US2675198A - Shock absorbing coupler for parachutes - Google Patents

Shock absorbing coupler for parachutes Download PDF

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Publication number
US2675198A
US2675198A US241324A US24132451A US2675198A US 2675198 A US2675198 A US 2675198A US 241324 A US241324 A US 241324A US 24132451 A US24132451 A US 24132451A US 2675198 A US2675198 A US 2675198A
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cylinder
rod
sleeve
housing
parachutes
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US241324A
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Richard F Reihman
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    • 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
    • B64D17/22—Load suspension
    • B64D17/36—Load suspension incorporating friction devices or frangible connections to reduce shock loading of canopy

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  • This invention appertains to improvements in devices for retarding the opening of a parachute and controlling the speed of descent, the primary object of this invention being to provide a shock absorbing device and coupler, which is connectable between a jumper or load and a pilot chute, lthe coupler, when disengaged from the load or jumper, enabling the pilot chute to pull the ripcord on the main chute and thus open the main chute. y.
  • Another object of this invention is to provide means for eiecting a safe and rapid' discharge of material or, a parachutist from rapidly moving aircraft and to provide means for lessening the initial .shock of the opening of a parachute on the load or cna parachutist.
  • A'further object of this invention is to provide' a couplingV device, 'which will automatically uncouple itself after being subjected to a certain amount of strain and then having the imposition of strain relaxed.
  • Figure 1 is a longitudinal sectional view of a coupling device, constructed in accordance with the principles of this invention, and especially designed for connection between a load or parachutist and the pilot chute and rip-cord of the main chute;
  • Figure 2 is a transverse sectional View taken on line 2--2 of Figure 1;
  • Figure 3 is a transverse sectional view taken on line 3-3 of Figure 1;
  • Figure 4 is a longitudinal sectional view, with the parts moved to a subsequent position from the normal position of Figure 1, and,
  • Figure 5 is a longitudinal sectional View, similar to Figures 1 and 4, with the parts moved to their linal position in operation.
  • the coupling device I0 is especially designed for connection between a load or parachutist and the connecting cord I2 of a pilot chute (not shown) and the rip-cord I4 of the main chute (not shown).
  • the coupling device includes an elongated cylinder I 6, which forms a housing and has a closed end I8 through which an elliptical ring 20 is extended, the outer end of the ring receiving one end of the rip-cord I4 and one end of the cord I2.
  • the opposing end of the cylinder is opened and a cap 22 is aixed thereto by means of a peripheral iiange 24.
  • a center opening 26 is formed in the cap and a rod 28 is slidably disposed therethrough, the outer end of the rod terminating in an integral ring or eye 30, which is connected by means of a cord 32 to the harness on the load or parachutist.
  • An ⁇ inner cylinder having a thick wall, is slidably disposed within the cylinder I 6 and is formed with diametrically opposed radial openings 36 and 38, Within which spring loaded detents dal and 42 are housed.
  • the detents are adapted to lockingly engage in sockets 44 and 4B formed interiorly of the outer cylinder I6 and disposed in diametrically opposed relation.
  • a sleeve 48 is formed at one end with an end plate Eil, which encloses the end of the sleeve and extends laterally therefrom, the peripheral edges of ⁇ the plate being slightly spaced from the inner surface of the outer cylinder I6.
  • the sleeve 48 is axially movable Within the bore 52 of the cylinder 34, the plate being of a diameter equal to the diameter of the cylinder 34 and the end 54 of the cylinder being engageable on the under side of the plate, as seen in Figure 1.
  • the rod 28 is formed adjacent its inner end 56 with opposed grooves 58 and 6D, which are adapted to receive ball bearings 6.2 and 64, the balls being disposed in apertures 68 and I0 formed in the sleeve.
  • the ball bearings 62 and 64 are of a diameter slightly less than the depth of one of the grooves 58 or 6I) plus the thickness of the walls of the sleeve 48.
  • a spring l2 is coiled Within the outer cylinder I6 and is affixed at its inner end to a boss 14, which extends from the outer face of the plate 50.
  • the opposite end 'I6 of the spring is connected to the inner end of the ring 20 and the spring is of a size and tensioned to permit the inner cylinder and sleeve to move to the position, illustrated in Figure 4, before retracting the sleeve, after the inner cylinder is locked, as seen in Figure 5.
  • the coupling device is illustrated in its normal position in Figure 1 with the load or the parachutist being connected to the outer end 3B of the rod 28 and the cords I2 and I4 being connected to the outer end of the ring ZIB.
  • the pilot chute In operation, when the user of the parachute jumps from the aircraft, the pilot chute is opened and the initial shock of the opening of the pilot chute causes the cylinder and sleeve to move from the position in Figure 1 to the position in Figure 4, Where the spring loaded detents lockingly engage in the slots 44 and 46 formed in the outer cylinder, the spring 12 being tensioned by being distended.
  • the spring 12 will be operative to pull the sleeve 48 outwardly from the bore 52 and the inner cylinder, the balls 62 and 64 disengaging from the grooves 58 and 60 in the rod and, thereby uncoupling the rod v281fr'om the sleeve 48.
  • Therad 28 is thereby free to slide completely out -of the cylinder I6 from the end 22, permitting the pilot chute to effect a direct pull on the rip-cord H and open the main chute.
  • the ⁇ main chute is carried by the harness of the parachutst or load in a conventional pack and until the rod slides out from the housing, the housing and inner cylinder and sleeve are carried by the rod, v
  • the housing is pulled upwardly by the pilot chute and the connection between the pilot chute and the rip cord of the main chute is through the housing at the ring 20.
  • the coupling device can be effectively employed as a couplingrmeans in any type of linkage or a like assembly, where it is desired to Vautomatically have one member uncouple from another, subject to the imposition of a certain amount of strain on the member and the relaxation of the strain.
  • a shocl for use with a pilot chute and a main chute, a shocl; absorbing coupler comprising a housing, a rod slidably disposed through one end of the housing, said rod being adapted for attachment to a parachutist, the opposing end of the cylinder being connectable to the pilot chute and the rip cord for the main chute, means in said housing releasably locking said rod therein, said last means including a cylinder having a bore and being slidable in said housing, a member mounted in the bore of the cylinder for sliding movement, means limiting movement of the member in the direction of pull of the rod, balls carried by said member urged by the'i'nner wall of the cylinder int-o engagement in grooves formed -in the rod, means for locking the cylinder in the' housing vand means for sliding the member from the cylinder when the cylinder is locked so that the balls are disengaged "from the grooves and the rod is free to slide from the housing, said last-mentioned means

