US3175699A - Hydraulic draft gear - Google Patents

Hydraulic draft gear Download PDF

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US3175699A
US3175699A US182428A US18242862A US3175699A US 3175699 A US3175699 A US 3175699A US 182428 A US182428 A US 182428A US 18242862 A US18242862 A US 18242862A US 3175699 A US3175699 A US 3175699A
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piston
variable volume
draft gear
volume chambers
fluid
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US182428A
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William G Price
Jr George E Frederick
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ACF Industries Inc
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ACF Industries Inc
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B61RAILWAYS
    • B61GCOUPLINGS; DRAUGHT AND BUFFING APPLIANCES
    • B61G9/00Draw-gear
    • B61G9/04Draw-gear combined with buffing appliances
    • B61G9/08Draw-gear combined with buffing appliances with fluid springs or fluid shock-absorbers; Combinations thereof

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  • resilient draft gears such as rubber cartridges, springs, etc., have the disadvantage of returning a major part of the energy which was initially applied to the draft gear by recoil to the train or cars.
  • This invention relates to shock absorbing units for use on railway vehicles to absorb impact shocks during shunting and/oito provide an energy dissipative type draft connection between vehicles during running.
  • the impact cushioning ability of the draft gear is ap- As for energy dissipative devices in the past, they have It is also true that there have been It is therefore a More particularly, it is an object of this invention to provide a structurally sound hydraulic shock absorber for a standard draft gear pocket which is capable of controlled automatic recovery from a compressed condition.
  • Still another object is to snub the return of said hydraulic drafti gear from its compressed condition tc eliminate recoil forces in the hydraulic draft gear.
  • a further object is to prevent rupture of the hydraulic draft gear upon the occurrence of excessive buff and draft forces.
  • FIGURE l is a plan view of a railway car sill structure mounting a coupler and an Iall hydraulic draft gear of the present invention
  • FIGURE 2 is a side v-iew of the assembly of FIG- 55 URE l;
  • FIGURE 3 is a sectional View of a shock absorber designed in accordance with the present invention.
  • FIGURES 4 and 5 are views of the end plates of the 0 FIGURE 6 is a sectional view of a modified shock absorber
  • FIGURE 7 is a sectional view showing another arrangement for the modified shock absorber of FIGURE 6.
  • FIGURE 1 there is shown a railway car center sill 10 having a striker face 12 and a center filler 14 between which is found a draft gear pocket 16.
  • a coupler 18 is passed through an opening 20 and bears, as at 22, against a follower plate 24 which in turn bears against stop flanges 26 provided by the rearward structure of the striker 12 thereby preventing movement of the follower plate 24 leftwardly from the position shown in FIGURES 1 and 2.
  • the coupler has la draft key 28 which is passed through a slot 30 of the coupler 18 and through an elongated opening 32 in a yoke 34.
  • the yoke 34 surrounds a shock absorber 36 centrally of the stop flanges 26 and a similar peripheral stop 38 formed with the center ller 14.
  • shock absorber details two general types are hereinafter discussed, namely a hydraulic shock absorber with an air return chamber and a hydraulic unit with a spring return.
  • both of these units incorporate several common features such as end plate design, see FIGURES 4 and 5, and a capacity to cushion forces being applied to cars having a wide range of load conditions.
  • This latter feature is accomplished by incorporating a metering pin into each of the various units which is capable of obtaining the above results.
  • a metering pin for each of the units that takes into consideration the minimum load and the maximum load of the railroad car, and such a pin could be described as one which has a step taper form. This means that the metering pin closes the orifice at one rate for a lightly loaded car and at another or faster rate with a heavier car load.
  • a cylinder 44 is shown having an integral wall 46 at one end through which the metering pin 41 is mounted, as at 48.
  • the wall 46 is formed as a rectangular structure that fits within the draft gear pocket such that it is in contact with one of the sill stop means above mentioned.
  • the cylinder 44 is also provided with an open end 50 through which a tubular member 52 may be inserted.
  • a wall 54 is mounted, said Wall having an orifice 56, which orifice is operatively associated with pin 41.
  • the member 52 is held centered in the cylinder by a bearing 5S, and the cylinder has its open end closed around member 52 by means of a packing gland 60 held in said open end by a gland nut 62. Behind the wall 54 within member 52 is a iioating piston 64. The member 52 is closed by an end cap 66 which is also formed as a rectangular structure to cooperate with the stops of the draft gear pocket as does wall 46. In addition, member 52 is provided with a charging valve 68, as seen in FIGURE 4, so that proper return pessure may be realized and that air leakage may be compensated for.
