US3056623A - Store ejector rack - Google Patents

Store ejector rack Download PDF

Info

Publication number
US3056623A
US3056623A US838288A US83828859A US3056623A US 3056623 A US3056623 A US 3056623A US 838288 A US838288 A US 838288A US 83828859 A US83828859 A US 83828859A US 3056623 A US3056623 A US 3056623A
Authority
US
United States
Prior art keywords
store
rack
lever
ejector
hooks
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
US838288A
Inventor
Donald H Herbert
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.)
BOHANAN Manufacturing Co
Original Assignee
BOHANAN Manufacturing Co
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 BOHANAN Manufacturing Co filed Critical BOHANAN Manufacturing Co
Priority to US838288A priority Critical patent/US3056623A/en
Application granted granted Critical
Publication of US3056623A publication Critical patent/US3056623A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/04Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B64D1/06Bomb releasing; Bombs doors

Definitions

  • This invention relates to a rack for carrying and ejecting stores from fast-moving aircraft, especially those moving at supersonic speeds.
  • the terms store or stores are intended to include a variety of devices, of which bombs and missiles are examples.
  • an object of the present invention is to provide a store'ejecting rack that is safe to use, is firmly locked against accidental release until ready for ejection of the store, and is so balanced in its ejecting means as to control the angle of ejection of the store, as desired.
  • Another object of the invention is to provide a storeejecting rack that is operated to eject a store by the pressure of gases generated by explosive means, the rack utilizing said pressure gases both to release or unlock the ejecting mechanism and to operate said mechanism to eject a store.
  • a further object of the invention is to provide a store ejector rack in which a store is so suspended that the weight of the store is cumulative to the pressure of the ejectors to cause completion of the ejection movement of the store-suspending means after the same is released or unlocked, as above indicated.
  • the invention also has for its objects to provide such means that are positive in operation, convenient in use, easily installed in a working position and easily disconnected therefrom, economical of manufacture, relatively simple, and of general superiority and serviceability.
  • FIG. 1 is a top plan view of a store ejector rack according to the present invention.
  • FIG. 2 is an enlarged and fragmentary vertical sectional view as taken on the line 22 of FIG. 7.
  • FIG. 3 is a similarly enlarged cross-sectional View as taken on the line 3-3 of FIG. 4.
  • FIG. 4 is a longitudinal sectional view as taken on the line 4-4 of FIG. 1 and drawn to a scale somewhat larger than FIG. 1.
  • FIG. 5 is an enlarged fragmentary sectional view as taken on the line 5-5 of FIG. 4.
  • FIG. 6 is a similarly enlarged sectional view of breech and control means shown in FIG. 4.
  • FIG. 7 is a sectional View of the night-hand end of the rack, the same constituting an extension of the rack portion shown in FIG. 4.
  • FIG. 8 is an enlarged partial elevational and partial sectional view of the breech shown in FIGS. 4 and 6.
  • FIG. 9 is a fragmentary elevational view of operating mechanism, as in FIG. 4, but shown in released or unlocked position.
  • the store ejector rack that is illustrated comprises, generally, a frame 10, means 11 to provide a source of power for operating the present rack, normally locked trnechainsm 12 for operating the rack, means 13 operated by the means 11 to actuate the means 12 to unlocked or released position, safety locking means 14 for the means 15, store hanger means 15 at each end of the rack frame 10 normally held locked by the means 12 and released for movement to release a store hanging therefrom by unlocking of the means 12, store ejector units 16 adjacent each end of the rack frame, adjustable means 17 pro vided at the lower portion of each unit 16 for engaging a store suspended or hung from the means 15, an adjustable ejector piston 18 in each unit 16, and means 19 for varying the operating pressure on at least one of the pistons 18 to effect control of the angle of ejection of a store suspended from the means 15.
