[go: up one dir, main page]

US2435980A - Tow target exchange device - Google Patents

Tow target exchange device Download PDF

Info

Publication number
US2435980A
US2435980A US560295A US56029544A US2435980A US 2435980 A US2435980 A US 2435980A US 560295 A US560295 A US 560295A US 56029544 A US56029544 A US 56029544A US 2435980 A US2435980 A US 2435980A
Authority
US
United States
Prior art keywords
exchange device
tow
tow line
target
nose piece
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
Application number
US560295A
Inventor
Marvin L Pyle
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US560295A priority Critical patent/US2435980A/en
Application granted granted Critical
Publication of US2435980A publication Critical patent/US2435980A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00Moving targets, i.e. moving when fired at
    • F41J9/08Airborne targets, e.g. drones, kites, balloons
    • F41J9/10Airborne targets, e.g. drones, kites, balloons towed

Definitions

  • This invention relates to aerial tow targets and more particularly to devices for exchanging targets at the end of a tow line while an airplane is in flight.
  • the usual tow target exchange device comprises a mechanism adapted to be towed by an airplane at the end of a tow line, the mechanism being adapted to releasably secure an air lled sleeve after it has been hit by anti-aircraft fire and substitute a new sleeve therefor, as described in the United States Patent to Foulk N0. 1,971,340 granted August 28, 1934.
  • the new sleeve is attached to the tow line at the airplane end thereof by means of a, slip ring adapted to slidably encompass the line, the sleeve then being slid along the tow line to the exchange device by virtue of the forward flight of the plane.
  • one of the drawbacks of present target exchange devices resides in the fact that at the point of attachment between the tow line and the exchange device a certain amount of angularity exists .between the tow line and the forward portion of the device due to swerving of the airplane and changing wind conditions acting on the tow line and the target.
  • the principal object of my invention is to overcome this diculty and, accordingly, I provide a target exchange device comprising a universal joint incorporated therein between the front portion thereof, l. e., the nose piece, which is attached to the tow line, and the detent mechanism.
  • Such a structure provides for a substantially straight path between the tow line and the nose piece of the exchange device so that the slip ring has substantially passed beyond the tow line before it can bring any shock force to bear, the shock force 2 then being taken by the body of the device which is substantially stronger in shear than the tow line and unlikely to be cut by the slip ring.
  • Fig. 1 illustrates a conventional tow target exchange device for the purpose of clearly demonstrating the distinction in operation between my invention and prior device;
  • Fig. 2 illustrates a general view of the improved tow target exchange device
  • Fig. 3 illustrates the invention in operation.
  • a tow target exchange device having a body comprising a nose piece I adapted to be attached to a tow line (not shown) and articulated to an elongated housing element of a detent mechanism, generally indicated by A, through a conventional universal ball and socket joint structure comprising a ball 3 and the universally movable sockets or retaining members 5 and 6 secured to nose piece I and the mechanism portion of the body, respectively, the said articulated body being of substantially cylindrical shape to permit unobstructed passage of an exchange target from the nose piece and over the ball and socket joint to the detent mechanism of the housing element when the nose piece and the housing element are aligned.
  • the detent mechanism is of conventional form and comprises a trigger 8 cooperating with a catch or detent lever 9 and a leaf spring iIl.
  • the structure and the operation of the mechanism is substantially the same as that described in the aforementioned United States Patent to Foulk No, 1,971,340, the operation being dependent upon engagement of a slip ring Il of a new target sleeve (not shown) with the trigger 8 therebyA actuating the lever 9 against the bias of spring I0, the hook I2 on lever ⁇ 9 releasing the slip ring I3 of the hit target sleeve (not shown) which is carried off by the air current and drops to the ground.
  • a tow line I5 being attached to nose piece I and being pulled in the -direction of the arrow, the tow line I5 assumes a substantially straight line with respect to the nose piece I due to the universal joint provided between the nose piece I and the detent mechanism A. Accordingly, a slip ring I'I of a substitute target sleeve I8 will have substantially a straightpath in passing from the tow line I5 to and over the nose piece I, the shock due to angularity between the tow line and the release mechanism A being taken along the body of the 3 device, and loss of the device due to cutting of the tow line being thereby eliminated.
  • a tow target exchange device comprising a body including a nose piece adapted to be attached to a tow line and an elongated housing element having therein a. detent mechanism adapted to releasably secure a tow target. and a universal joint comprising a retaining member secured to said nose piece and a second retaining member secured to said housing element and a spherical member retained between said retaining members whereby said body is pivotally articulated intermediate said nose piece and said housing element for the purpose of providing a straight path for movement of an exchange target between said tow line and said nose piece, said body being of substantially cylindrical shape to permit unobstructed passage of the exchange target from the nose piece to the detent mechanism of the housing element when said nose piece and housing element are aligned.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Joints Allowing Movement (AREA)

