10 and its associated bracket or lug 9 has operatively engaged therewith a coil spring 17 of requisite tension which serves to constantly urge the rod 10 in a direction to ⁇ maintain the block or arm Y15 in from the lower portion of the locking position.
- the spring 17 encircles a portion of the rod 10 and has one end secured to the bracket or lug 9 and its opposite end portion anchored to the rod 10.
- the lapping connection 11 between the rods 10 and as further facilitated by the applied' sleeve 12 assures said rods 1() to have unitary rotation in the same general direction under the influence of the operating arm 18 fixed to one of the rods 10.
- the arm 18 may be operated in any desired manner but preferably through the instrumentalityof a flexible cable 18 or the like suitably secured to the arm 18 and leading Within the cockpit of an aeroplane for ready access by the aviator or other occupant of the pit.
- an inner casing A Arranged axially of the casing C is an inner casing A cylindrical in form and of a diameter less than the interior diameter of the casing C so that in the assembly of the casi'ngs C apd A an intervening space 19 is provided intwhich is adapted to be substantially housed a parachute P and the cords 20 associate therewith.
- One end f the casing A terminates in relatively close proximity to the forward end of the casing' C when infits normal horizontal position and said end portion of the casing A is defined by an outstanding flange 21, the periph ral portion of .which being in close contact ith lthe adjacent portion of the wall of th lcasing C.- Immediately adjacent to this Qflange21 the casings C and A are held one to the vother by the circumferentially spaced bolts 22 and each of said bolts 22 is surrounded by a spacing sleeve 23 snugly bridging the space between the adjacent end portions of the casin'gsC and A.
- These bolts 22, as herein disclosed, are four in number and are equidistantly spaced circumferentially of the casings .C and A.
- the opposite end portion-of the casing A terminates a material distance inwardly of the adjacent end of the casing C and said end edge of the casing A is beaded or otherwise rounded, as at 24, in order to minimize liability of injury to the cords 20 by contact with such edge.
- each of the trunnions 25 constitutes a member having opposed faces flat and' normally.
- each of the trunnions 25 is received within the enlarged or circular portion 26 of a buttonhole slot provided in an upstanding bearing plate 27.
- the descriptive portion 28 of this slot is disposed downwardly and receives a trunnion 25 when the casing C is in a vertical position as illustrated ih Figure 4 and the parachute extended or projected.
- a suitable anti-friction medium 29, as illustrated in detail Figure 9, to facilitate the desired swinging movement of the casing C from its normal horizontal position to an upright or vertical position. Then the casing C is in its normal horizontal position the flat faces of each of the trunnions 25 are similarly arranged or, in other words, the flat faces of each of the trunnions 25 are disposed in parallelism with the longitudinal ends of the casing C.
- the bearing plates 27 are suitably affixed to the. upper portions of the side frames30.
- These frames 30 are'arranged side by side in desired spaced relation and are suitably anchored upon the upper portion of a wing W of the aeroplane, or otherwise as the requirements of practice may prefer.
- the upper portions of these frames 30 are provided with rearwardly disposed elongated arms 31, the outer end portions of which being connected by a' saddle 32 upon which rests the rear portion of the casing C when in its normal horizontal position and which saddle serves to prevent the casing C fronr swinging downwardly below such normal position.
- the central part of the saddle 32 has a depressed portion 33 which carries an upstanding spring socket or femalemember 34 to receive the headed or male member 35 carried by the under part of the rear portion of the/casing C and thus provide means for effectively holding the casing C in its normal position and also effectively' holds the casing C against being jolted or other undue or unnecessary vibration especially when the aeroplane is in motion.
- the outer end portions of the cords 20 of the parachute P are connected to a ring member 36 or the like and to which is also attached an end portion of a cable 38.
- the opposite end portion of the cable 3S is anchored, as at 39, to a desired point on the aeroplane and this cable enters my improved container through the forward open end of the inner casing A.
- the opposed portions of the lid member L and the adjacent end of the casing C are so formed astocompensatefor the cable 38 when the lid member M is in full closed position.
- surplus portion of the cable 38 is coiled around the winding arms 40 suitably positioned within the forward end of the casing A and anchored to the flange 21 of said casing. These arms 40 permit the cablato readily unwind therefrom as the parachute leaves the container.
- the parachute cords 20 ontheloadingofthe parachute within the container extend from the member 36 over the rear edge of the casing A and then forwardly of the space 19 to a point closely adjacent the forward end of the casing A.
- the remaining portions of the cords are returned but in folded relation as indicated in Figure 1, and interposed between adjacent folds of the cords 20 are the paper washers 41.