  • the frame 16 is shown as comprising two side plates 25 that are spaced and connected by top, end and lower spacers 26 to provide the frame with an inner space 27.
  • the means 11 is shown as a breech block 28 mounted in the space 2 7 and formed to have two bores 29 into which explosives are placed in tubular closure plugs 30 that are screwed into bores 29.
  • Such explosives may be in cartridge form and, when detonated, as by caps 31, capable of creating pressures as high as 50,000 psi. in the interiors of the plugs.
  • Such explosives generate temperatures between 8,000 and 10,000 F. Accordingly, the block 28 and plugs 30 are designed to withstand the high pressures and temperatures above mentioned.
  • the explosives may be detonated in any of various ways. Electrical detonation is preferred. The means that may be used for this purpose is not illustrated because it is quite conventional.
  • the mechanism 12 (FIGS. 4 and 9) is shown as comprising a lever 37 of inverted T form having a cross arm 39 and rockable on a pivot 38 carried by the plates 25.
  • a spring device 40 is arranged to bias the cross arm in one direction against a fixed stop 41, and an adjustable rod 42 extends from each end of said cross arm and pivotally connects at 43 to said ends.
  • the cross arm is so angled, that when against stop 41, the axis of the rods 42 connected to the stopped end of the cross arm passes through the axis of pivot 33 while the axis of the other rod 42 will pass in over-center relationship to the pivot 38.
  • any forces imposed axially on the rods 42 in a direction toward pivot 38- are solidly resisted. Only when the lever 37 is rocked in a clockwise direction, as shown in FIG. 9, is the means 12 unlocked.
  • the actuating means 13 for the mechanism 12 is best seen in FIGS. 3, 4 and 6, the same being powered by the pressure gas flowing into the passage 34.
  • Said means 13 comprises a.- fitting 43a that has a cylinder bore 44 that opens into passage 34 and a connecting rod bore 45, a piston 46 in the cylinder bore and subject to the pressure in passage 34 to be projected into the cylinder bore, a rod 47 on the piston and extending through the bore 45, an adjustable stop nut 48 on said rod, an actuator 49 engaged against the nut 48 and provided with ends 50 (seen in FIG. 3 and shown dotted in FIG. 6) that slide in horizontal slots 51 in the side plates 25 (FIG. 3), an extension rod 52 carried by the actuator 49 and guided in a bracket 53, and a spring 54 around rod 52 having abutment, at one end, against bracket 53 and, at the other end, in biasing engagement with the actuator 49.
  • lever 37 is forked at its upper end so that the rod 52 may be disposed between the sides of said lever, the sides having bearing engagement against the edge of the actuator 49.
  • the pressure of gases on piston 46 projects the actuator 49 against the bias of spring 54 and rocks lever 37 from the locked position of FIG. 4 to the released position of FIG. 9, thereby unlocking the mechanism 12.
  • the safety locking means 14 is shown as electrical and comprises a solenoid 56 that has a spring projected floating core 57, and a bell crank lever 58 that is moved by said solenoid around a pivot 59.
  • An arm 69 of lever 58 normally has interfering engagement, as shown, with arm 37 and is withdrawn from such engagement upon retraction of the core 57 and clockwise rocking of the lever 58. Only when the arm 37 is freed can the mechanism operate. Hence, inadvertent firing of the explosive cannot cause unlocking of the means 12.
  • physical or mechanical safety locks may be used instead of the means 14 or in addition thereto.