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Flexible Shafts (AREA)

Description

April 13, 1954 R. F. REIHMAN SHOCK ABSORBING COUPLER F'OR PARACHUTES Filed Aug. 1o, 1951 3 r 'ncHoTERs #fag/)veas Traum? Patented pr. 13, 1954 .aff
OFFICE SHOCK ABSORBING COUPLER FOR PARACHUTES Richard F. Reihman,V Coopersbux'g, Pa. Application August 1o, 1951, serial No. 241,324
3- Claims. 1
This invention appertains to improvements in devices for retarding the opening of a parachute and controlling the speed of descent, the primary object of this invention being to provide a shock absorbing device and coupler, which is connectable between a jumper or load and a pilot chute, lthe coupler, when disengaged from the load or jumper, enabling the pilot chute to pull the ripcord on the main chute and thus open the main chute. y.
Another object of this invention is to provide means for eiecting a safe and rapid' discharge of material or, a parachutist from rapidly moving aircraft and to provide means for lessening the initial .shock of the opening of a parachute on the load or cna parachutist.
A'further object of this invention is to provide' a couplingV device, 'which will automatically uncouple itself after being subjected to a certain amount of strain and then having the imposition of strain relaxed.
These and ancillary objects and structural features of merit are obtained by this invention, the preferred embodiment of which is set forth in the following description and illustrated in the accompanying drawing, wherein:
Figure 1 is a longitudinal sectional view of a coupling device, constructed in accordance with the principles of this invention, and especially designed for connection between a load or parachutist and the pilot chute and rip-cord of the main chute;
Figure 2 is a transverse sectional View taken on line 2--2 of Figure 1;
Figure 3 is a transverse sectional view taken on line 3-3 of Figure 1;
Figure 4 is a longitudinal sectional view, with the parts moved to a subsequent position from the normal position of Figure 1, and,
Figure 5 is a longitudinal sectional View, similar to Figures 1 and 4, with the parts moved to their linal position in operation.
Referring now more particularly to the accompanying drawing, the coupling device I0 is especially designed for connection between a load or parachutist and the connecting cord I2 of a pilot chute (not shown) and the rip-cord I4 of the main chute (not shown).
The coupling device includes an elongated cylinder I 6, which forms a housing and has a closed end I8 through which an elliptical ring 20 is extended, the outer end of the ring receiving one end of the rip-cord I4 and one end of the cord I2.
The opposing end of the cylinder is opened and a cap 22 is aixed thereto by means of a peripheral iiange 24. A center opening 26 is formed in the cap and a rod 28 is slidably disposed therethrough, the outer end of the rod terminating in an integral ring or eye 30, which is connected by means of a cord 32 to the harness on the load or parachutist.
An `inner cylinder, having a thick wall, is slidably disposed within the cylinder I 6 and is formed with diametrically opposed radial openings 36 and 38, Within which spring loaded detents dal and 42 are housed. The detents are adapted to lockingly engage in sockets 44 and 4B formed interiorly of the outer cylinder I6 and disposed in diametrically opposed relation.
A sleeve 48 is formed at one end with an end plate Eil, which encloses the end of the sleeve and extends laterally therefrom, the peripheral edges of` the plate being slightly spaced from the inner surface of the outer cylinder I6. The sleeve 48 is axially movable Within the bore 52 of the cylinder 34, the plate being of a diameter equal to the diameter of the cylinder 34 and the end 54 of the cylinder being engageable on the under side of the plate, as seen in Figure 1.
The rod 28 is formed adjacent its inner end 56 with opposed grooves 58 and 6D, which are adapted to receive ball bearings 6.2 and 64, the balls being disposed in apertures 68 and I0 formed in the sleeve. The ball bearings 62 and 64 are of a diameter slightly less than the depth of one of the grooves 58 or 6I) plus the thickness of the walls of the sleeve 48.
A spring l2 is coiled Within the outer cylinder I6 and is affixed at its inner end to a boss 14, which extends from the outer face of the plate 50. The opposite end 'I6 of the spring is connected to the inner end of the ring 20 and the spring is of a size and tensioned to permit the inner cylinder and sleeve to move to the position, illustrated in Figure 4, before retracting the sleeve, after the inner cylinder is locked, as seen in Figure 5.