- These washers 41 are preferably made in two pieces with their extremities provided with suitable interlocking means, as at 42, for maintaining said sections in desired assembled relation.
- the parachute proper has its marginal portions forced Within the space 19 with the central portion of the chute stretched over the inside or rear end of the casing A- as illustrated in Figure 1.
- each of the brackets 9 is provided with suitable antifriction means, as at 43, to facilitate the desired rotation or rocking movement of the associated rod 10.
- a parachute container comprising an elongated casing having its ends open, lid members for the open ends of the easing ⁇ means for automatically moving said lid members into fully open position, releasablc means for holding the lid members in closed position, said casing being adapted to house a parachute, means for supporting the casing for swinging movement in a vertical direction, and means for maintaining said easing in a substantially horizontal position.
- a parachute container comprising an elongated casing having its ends open, lid members for the open ends of the casing, means for automatically moving said lid members into fully open position, releasable means for holding the lid members in closed position, a second casing support-ed within the first named casing and extending lengthwise thereof, said second casing being opeii at both ends, said second casing being spaced from the first casing. a parachute being housed within the first casing in the space between the two casings with a portion of the parachute overlying an end of the second casing.
- a parachute container comprising an elongated casing having its ends open, lid members for the open ends of the casing, means for automatically moving said lid members into fully open position, releasable means for holding the lid members in closed position, said casing being adapted to house a parachute ⁇ means for supporting the casing for swinging movement in a vertical direction, means for maintaining said casing in a substantially horizontal position, and means effective when the casing is in a vertical position to hold said casing against swinging movement.
- a parachute container comprising an elongated casing having its ends open and an outstanding flange on each end, hinged lid members for the open ends of the easing, means for automatically moving said lid members into fully open position, and releasable means for holding the lid members in being adapted to house a parachute, said releasable means comprising a pair of pivoted slotted arms i'eleasably engaging the outstanding flange of the casing and the outer edge of said lid members.
- rA ...1t tu.. o. paiac iu e con ainci comprising an elongated ea sing having its ends open.
- hinged lid members for the open ends of the casing, said lid means for automatically moving members into fully open position, releasable means for holding ⁇ the lid members in closed position, said casing being adapted to house a parachute, and coacting means carried by the casing and the lid members for holding said lid members in fully open position, said releasablc means comprising a pair of pivoted slotted arms releasably engaging the ends of the casing and the outer edge of said lid members.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Closures For Containers (AREA)
Description
May 13, 1930. H. E. PARKER. sR 1,758,170
PARACHUTE CONTA INER H E, pare/3 5f:
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May 13, 1930. H. E. PARKER, sR 1,758,170
PARACHUTE CONTAINER Filed Aug. 14. 1929 2 Sheets-Sheet 2 grvvcnhw /f I l Patented May 13, 1930 UNITED STATES PATENT OFFICEy HARRY EDGERTON PARKER, SIL, 0F SAN DIEGO, CALIFORNIA PARACHUTE CONTAINER i Application led August 14, 1929.l Serial No. 385,819.
This invention relates to a parachute container, and it is an object of the invention to provide a device of this kind which is especially adapted for use in connection with an aeroplane and which serves to effectively house the parachute when not in use, yet readily permitting said parachute to become effective when desired.
Another object. of the invention is to provide a container of this kind which is supported for swinging movement in a vertical i direction and which is normally in substan` tially a horizontal position, together with closure members or lids associated with the opposite ends of the body of the container whereby the parachute housed within the container is effectively protected against outside elements.
A further object of the invention is to provide a device of this kind wherein the ends of the body of the container are closed by members or lids which automatically assume an open position, together with a releasable means for maintaining said lids in closed 0- sition, said lids when released automaticalll moving into open position so that substantia ly' instantaneous release will be effected of the parachute housed within the container.
Furthermore, it is an object of the invention to provide a container of this kind which is provided with an interior casin' suitably spaced from the peripheral wall o the body of the container to provide a chamber in which the major portion of the parachute is adapted to be received, said inside casing being open from end to end and affording effective means to assurea substantially immediate release of the parachute when desired;
The invention consists in the details of construction and in the combination and arrangement ofthe several parts of my improved parachute container whereby certain important advantages are attained and the device rendered simpler, less expensive and otherwise more convenient and advantageous for use, as will be hereinafter more fully set forth.
The novel features of my invention will hereinafter be definitely claimed.