  • a cross pin may lock the end of lever 37 to the frame and be withdrawn when ejection is to be instituted.
  • the hanger means 15 each comprises hooks 61 and 62 on respective pivots 63 and 64 and connected by a link 65 so as to move together on their respective pivots. Said link is shown with an opening 66 to accommodate the unit 16 that is disposed between the hooks.
  • the book 61 of each pair of hooks is connected by a pivot 67 to the rod 42. It will be evident that when the means 12 is locked, the ledges 68 and 69 of the respective hooks 61 and 62 are horizontal and constitute level supports that engage loops 70 and 71 of stores 72 and 73.
  • the hooks 61 may carry one size of store and the hooks 62 a larger store. Or, all four hooks may be used to carry one store. In any case, the four hooks shown, being simultaneously movable by reason of their connecting links 65 and substantially simultaneously operable to store-releasing position, may be used together or in pairs, as the case may be.
  • Each store ejector unit is shown as a vertical housing 74 having a cylinder bore 75 therein and formed to have a closed end 76 and an open end 77, mounting ears 78 provided on the upper end of housing 74 and by means of which the rack is fastened in operative position on or in an aircraft, and a saddle-shaped end fitting 79 secured to the lower end of housing 74 and designed as laterally extending means that engage the store and hold the same against lateral movement while held suspended by the hanger means 15.
  • said fitting 79 is provided with means 17 that comprise a plurality of individually adjustable shoes 80 that are swivelly carried on ball joints 81 by adjustable screw plugs 82. It will be evident that said means 17, when adjusted according to the outer contours of the store, hold said store steady on its hooks.
  • Each ejector piston 18 is provided with a piston part 83 that fits the cylinder bore 75, and a ram part 84 that extends through the open end 77 of the housing 74 and is guided at said end in a bearing 85 carried by the housing.
  • the piston 18 is shown as lower end and as provided in the hollow thereof with an adjustable foot 86. The drawings clearly show that said foot may be retracted or extended, as desired, so the same firmly bears against a store while the piston is in its retracted position.
  • one or both units 16 may be provided with the means 19 for varying the ejection pressures reaching the ejection piston 18 of one unit 16 with respect to that of the piston of the other unit.
  • the means 19 is shown as a fitting 86 that is disposed across a passage 87 in the housing end 76 and which receives gases under pressure from the pipe 36.
  • Said fitting is provided with an orifice 8 8 that is smaller than the passage 87, the size of said orifice lowering the fiow of gases from said passage 87 into the inlet 89 to the cylinder bore 75.
  • one piston may have a lesser operating pressure thereon than the other, or the pressures on the two pistons may be equalized.
  • exact ejection control is afforded by the means 19.
  • An explosively operated ejector rack comprising: a pair of single hook means to suspend a store at longitudinally spaced points; a single pivoted lever of inverted T form; rods pivotally connected between the ends of the cross head of said lever and said hooks; a fixed stop effective to prevent rotation of said lever through an angle, in one direction, greater than required to hold the hooks in locked position; resilient means urging said lever against said stop; at least two store ejector means operated by pressure gas; a pressure chamber adapted to receive explosive means; pressure gas operated means effective when operated to rotate said lever against the effort of said resilient means in a direction to move said hooks to released position; and conduits directly connecting said pressure chamber with said ejector means and said means rotating said lever to ensure simultaneous flow of pressure gas into, and operation of, said ejector means and means rotating said lever.