  • the cylinder 44 is substantially filled with an incompressible Huid; whe-reas the tubular member 52 is charged with a compressible fluid, such as air by means of valve 68.
  • the floating piston 64 separates Athe two fluids.
  • the tubular member 52 is provided with a plurality of annularly spaced bores 76 about which an annular collar 72 having a metering orioe 74 is placed such that compression of the shock absorber ports fluid to an annular chamber 76 by displacing the collar 72, and extension of the unit, -by release of the stored energy in the compressible iiuid, causes the collar to cover the bores 70 and meter the ow from chamber 76 to within the tubular member 52. This effectively snubs the extension of the shock absorber.
  • shock absorbers of FIGURES 6 and 7 represent the preferred shock absorber arrangement in that return forces of the spring are not as intense as in the compressed air lunit ⁇ of FIGURE 3.
  • a tubular member 78 is provided having integral radiating iianges 80 at one end thereof.
  • a ller plug S2 is joined to said tubular member 78 centrally of the flanges 0, as by the screw threads S4 shown in FIGURE 6; ⁇ and plug S2 mounts the metering pin 42 along the central axis of tube 78.
  • a rod 86 is reciprocaliy mounted within member 78 as by a bearing seal 88, and rod 36 has a rectangular plate 90 joined therewith.
  • a tapped hole 91 shown in FIGURE 7 may be provided for joining plate 90 to rod 86.
  • Plate 90 and flange are operatively associated with the stops 26 and 38 of the draft gear pocket 16.
  • the diameter of rod 86 is such as to form an ⁇ annular space 92 between it and the inner diameter of tube 78; and the rod 86 is provided with a piston face 94 having centrally located oriiice 96 opening into a bore 98 within the rod 86 adjacent its piston face.
  • the bore 98 is provided with radial passages 100, which passages communicate the bore 93 with space 92 about the rod S6.
  • a sleeve 102 is mounted to tube 78 Within space 92, and sleeve 102 in turn mounts a compressible member 104, such as a neoprene sponge rubber, occupying a major portion of the space 92.
  • the compressible metmber should be made of a material capable of operation throughout a temperature range of from -50 F. to 200 F.
  • an impervious membrane 106 encloses the member.
  • a rod 87 is provided with a piston 95 at one end adapted to slide in a cylinder or tube 79.
  • Tube 79 is provided with a ange 81 and an end wall 83 in which a variably tapered metering pin 43 is removably mounted.
  • Sleeve 103 forms the bearing seal between rod 87 and tube 79.
  • a nozzle or valve body 111 is held by a retaining ring 109 in a central aperture of piston 95.
  • Valve body 111 is formed with a seat 107 and with a plurality of axial passages 112 leading to groove or opening 113.
  • Opening 113 is normally closed by valve spool 115 having notched portions 117 at the outer end thereof and arranged to abut sleeve 119 at its other end.
  • Sleeve 119 has openings 121 to the bore 99 and chamber 93.
  • Valve spool 115 has a stepped coniiguration providing an annular pressure responsive face 110 whose ⁇ area is such as to enable a predetermined pressure in chamber 129 to overcome the force of spring 123, which acts against bearing plate 125. Plate 125 is threaded to sleeve 119 and is locked thereto by set screw 127.
  • valve spool 115 moves further into chamber 129 and during the course of travel metering pin 43 enters orifice 97 and controls the flow Ithrough it into chamber 93. If excessive pressure is developed in chamber 129, due to excessive buff or draft forces, the iiuid in passages 112 acting on face 110 of valve spool 115 overcomes the force of spring 123 on spool 115 and moves spool 115 so as to place passages 112 in communication through tubular network 108 with chamber 93.
  • the path between chambers 129 and 93 is via passages 112, opening 113, notches 117, opening 121 and passage 101.
  • the length of spool 115 is such as to provide bearing support for the spool when it moves to the left to open notches 117 to opening 113.
  • Ithe tubular network 108 and spool 115 and their assorted elements form a spring loaded bypass valve that relieves excess pressure within chamber 129.
  • a spring 114 as seen in FIGURE 6, is provided, which spring is compressed between plate 90 and a shoulder 116 of the tube 78.
  • a similar shoulder and spring may be provided with the unit of FIGURE 7.