The coupling device is illustrated in its normal position in Figure 1 with the load or the parachutist being connected to the outer end 3B of the rod 28 and the cords I2 and I4 being connected to the outer end of the ring ZIB.
In operation, when the user of the parachute jumps from the aircraft, the pilot chute is opened and the initial shock of the opening of the pilot chute causes the cylinder and sleeve to move from the position in Figure 1 to the position in Figure 4, Where the spring loaded detents lockingly engage in the slots 44 and 46 formed in the outer cylinder, the spring 12 being tensioned by being distended.
As the resistance between the parachutist and the pilot chute lessens, due to decreased velocity, the spring 12 will be operative to pull the sleeve 48 outwardly from the bore 52 and the inner cylinder, the balls 62 and 64 disengaging from the grooves 58 and 60 in the rod and, thereby uncoupling the rod v281fr'om the sleeve 48. Therad 28 is thereby free to slide completely out -of the cylinder I6 from the end 22, permitting the pilot chute to effect a direct pull on the rip-cord H and open the main chute. Of course, the `main chute is carried by the harness of the parachutst or load in a conventional pack and until the rod slides out from the housing, the housing and inner cylinder and sleeve are carried by the rod, v
which is connected directly "to the parachutist.
However, when the rod is disengaged, the housing is pulled upwardly by the pilot chute and the connection between the pilot chute and the rip cord of the main chute is through the housing at the ring 20.
While the device has been described and illusv 'trated in connection with the opening of a parachuteJ it is obvious that the coupling device can be effectively employed as a couplingrmeans in any type of linkage or a like assembly, where it is desired to Vautomatically have one member uncouple from another, subject to the imposition of a certain amount of strain on the member and the relaxation of the strain.
Having thus described this invention, what is claimed is:
1. For use with a pilot chute and a main chute, a shocl; absorbing coupler comprising a housing, a rod slidably disposed through one end of the housing, said rod being adapted for attachment to a parachutist, the opposing end of the cylinder being connectable to the pilot chute and the rip cord for the main chute, means in said housing releasably locking said rod therein, said last means including a cylinder having a bore and being slidable in said housing, a member mounted in the bore of the cylinder for sliding movement, means limiting movement of the member in the direction of pull of the rod, balls carried by said member urged by the'i'nner wall of the cylinder int-o engagement in grooves formed -in the rod, means for locking the cylinder in the' housing vand means for sliding the member from the cylinder when the cylinder is locked so that the balls are disengaged "from the grooves and the rod is free to slide from the housing, said last-mentioned means including a spring coiled in the housingvand connected between the end of the housing opposite the end receiving the rod and the member. v
Y 2. The combination Afof claim 1 wherein said member includes a sleeve and `rsaid movement limiting means includes a plate on one end of the sleeve closing toil said end Iand extending laterally from the sleeve for abutting engagement of one end .of the cylinder.
3. The combination of claim l, wherein said locking means rfor the cylinder .includes spring l,loaded detents carried by the `cylinder and .en- :gageable in openings in the inner ,surface of the housing.
References Cited in the file of this patent UNITED AS'TAlflllS PA'I'ENTS Number `Name Date 1,895,999 Kuhlemann Jan. 31., 1933 1,985,890 Ellis Jan. 1, 1935 2,562,459 ,Heey July 31, 1951
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969212A (en) * 1956-08-31 1961-01-24 Martin James Apparatus for ejecting bodies from a parent aerodyne
US2995323A (en) * 1960-02-03 1961-08-08 Irving Air Chute Co Inc Device for controlling the effective reefing and dereefing of a parachute canopy
US3018074A (en) * 1957-09-09 1962-01-23 Gq Parachute Comp Ltd Parachute pack
US3056568A (en) * 1959-04-20 1962-10-02 Gen Mills Inc Aerodynamic retardation device
DE3708160A1 (en) * 1986-04-07 1990-12-06 Burghardt Krebber DEVICE FOR ACCELERATING THE OPENING OPERATION AND / OR. SHAPING OF AIRCRAFT DEVICES, LIKE CAPS, UMBRELLAS, MATTRESSES, PARAGLIDES, GLIDERS (DRAGONS), etc.
US7134701B1 (en) 2003-01-03 2006-11-14 Ronning James M Frame for lifting beams and other elongated loads
CN103523230A (en) * 2013-10-15 2014-01-22 江苏艾锐泰克无人飞行器科技有限公司 Landing assistant parachute of unmanned aerial vehicle
CN103523237A (en) * 2013-10-15 2014-01-22 江苏艾锐泰克无人飞行器科技有限公司 Buffering connecting rod of landing assistant parachute of unmanned aerial vehicle