In order that my invention may be t-he better understood, I will now proceed to describe the same with reference to the accompanying drawings, wherein Figure 1 is a view partly in section and partly in elevation of a parachute container constructed in accordance with an embodiment of my invention;
Figure 2 is a sectional view taken substantially on the line 2-2 of Figure 1 looking in the direction of the arrow;
Figure 3 is a fragmentary sectional view taken substantially on the same line as Figure 2 but looking in the opposite direction;
Figure 4 is a view in elevation of my container in release position and with the parachute extended or projected;
Figure 5 is a view in plan of one of the paper washers as herein disclosed;
Figure 6 is a. fragmentary view partly in elevation and partly in section particularly illustrating the means for holding one of the lidy members normally closed;
Figure 7 is a fragmentar detailed view partly in elevation and part y i.; section illustrating an anti-friction means for one of the release rods as herein employed;
Figure 8 is a fragmentary view partly in section and partly in elevation of one of the mountings for the outer casing;
Figure 9 is a fragmentary view partly in 80 front elevation arid artl in section of the structure illustrated 1h F lgure 8.
As disclosed in the accompanying drawings, C denotes an outer casing of desired dimensions and which has its open end de- 35 fined b an outstanding flange 1 to which is secure by an adhesive or otherwise as may be preferred a gasketl 2 of cork or other suitable material with which is adapted to have direct contact a marginal portion of the lid 9 member L for the forward end of the casing C. The marginal portion of this lid member L is defined by a flange 3 which, when the lid member L 1s closed as illustrated in Fig-' ure 1, surrounds the liange 1 of the casing C 95 and thus provides effective means to prevent water, dust or the like from having ingress within the casing C through the front end thereof when the lid member L is closed. The opposite or rear end portion of the casing C 10 is defined by an angular flange 4 providing a seat for a gasket 5 which also may be of oo rk or other desired material and which is maintained in applied position by an adhesive or otherwise as may be preferred. The marginal portion of the lid member M for said rear end of the casing C has direct contact with this gasket 5 when infull closed position.
Each of the lid members L and M is connected to the adjacent end portion of the casing C by a hinge 6 of a conventional spring type which operates to constantly urge the lid member L or M into full open position and which also operates to provide automatic' means for moving said member L or M into fullopen position upon release from closed position.
Each of the lid members L and M carries an outstanding headed lug or male member 7 which, when said lid member is in full open position, is received within an expansible socket or female member 8, thus providing additional means for effectively maintaining the lid member L or M in desired full open position.
The socket or female members 8 are preferably placed exteriorly of the casing C at the top thereof.
Depending casing C adjacent to opposite ends thereof are the brackets or lugs 9 providing mountings for the rods 10. The adjacent or inner ends of the rods 10 are stepped, as at 11, so that they can be readily brought into lapping relation and snugly surrounding said adjacent end. portions of the rods 10, and more particularly the lapping portions thereof, is a sleeve 12 held in applied position by the cotter pins 14 or their equivalent, said pins as herein disclosed being disposed through the opposite end portions of the sleeve 12 vand the adjacent portions of the rods 10. The `two rods 10 are coupled in order to facilitate thel desired application or removal thereof with respect to the brackets or lugs 9. The outer end portion of each of the rods 10 carries a block or arm 15 xed thereto. l
The outer portion of each of the blocks or arms 15 is provided with a groove 16 which, upon requisite rocking movelnent of the head or arm 15, is adapted to receive therein a portion of the flange 1 or 4 of the casing C and the adjacent peripheral portion of the lid member L or M whereby said lid member will be effectively locked in full closed position, yet readily released upon suflicient swinging movement of the block or arm 15 in a direction away from the casingC. Each of the rods 10 and its associated bracket or lug 9 has operatively engaged therewith a coil spring 17 of requisite tension which serves to constantly urge the rod 10 in a direction to` maintain the block or arm Y15 in from the lower portion of the locking position. As herein disclosed, the spring 17 encircles a portion of the rod 10 and has one end secured to the bracket or lug 9 and its opposite end portion anchored to the rod 10.
The lapping connection 11 between the rods 10 and as further facilitated by the applied' sleeve 12 assures said rods 1() to have unitary rotation in the same general direction under the influence of the operating arm 18 fixed to one of the rods 10. The arm 18 may be operated in any desired manner but preferably through the instrumentalityof a flexible cable 18 or the like suitably secured to the arm 18 and leading Within the cockpit of an aeroplane for ready access by the aviator or other occupant of the pit.
Arranged axially of the casing C is an inner casing A cylindrical in form and of a diameter less than the interior diameter of the casing C so that in the assembly of the casi'ngs C apd A an intervening space 19 is provided intwhich is adapted to be substantially housed a parachute P and the cords 20 associate therewith.