  • Such ⁇ a spring return is, however, aided by the comprcssible member 104 or 105 which forces the fluid from space 92 or 93 ⁇ through passages or 101 and bore 93 or 99 into orifice 96 or 97 and out into tube 7S or 79.
  • a kinetic energy absorbing device comprising:
  • a piston dividing said cylinder into two variable volume chambers, said piston having a tubular extension with radial passageways which in association with passageways in said piston provide fluid communication for said variable volume chambers;
  • iiuid pressure responsive means controls ejection of a uid from one of said variable volume chambers upon relief of loads on said energy absorbing device
  • a kinetic energy absorbing device according to claim l further comprising a step taper form metering pin removably mounted within said cylinder in axial alignment with one of the passageways in said piston to close the area of the passageway at a varying rate.
  • a kinetic energy absorbing device comprising:
  • a piston dividing said cylinder into two variable volume chambers, said piston having a tubular extension with passageways in said piston which provide iiuid communication for said variable volume chambers;
  • iiuid pressure responsive means in one of said variable volume chambers, which iuid pressure responsive eans controls ejection of a fluid from one of said variable volume chambers upon relief of loads on said energy absorbing device;

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Fluid-Damping Devices (AREA)

Description

March 30, 1965 w. cs. PRICE ETAL HYDRAULIC DRAFT GEAR 4 Sheets-Sheet l Filed March 26, 1962 i Ill @DIW ATTORNEY March 30, i965 w. G. PRICE ETAL 3,][75699 HYDRAULIC DRAFT GEAR Filed Maron ze, 1962 4 sheets-sheet 2 March 30, 1965 w. G. PRICE ETAL 3,175,699
, HYDRAULIC DRAFT GEAR Filed March 26, 1962 4 Sheets-Sheet 5 7 Taf/VE? March 30, 1965 w. G. PRICE ETAL HYDRAULIC DRAFT GEAR 4 Sheets-Sheet 4 Filed March 26, 1962 proximately equivalent to the amount of energy that it can absorb during a closure movement of the gear. addition resilient draft gears, such as rubber cartridges, springs, etc., have the disadvantage of returning a major part of the energy which was initially applied to the draft gear by recoil to the train or cars.
shock absorber of FIGURE 3;
nied States Patent 3,175,699 HYDRAULIC DRAFT GEAR William G. Price and George lE. Frederick, Jr., South Bend, Ind., assignors, by mesne assignments, to ACF Industries, Incorporated, New York, NSY., a corporation of New .Iersey Filed Mar. 26, 1962, Ser. No. 182,423 3 Claims. (Cl. 213-43) This invention relates to shock absorbing units for use on railway vehicles to absorb impact shocks during shunting and/oito provide an energy dissipative type draft connection between vehicles during running.
The impact cushioning ability of the draft gear is ap- As for energy dissipative devices in the past, they have It is also true that there have been It is therefore a More particularly, it is an object of this invention to provide a structurally sound hydraulic shock absorber for a standard draft gear pocket which is capable of controlled automatic recovery from a compressed condition.
It is another object to provide an all hydraulic draft gear so that a high initial resistance to buff or draft forces is developed at the inception of such forces, which resistance is maintained at a substantial value throughout the duration of such force.
Still another object is to snub the return of said hydraulic drafti gear from its compressed condition tc eliminate recoil forces in the hydraulic draft gear.
A further object is to prevent rupture of the hydraulic draft gear upon the occurrence of excessive buff and draft forces.
Other objects and features of our invention will become apparent from a detailed description of the device which follows with reference to the accompanying draw ings wherein:
FIGURE l is a plan view of a railway car sill structure mounting a coupler and an Iall hydraulic draft gear of the present invention;
FIGURE 2 is a side v-iew of the assembly of FIG- 55 URE l;
FIGURE 3 is a sectional View of a shock absorber designed in accordance with the present invention;
FIGURES 4 and 5 are views of the end plates of the 0 FIGURE 6 is a sectional view of a modified shock absorber; and
FIGURE 7 is a sectional view showing another arrangement for the modified shock absorber of FIGURE 6.
Referring now to FIGURE 1, there is shown a railway car center sill 10 having a striker face 12 and a center filler 14 between which is found a draft gear pocket 16. A coupler 18 is passed through an opening 20 and bears, as at 22, against a follower plate 24 which in turn bears against stop flanges 26 provided by the rearward structure of the striker 12 thereby preventing movement of the follower plate 24 leftwardly from the position shown in FIGURES 1 and 2.