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1895999A (en) * 1928-09-17 1933-01-31 Carl H Lundholm Aktiebolag Parachute device
US1985890A (en) * 1933-08-31 1935-01-01 Walter C Ellis Time controlled releasing mechanism
US2562459A (en) * 1949-01-14 1951-07-31 Richard Keoleian Automatic parachute release

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1895999A (en) * 1928-09-17 1933-01-31 Carl H Lundholm Aktiebolag Parachute device
US1985890A (en) * 1933-08-31 1935-01-01 Walter C Ellis Time controlled releasing mechanism
US2562459A (en) * 1949-01-14 1951-07-31 Richard Keoleian Automatic parachute release

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2969212A (en) * 1956-08-31 1961-01-24 Martin James Apparatus for ejecting bodies from a parent aerodyne
US3018074A (en) * 1957-09-09 1962-01-23 Gq Parachute Comp Ltd Parachute pack
US3056568A (en) * 1959-04-20 1962-10-02 Gen Mills Inc Aerodynamic retardation device
US2995323A (en) * 1960-02-03 1961-08-08 Irving Air Chute Co Inc Device for controlling the effective reefing and dereefing of a parachute canopy
DE3708160A1 (en) * 1986-04-07 1990-12-06 Burghardt Krebber DEVICE FOR ACCELERATING THE OPENING OPERATION AND / OR. SHAPING OF AIRCRAFT DEVICES, LIKE CAPS, UMBRELLAS, MATTRESSES, PARAGLIDES, GLIDERS (DRAGONS), etc.
US7134701B1 (en) 2003-01-03 2006-11-14 Ronning James M Frame for lifting beams and other elongated loads
CN103523230A (en) * 2013-10-15 2014-01-22 江苏艾锐泰克无人飞行器科技有限公司 Landing assistant parachute of unmanned aerial vehicle
CN103523237A (en) * 2013-10-15 2014-01-22 江苏艾锐泰克无人飞行器科技有限公司 Buffering connecting rod of landing assistant parachute of unmanned aerial vehicle

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