One end f the casing A terminates in relatively close proximity to the forward end of the casing' C when infits normal horizontal position and said end portion of the casing A is defined by an outstanding flange 21, the periph ral portion of .which being in close contact ith lthe adjacent portion of the wall of th lcasing C.- Immediately adjacent to this Qflange21 the casings C and A are held one to the vother by the circumferentially spaced bolts 22 and each of said bolts 22 is surrounded by a spacing sleeve 23 snugly bridging the space between the adjacent end portions of the casin'gsC and A. These bolts 22, as herein disclosed, are four in number and are equidistantly spaced circumferentially of the casings .C and A.
The opposite end portion-of the casing A terminates a material distance inwardly of the adjacent end of the casing C and said end edge of the casing A is beaded or otherwise rounded, as at 24, in order to minimize liability of injury to the cords 20 by contact with such edge.
The sides of the casing C are provided with the diametrically opposed outstanding trunnions 25 suitably anchored to the wall of the casing C. vThese trunnions 25 are spaced from the forward end of the casing C a distance equal to approximately one-third of the length of such casing C. As illustrated in detail Figure 9, each of the trunnions 25 constitutes a member having opposed faces flat and' normally. each of the trunnions 25 is received within the enlarged or circular portion 26 of a buttonhole slot provided in an upstanding bearing plate 27. The descriptive portion 28 of this slot is disposed downwardly and receives a trunnion 25 when the casing C is in a vertical position as illustrated ih Figure 4 and the parachute extended or projected. Associated' with the enlarged opening 26 in each of the slots is a suitable anti-friction medium 29, as illustrated in detail Figure 9, to facilitate the desired swinging movement of the casing C from its normal horizontal position to an upright or vertical position. Then the casing C is in its normal horizontal position the flat faces of each of the trunnions 25 are similarly arranged or, in other words, the flat faces of each of the trunnions 25 are disposed in parallelism with the longitudinal ends of the casing C.
The bearing plates 27 are suitably affixed to the. upper portions of the side frames30. These frames 30 are'arranged side by side in desired spaced relation and are suitably anchored upon the upper portion of a wing W of the aeroplane, or otherwise as the requirements of practice may prefer. The upper portions of these frames 30 are provided with rearwardly disposed elongated arms 31, the outer end portions of which being connected by a' saddle 32 upon which rests the rear portion of the casing C when in its normal horizontal position and which saddle serves to prevent the casing C fronr swinging downwardly below such normal position. The central part of the saddle 32 has a depressed portion 33 which carries an upstanding spring socket or femalemember 34 to receive the headed or male member 35 carried by the under part of the rear portion of the/casing C and thus provide means for effectively holding the casing C in its normal position and also effectively' holds the casing C against being jolted or other undue or unnecessary vibration especially when the aeroplane is in motion.
In practice I tind it of advantage to have one of my improved containers arranged on the end of each wing and one on the tail of the fuselage.
As each of the devices is of a similar structure it is believed that the detailed description and illustration of one is sufficient for the purposes of disclosure especially in view of the fact that the devices may be otherwise arranged if preferred.
The outer end portions of the cords 20 of the parachute P are connected to a ring member 36 or the like and to which is also attached an end portion of a cable 38. The opposite end portion of the cable 3S is anchored, as at 39, to a desired point on the aeroplane and this cable enters my improved container through the forward open end of the inner casing A. The opposed portions of the lid member L and the adjacent end of the casing C are so formed astocompensatefor the cable 38 when the lid member M is in full closed position. In loading my improved container surplus portion of the cable 38 is coiled around the winding arms 40 suitably positioned within the forward end of the casing A and anchored to the flange 21 of said casing. These arms 40 permit the cablato readily unwind therefrom as the parachute leaves the container.
The parachute cords 20 ontheloadingofthe parachute within the container extend from the member 36 over the rear edge of the casing A and then forwardly of the space 19 to a point closely adjacent the forward end of the casing A. The remaining portions of the cords are returned but in folded relation as indicated in Figure 1, and interposed between adjacent folds of the cords 20 are the paper washers 41. These washers 41 are preferably made in two pieces with their extremities provided with suitable interlocking means, as at 42, for maintaining said sections in desired assembled relation.