The coupler has la draft key 28 which is passed through a slot 30 of the coupler 18 and through an elongated opening 32 in a yoke 34. The yoke 34 surrounds a shock absorber 36 centrally of the stop flanges 26 and a similar peripheral stop 38 formed with the center ller 14.
When undergoing a buff load the coupler displaces the plate 24 to compress the shock absorber against stops 38; whereas a draft force on coupler 18 cau-ses the yoke 34 to compress the shock absorber against stops 26.
As for the shock absorber details, two general types are hereinafter discussed, namely a hydraulic shock absorber with an air return chamber and a hydraulic unit with a spring return. However, both of these units incorporate several common features such as end plate design, see FIGURES 4 and 5, and a capacity to cushion forces being applied to cars having a wide range of load conditions. This latter feature is accomplished by incorporating a metering pin into each of the various units which is capable of obtaining the above results. In more detail, it is our intent to provide a metering pin for each of the units that takes into consideration the minimum load and the maximum load of the railroad car, and such a pin could be described as one which has a step taper form. This means that the metering pin closes the orifice at one rate for a lightly loaded car and at another or faster rate with a heavier car load.
With regard to the air return type of shock absorber as shown by FIGURE 3, a cylinder 44 is shown having an integral wall 46 at one end through which the metering pin 41 is mounted, as at 48. The wall 46 -is formed as a rectangular structure that fits within the draft gear pocket such that it is in contact with one of the sill stop means above mentioned. The cylinder 44 is also provided with an open end 50 through which a tubular member 52 may be inserted. At one end of member 52 a wall 54 is mounted, said Wall having an orifice 56, which orifice is operatively associated with pin 41. The member 52 is held centered in the cylinder by a bearing 5S, and the cylinder has its open end closed around member 52 by means of a packing gland 60 held in said open end by a gland nut 62. Behind the wall 54 within member 52 is a iioating piston 64. The member 52 is closed by an end cap 66 which is also formed as a rectangular structure to cooperate with the stops of the draft gear pocket as does wall 46. In addition, member 52 is provided with a charging valve 68, as seen in FIGURE 4, so that proper return pessure may be realized and that air leakage may be compensated for.
The cylinder 44 is substantially filled with an incompressible Huid; whe-reas the tubular member 52 is charged with a compressible fluid, such as air by means of valve 68. The floating piston 64 separates Athe two fluids. Between the wall 54 and the piston 64 the tubular member 52 is provided with a plurality of annularly spaced bores 76 about which an annular collar 72 having a metering orioe 74 is placed such that compression of the shock absorber ports fluid to an annular chamber 76 by displacing the collar 72, and extension of the unit, -by release of the stored energy in the compressible iiuid, causes the collar to cover the bores 70 and meter the ow from chamber 76 to within the tubular member 52. This effectively snubs the extension of the shock absorber.
As for the shock absorbers of FIGURES 6 and 7, they represent the preferred shock absorber arrangement in that return forces of the spring are not as intense as in the compressed air lunit `of FIGURE 3. With reference to the unit shown in FIGURE 6, a tubular member 78 is provided having integral radiating iianges 80 at one end thereof. A ller plug S2 is joined to said tubular member 78 centrally of the flanges 0, as by the screw threads S4 shown in FIGURE 6; `and plug S2 mounts the metering pin 42 along the central axis of tube 78. A rod 86 is reciprocaliy mounted within member 78 as by a bearing seal 88, and rod 36 has a rectangular plate 90 joined therewith. A tapped hole 91 shown in FIGURE 7 .may be provided for joining plate 90 to rod 86. Plate 90 and flange are operatively associated with the stops 26 and 38 of the draft gear pocket 16. The diameter of rod 86 is such as to form an `annular space 92 between it and the inner diameter of tube 78; and the rod 86 is provided with a piston face 94 having centrally located oriiice 96 opening into a bore 98 within the rod 86 adjacent its piston face. The bore 98 is provided with radial passages 100, which passages communicate the bore 93 with space 92 about the rod S6. In addition, a sleeve 102 is mounted to tube 78 Within space 92, and sleeve 102 in turn mounts a compressible member 104, such as a neoprene sponge rubber, occupying a major portion of the space 92. The compressible metmber should be made of a material capable of operation throughout a temperature range of from -50 F. to 200 F. In order that the compressible member may be protected an impervious membrane 106 encloses the member.