Description

Feb. 17, 1948. M PYLE TOW TRGT EXCHANGE DEVICE Filed OCT.. 25, 1944 INVENTOR. /VQI//N /DVLE Patented Feb. 17,1948 'il Y.
UNITED STATES 'row TARGET E'XCHANGEl DEvIcE Marvin L. Pyle, Los Angeles; 'Califf Application octet-er 251944', serialfNof.: 561x295" Y 1 cina; (cine- 1055351 (Granted under nie-- act of Maren 3; lists-ias amended April 30, 1928; 370 0. G. 757) The invention described herein may be manufactured and used by or for Government for governmental purposes, without the payment to me of any royalty thereon.
This invention relates to aerial tow targets and more particularly to devices for exchanging targets at the end of a tow line while an airplane is in flight.
The usual tow target exchange device comprises a mechanism adapted to be towed by an airplane at the end of a tow line, the mechanism being adapted to releasably secure an air lled sleeve after it has been hit by anti-aircraft fire and substitute a new sleeve therefor, as described in the United States Patent to Foulk N0. 1,971,340 granted August 28, 1934. The new sleeve is attached to the tow line at the airplane end thereof by means of a, slip ring adapted to slidably encompass the line, the sleeve then being slid along the tow line to the exchange device by virtue of the forward flight of the plane. Upon the arrival of the slip ring at the end of the tow line it engages the exchange device, actuating a detent mechanism therein to release the hit target sleeve which is thus dropped to the ground, the new target sleeve then moving into position whereat the slip ring thereof is arrested by the detent mechanism, and is in position to be iired upon. As illustrated in Fig. 1 of the drawing, one of the drawbacks of present target exchange devices resides in the fact that at the point of attachment between the tow line and the exchange device a certain amount of angularity exists .between the tow line and the forward portion of the device due to swerving of the airplane and changing wind conditions acting on the tow line and the target. As a result of this angular relation the slip ring of the new target sleeve cannot slide smoothly from the tow line to the exchange device and at the point of attachment therebetween, which is the vertex of the angle, the slip ring brings a shock force to bear which is at times sufficient to cut the tow line at this point, the exchange mechanism and the sleeve being thus lost. The principal object of my invention is to overcome this diculty and, accordingly, I provide a target exchange device comprising a universal joint incorporated therein between the front portion thereof, l. e., the nose piece, which is attached to the tow line, and the detent mechanism. Such a structure provides for a substantially straight path between the tow line and the nose piece of the exchange device so that the slip ring has substantially passed beyond the tow line before it can bring any shock force to bear, the shock force 2 then being taken by the body of the device which is substantially stronger in shear than the tow line and unlikely to be cut by the slip ring.
A detailed disclosure of my invention now follows with reference to the appended drawing in which:
Fig. 1 illustrates a conventional tow target exchange device for the purpose of clearly demonstrating the distinction in operation between my invention and prior device;
Fig. 2 illustrates a general view of the improved tow target exchange device; and
Fig. 3 illustrates the invention in operation.
With reference to Fig. 2, there is disclosed a tow target exchange device having a body comprising a nose piece I adapted to be attached to a tow line (not shown) and articulated to an elongated housing element of a detent mechanism, generally indicated by A, through a conventional universal ball and socket joint structure comprising a ball 3 and the universally movable sockets or retaining members 5 and 6 secured to nose piece I and the mechanism portion of the body, respectively, the said articulated body being of substantially cylindrical shape to permit unobstructed passage of an exchange target from the nose piece and over the ball and socket joint to the detent mechanism of the housing element when the nose piece and the housing element are aligned. The detent mechanism is of conventional form and comprises a trigger 8 cooperating with a catch or detent lever 9 and a leaf spring iIl. The structure and the operation of the mechanism is substantially the same as that described in the aforementioned United States Patent to Foulk No, 1,971,340, the operation being dependent upon engagement of a slip ring Il of a new target sleeve (not shown) with the trigger 8 therebyA actuating the lever 9 against the bias of spring I0, the hook I2 on lever `9 releasing the slip ring I3 of the hit target sleeve (not shown) which is carried off by the air current and drops to the ground.
In flight, as shown in Fig. 3, a tow line I5 being attached to nose piece I and being pulled in the -direction of the arrow, the tow line I5 assumes a substantially straight line with respect to the nose piece I due to the universal joint provided between the nose piece I and the detent mechanism A. Accordingly, a slip ring I'I of a substitute target sleeve I8 will have substantially a straightpath in passing from the tow line I5 to and over the nose piece I, the shock due to angularity between the tow line and the release mechanism A being taken along the body of the 3 device, and loss of the device due to cutting of the tow line being thereby eliminated.
Having thus described my invention and the manner in which it overcomes disadvantages of prior constructions, I claim:
A tow target exchange device comprising a body including a nose piece adapted to be attached to a tow line and an elongated housing element having therein a. detent mechanism adapted to releasably secure a tow target. and a universal joint comprising a retaining member secured to said nose piece and a second retaining member secured to said housing element and a spherical member retained between said retaining members whereby said body is pivotally articulated intermediate said nose piece and said housing element for the purpose of providing a straight path for movement of an exchange target between said tow line and said nose piece, said body being of substantially cylindrical shape to permit unobstructed passage of the exchange target from the nose piece to the detent mechanism of the housing element when said nose piece and housing element are aligned.
MARVIN L. PYLE.
REFERENCES CITED The following references are of record in the ille of this patent: l
UNITED STATES PATENTS
US560295A 1944-10-25 1944-10-25 Tow target exchange device Expired - Lifetime US2435980A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US560295A US2435980A (en) 1944-10-25 1944-10-25 Tow target exchange device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US560295A US2435980A (en) 1944-10-25 1944-10-25 Tow target exchange device