The parachute proper has its marginal portions forced Within the space 19 with the central portion of the chute stretched over the inside or rear end of the casing A- as illustrated in Figure 1. By this manner of loading it is assured that the inside or rear portion of the casing A is in most elfective position with respect to the loaded parachute to assure the desired release of the parachute for instant inflation. As the parachute moves out from within the space 19 the paper washers 41 hereinbefore referred to will readily fall ofi' and fly free of everything. When the occasion requires the use of the parachute P it is only necessary to impart requisite pull on the arm 18 whereu on the lid members L and M will be released). U on release of these members L and M they will instantaneously swing automatically into full open position and in view of the normal horizontal position of the casing C just immediately upon such opening movement, air will enter within thek casing A through the forward end thereof with resultant force to carry the loaded or folded parachute out of the container but in a manner to effect an inflation of the parachute P as it leaves the container. Vhen the parachute is in full free position, as illustrated in Figure 4, the same will offer resistance direct to the plane through the cable 38 without any hindrance or obstruction being offered by the container itself. As the container swings upwardly and when it reaches substantially a vertical, position it will drop down a distance as afforded by the restricted portions 28 of the slots in the bearing plates 27 and thus assure the maintenance of the container in the vertical position as illustrated in Figure 4.
As illustrated in detail Figure 7, each of the brackets 9 is provided with suitable antifriction means, as at 43, to facilitate the desired rotation or rocking movement of the associated rod 10.
From the foregoing description it is llO ' closed positionsaid casing thought to be obvious that a parachute container constructed in accordance with my iiiveiition is particularly well adapted for use by reason of the convenience and facility with which it may be assembled and operated, and it will also be obvious that my invention is susceptible of some change and modification without departing from the principles and spirit thereof and for this reason l do not wish to be understood as limiting myself to the precise arrangement and formation of the several parts herein shown in carrying out my invention in practice except as hereinafter claimed.
I claim l l. A parachute container comprising an elongated casing having its ends open, lid members for the open ends of the easing` means for automatically moving said lid members into fully open position, releasablc means for holding the lid members in closed position, said casing being adapted to house a parachute, means for supporting the casing for swinging movement in a vertical direction, and means for maintaining said easing in a substantially horizontal position.
2. A parachute container comprising an elongated casing having its ends open, lid members for the open ends of the casing, means for automatically moving said lid members into fully open position, releasable means for holding the lid members in closed position, a second casing support-ed within the first named casing and extending lengthwise thereof, said second casing being opeii at both ends, said second casing being spaced from the first casing. a parachute being housed within the first casing in the space between the two casings with a portion of the parachute overlying an end of the second casing.
3. A parachute container comprising an elongated casing having its ends open, lid members for the open ends of the casing, means for automatically moving said lid members into fully open position, releasable means for holding the lid members in closed position, said casing being adapted to house a parachute` means for supporting the casing for swinging movement in a vertical direction, means for maintaining said casing in a substantially horizontal position, and means effective when the casing is in a vertical position to hold said casing against swinging movement.
4. A parachute container comprising an elongated casing having its ends open and an outstanding flange on each end, hinged lid members for the open ends of the easing, means for automatically moving said lid members into fully open position, and releasable means for holding the lid members in being adapted to house a parachute, said releasable means comprising a pair of pivoted slotted arms i'eleasably engaging the outstanding flange of the casing and the outer edge of said lid members.
rA ...1t tu.. o. paiac iu e con ainci comprising an elongated ea sing having its ends open. hinged lid members for the open ends of the casing, said lid means for automatically moving members into fully open position, releasable means for holding` the lid members in closed position, said casing being adapted to house a parachute, and coacting means carried by the casing and the lid members for holding said lid members in fully open position, said releasablc means comprising a pair of pivoted slotted arms releasably engaging the ends of the casing and the outer edge of said lid members.
In testimony whereof l hereunto aliX my signature.
HARRY E. PARKER, SR.
Cil
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US385819A US1758170A (en) | 1929-08-14 | 1929-08-14 | Parachute container |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US385819A US1758170A (en) | 1929-08-14 | 1929-08-14 | Parachute container |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1758170A true US1758170A (en) | 1930-05-13 |
Family
ID=23523002
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US385819A Expired - Lifetime US1758170A (en) | 1929-08-14 | 1929-08-14 | Parachute container |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1758170A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2470120A (en) * | 1943-05-06 | 1949-05-17 | Walker Brooks | Method of bombing from fast moving planes |
| US2972457A (en) * | 1957-04-26 | 1961-02-21 | Steinthal & Co Inc M | Retractable parachute system for aircraft and pilot chute ejecting mechanism |
-
1929
- 1929-08-14 US US385819A patent/US1758170A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2470120A (en) * | 1943-05-06 | 1949-05-17 | Walker Brooks | Method of bombing from fast moving planes |
| US2972457A (en) * | 1957-04-26 | 1961-02-21 | Steinthal & Co Inc M | Retractable parachute system for aircraft and pilot chute ejecting mechanism |
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