In the shock absorber shown in FIG. 7, a rod 87 is provided with a piston 95 at one end adapted to slide in a cylinder or tube 79. Tube 79 is provided with a ange 81 and an end wall 83 in which a variably tapered metering pin 43 is removably mounted. A compressible material 105 similar to material 104 in FIG. 6, occupies chamber 93. Sleeve 103 forms the bearing seal between rod 87 and tube 79. A nozzle or valve body 111 is held by a retaining ring 109 in a central aperture of piston 95. Valve body 111 is formed with a seat 107 and with a plurality of axial passages 112 leading to groove or opening 113. Opening 113 is normally closed by valve spool 115 having notched portions 117 at the outer end thereof and arranged to abut sleeve 119 at its other end. Sleeve 119 has openings 121 to the bore 99 and chamber 93. Valve spool 115 has a stepped coniiguration providing an annular pressure responsive face 110 whose `area is such as to enable a predetermined pressure in chamber 129 to overcome the force of spring 123, which acts against bearing plate 125. Plate 125 is threaded to sleeve 119 and is locked thereto by set screw 127.
When a load or force is applied to the shock absorber,
piston moves further into chamber 129 and during the course of travel metering pin 43 enters orifice 97 and controls the flow Ithrough it into chamber 93. If excessive pressure is developed in chamber 129, due to excessive buff or draft forces, the iiuid in passages 112 acting on face 110 of valve spool 115 overcomes the force of spring 123 on spool 115 and moves spool 115 so as to place passages 112 in communication through tubular network 108 with chamber 93. The path between chambers 129 and 93 is via passages 112, opening 113, notches 117, opening 121 and passage 101. The length of spool 115 is such as to provide bearing support for the spool when it moves to the left to open notches 117 to opening 113. Thus, Ithe tubular network 108 and spool 115 and their assorted elements form a spring loaded bypass valve that relieves excess pressure within chamber 129.
In order to re-turn the shock absorber to its normal extended position after buff or draft forces are relieved, a spring 114, as seen in FIGURE 6, is provided, which spring is compressed between plate 90 and a shoulder 116 of the tube 78. A similar shoulder and spring may be provided with the unit of FIGURE 7. Such `a spring return is, however, aided by the comprcssible member 104 or 105 which forces the fluid from space 92 or 93 `through passages or 101 and bore 93 or 99 into orifice 96 or 97 and out into tube 7S or 79.
It may be readily appreciated that other structural variations tmay be encompassed by our invention, Therefore, we do not intend to be limited by the above description, but rather by `the appended claims.
We claim:
1. In a railroad draft gear pocket, a kinetic energy absorbing device comprising:
a fluid containing cylinder;
a piston dividing said cylinder into two variable volume chambers, said piston having a tubular extension with radial passageways which in association with passageways in said piston provide fluid communication for said variable volume chambers;
a fluid pressure responsive means in one of said variable volume chambers, which iiuid pressure responsive means controls ejection of a uid from one of said variable volume chambers upon relief of loads on said energy absorbing device;
a Spring loaded valve in said tubular extension of said piston to relieve excess pressures in the other of said variable volume chambers by opening one of the passageways in said piston to permit an increased iiuid flow therethrough; and
means mounting said energy absorbing device in an operative arrangement within said draft gear pocket.
2. A kinetic energy absorbing device according to claim l further comprising a step taper form metering pin removably mounted within said cylinder in axial alignment with one of the passageways in said piston to close the area of the passageway at a varying rate.
3. In a railroad draft gear pocket, a kinetic energy absorbing device comprising:
a fluid containing cylinder;
a piston dividing said cylinder into two variable volume chambers, said piston having a tubular extension with passageways in said piston which provide iiuid communication for said variable volume chambers;
a iiuid pressure responsive means in one of said variable volume chambers, which iuid pressure responsive eans controls ejection of a fluid from one of said variable volume chambers upon relief of loads on said energy absorbing device;
a spring loaded valve in said tubular extension of said piston to relieve excess pressures in the other of said variable volume chambers by opening one of the passageways in said piston to permit an increased fluid flow therethrough; and
means mounting said energy absorbing device in an operative arrangement within said draft gear pocket.