Publications (1)

Publication Number Publication Date
US2435980A true US2435980A (en) 1948-02-17

Family

ID=24237173

Family Applications (1)

Application Number Title Priority Date Filing Date
US560295A Expired - Lifetime US2435980A (en) 1944-10-25 1944-10-25 Tow target exchange device

Country Status (1)

Country Link
US (1) US2435980A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2604324A (en) * 1951-03-13 1952-07-22 Richard L Weir Positive tow target exchanger

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US45720A (en) * 1865-01-03 Improved attachment of trains of boats
US1319565A (en) * 1919-10-21 Anchorage fob towed bodies
US1971340A (en) * 1933-08-05 1934-08-28 Albert C Foulk Tow target releasing device
US2382854A (en) * 1944-01-22 1945-08-14 American Steel & Wire Co Airplane tow target release device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US45720A (en) * 1865-01-03 Improved attachment of trains of boats
US1319565A (en) * 1919-10-21 Anchorage fob towed bodies
US1971340A (en) * 1933-08-05 1934-08-28 Albert C Foulk Tow target releasing device
US2382854A (en) * 1944-01-22 1945-08-14 American Steel & Wire Co Airplane tow target release device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2604324A (en) * 1951-03-13 1952-07-22 Richard L Weir Positive tow target exchanger

Similar Documents

Publication Publication Date Title
US20140155202A1 (en) Automatic opening mechanical archery broadhead
US2924175A (en) Foldable fin arrangement for a projectile
US3387400A (en) Automatic safety device with manual release for bolt action firearms
US2435980A (en) Tow target exchange device
US3490799A (en) Aerial target coupling
US4524675A (en) Detachably connectable sight assembly for a small defense weapon
US2589227A (en) Trigger conversion device for rifles
GB721541A (en) Improvements in or relating to safety devices for apparatus containing substances capable of generating pressure by the combustion thereof
US3586332A (en) Time delay triggering unit
US1975809A (en) Fuse for projectiles
US1418606A (en) Aerial torpedo or drop bomb
US2307009A (en) Discharger for pyrotechnic cartridges
US3838532A (en) Multipurpose powerhead
US2777696A (en) Multi-purpose cable fitting
US2427371A (en) Fuse for land mines
US2310249A (en) Aerodynamic release drag for tow targets
US2486397A (en) Automatically self-releasing aircraft landing hook
US2345618A (en) Fuse
US3311376A (en) Off-set tow target
US3007411A (en) Projectile stabilizer
US2588167A (en) Striker for igniters
US2604324A (en) Positive tow target exchanger
US2567170A (en) Tow target cable attachment
US2426221A (en) Positive action release hook
US2492154A (en) Tow target exchange device