References Cited in the file of this patent UNITED STATES PATENTS 1,955,349 Stevens Apr. 17, 1934 2,841,294 Hendrickson et al. July l, 1958 2,909,292 Hendrickson c Oct. 20, 1959 2,914,195 Pawling Nov. 24, 1959 2,963,175 Thornhill Dec. 6, 1960 2,994,442 Frederick Aug. 1, 1961

Claims (1)

1. IN A RAILROAD DRAFT GEAR POCKET, A KINETIC ENERGY ABSORBING DEVICE COMPRISING: A FLUID CONTAINING CYLINDER; A PISTON DIVIDING SAID CYLINDER INTO TWO VARIABLE VOLUME CHAMBERS, SAID PISTON HAVING A TUBULAR EXTENSION WITH RADIAL PASSAGEWAYS WHICH IN ASSOCIATION WITH PASSAGEWAYS IN SAID PISTON PROVIDED FLUID COMMUNICATION FOR SAID VARIABLE VOLUME CHAMBERS; A FLUID PRESSURE RESPONSIVE MEANS IN ONE OF SAID VARIABLE VOLUME CHAMBERS, WHICH FLUID PRESSURE RESPONSIVE MEANS CONTROLS EJECTION OF A FLUID FROM ONE OF SAID VARIABLE VOLUME CHAMBERS UPON RELIEF OF LOADS ON SAID ENERGY ABSORBING DEVICE; A SPRING LOADED VALVE IN SAID TUBULAR EXTENSION OF SAID PISTON TO RELIEVE EXCESS PRESSURES IN THE OTHER OF SAID VARIABLE VOLUME CHAMBERS BY OPENING ONE OF THE PASSAGEWAY IN SAID PISTON TO PERMIT AN INCREASED FLUID FLOW THERETHROUGH; AND MEANS MOUNTING SAID ENERGY ABSORBINT DEVICE IN AN OPERATIVE ARRANGEMENT WITHIN SAID DRAFT GEAR POCKET.
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3237574A (en) * 1964-09-10 1966-03-01 Keystone Railway Equip Impact absorbing apparatus
US3332364A (en) * 1964-09-10 1967-07-25 Keystone Railway Equip Impact absorbing apparatus
US3378149A (en) * 1966-02-14 1968-04-16 Acf Ind Inc Railway car cushioning device
US3398812A (en) * 1966-09-07 1968-08-27 Gerald H. Peterson Kinetic energy absorber
US3499546A (en) * 1968-01-25 1970-03-10 Hydra Cushion Inc Hydraulic cushion device
US3762695A (en) * 1972-01-19 1973-10-02 Us Navy Shock absorber

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1955349A (en) * 1928-10-27 1934-04-17 Cardwell Westinghouse Co Hydraulic draft gear
US2841294A (en) * 1956-06-04 1958-07-01 Pacific Car & Foundry Co Hydraulic draft gears
US2909292A (en) * 1956-06-06 1959-10-20 Pacific Car & Foundry Co Hydraulic draft gears
US2914105A (en) * 1957-06-06 1959-11-24 Sydney Accessories Inc Handbag structure
US2963175A (en) * 1957-05-16 1960-12-06 Oleo Pneumatics Ltd Buffers for railway, tramway and like vehicles
US2994442A (en) * 1960-06-20 1961-08-01 Bendix Corp Kinetic energy absorbing device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1955349A (en) * 1928-10-27 1934-04-17 Cardwell Westinghouse Co Hydraulic draft gear
US2841294A (en) * 1956-06-04 1958-07-01 Pacific Car & Foundry Co Hydraulic draft gears
US2909292A (en) * 1956-06-06 1959-10-20 Pacific Car & Foundry Co Hydraulic draft gears
US2963175A (en) * 1957-05-16 1960-12-06 Oleo Pneumatics Ltd Buffers for railway, tramway and like vehicles
US2914105A (en) * 1957-06-06 1959-11-24 Sydney Accessories Inc Handbag structure
US2994442A (en) * 1960-06-20 1961-08-01 Bendix Corp Kinetic energy absorbing device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3237574A (en) * 1964-09-10 1966-03-01 Keystone Railway Equip Impact absorbing apparatus
US3332364A (en) * 1964-09-10 1967-07-25 Keystone Railway Equip Impact absorbing apparatus
US3378149A (en) * 1966-02-14 1968-04-16 Acf Ind Inc Railway car cushioning device
US3398812A (en) * 1966-09-07 1968-08-27 Gerald H. Peterson Kinetic energy absorber
US3499546A (en) * 1968-01-25 1970-03-10 Hydra Cushion Inc Hydraulic cushion device
US3762695A (en) * 1972-01-19 1973-10-02 Us Navy Shock absorber

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