Description

Oct. 2, 1962 D. H. HERBERT 3,056,623
STORE EJECTOR RACK Filed Sept. 4, 1959 3 Sheets-Sheet 1 INVENTOR. Dom/.0 H. HERBERT ATTOR Y Oct. 2, 1962 D. H. HERBERT STORE EJECTOR RACK 3 Sheets-Sheet 2 Filed Sept. 4, 1959 v T Q W k w O5 ltI .o w% m \m, mm. m E Q W r w m 1 A 9N RD gm M H a u 1 D wwww A o W. A o J Q2 m? fuk N am mm .1 m 3 m li Pm 0 WU R I g kw h @m M mm hm M J Oct. 2, 1962 HERBERT 3,056,623
STORE EJECTOR RACK Filed Sept. 4, 1959 5 Sheets-Sheet 3 United States Patent @fifice 3,055,623 Patented Got. 2, 1962 Ohio Filed Sept. 4, 1959, Ser. No. 838,235 4 Claims. (Cl. 294-83) This invention relates to a rack for carrying and ejecting stores from fast-moving aircraft, especially those moving at supersonic speeds. As here used, the terms store or stores are intended to include a variety of devices, of which bombs and missiles are examples.
Since stores, as above contemplated, require careful handling, in the interests of safety, and accurate discharge to insure efiicient direction toward a target area, an object of the present invention is to provide a store'ejecting rack that is safe to use, is firmly locked against accidental release until ready for ejection of the store, and is so balanced in its ejecting means as to control the angle of ejection of the store, as desired.
Another object of the invention is to provide a storeejecting rack that is operated to eject a store by the pressure of gases generated by explosive means, the rack utilizing said pressure gases both to release or unlock the ejecting mechanism and to operate said mechanism to eject a store.
A further object of the invention is to provide a store ejector rack in which a store is so suspended that the weight of the store is cumulative to the pressure of the ejectors to cause completion of the ejection movement of the store-suspending means after the same is released or unlocked, as above indicated.
The invention also has for its objects to provide such means that are positive in operation, convenient in use, easily installed in a working position and easily disconnected therefrom, economical of manufacture, relatively simple, and of general superiority and serviceability.
The invention also comprises novel details of construction and novel combinations and arrangements of parts, which will more fully appear in the course of the following description. However, the drawings merely show and the following description merely describes, one embodiment of the present invention, which is given by way of illustration or example only.
In the drawings, like reference characters designate similar parts in the several views.
FIG. 1 is a top plan view of a store ejector rack according to the present invention.
FIG. 2 is an enlarged and fragmentary vertical sectional view as taken on the line 22 of FIG. 7.
FIG. 3 is a similarly enlarged cross-sectional View as taken on the line 3-3 of FIG. 4.
FIG. 4 is a longitudinal sectional view as taken on the line 4-4 of FIG. 1 and drawn to a scale somewhat larger than FIG. 1.
FIG. 5 is an enlarged fragmentary sectional view as taken on the line 5-5 of FIG. 4.
FIG. 6 is a similarly enlarged sectional view of breech and control means shown in FIG. 4.
FIG. 7 is a sectional View of the night-hand end of the rack, the same constituting an extension of the rack portion shown in FIG. 4.
FIG. 8 is an enlarged partial elevational and partial sectional view of the breech shown in FIGS. 4 and 6.
FIG. 9 is a fragmentary elevational view of operating mechanism, as in FIG. 4, but shown in released or unlocked position.
The store ejector rack that is illustrated comprises, generally, a frame 10, means 11 to provide a source of power for operating the present rack, normally locked trnechainsm 12 for operating the rack, means 13 operated by the means 11 to actuate the means 12 to unlocked or released position, safety locking means 14 for the means 15, store hanger means 15 at each end of the rack frame 10 normally held locked by the means 12 and released for movement to release a store hanging therefrom by unlocking of the means 12, store ejector units 16 adjacent each end of the rack frame, adjustable means 17 pro vided at the lower portion of each unit 16 for engaging a store suspended or hung from the means 15, an adjustable ejector piston 18 in each unit 16, and means 19 for varying the operating pressure on at least one of the pistons 18 to effect control of the angle of ejection of a store suspended from the means 15.
The frame 16 is shown as comprising two side plates 25 that are spaced and connected by top, end and lower spacers 26 to provide the frame with an inner space 27.
The means 11 is shown as a breech block 28 mounted in the space 2 7 and formed to have two bores 29 into which explosives are placed in tubular closure plugs 30 that are screwed into bores 29. Such explosives may be in cartridge form and, when detonated, as by caps 31, capable of creating pressures as high as 50,000 psi. in the interiors of the plugs. Such explosives generate temperatures between 8,000 and 10,000 F. Accordingly, the block 28 and plugs 30 are designed to withstand the high pressures and temperatures above mentioned.
It will be realized that the pressures needed for ejecting a store at supersonic speeds and for controlling the angle of ejection must necessarily be high. Hence the 50,000 psi. above mentioned. As can be seen from FIGS. 6 and 8, the gases of explosion have two paths, one through ports 32 in the plugs 30 to passages 33 into a passage 34, and the other through ports 35 into two oppositely directed pipes or tubes 36.
The explosives may be detonated in any of various ways. Electrical detonation is preferred. The means that may be used for this purpose is not illustrated because it is quite conventional.
The mechanism 12 (FIGS. 4 and 9) is shown as comprising a lever 37 of inverted T form having a cross arm 39 and rockable on a pivot 38 carried by the plates 25. A spring device 40 is arranged to bias the cross arm in one direction against a fixed stop 41, and an adjustable rod 42 extends from each end of said cross arm and pivotally connects at 43 to said ends. As will be seen from FIG. 4, the cross arm is so angled, that when against stop 41, the axis of the rods 42 connected to the stopped end of the cross arm passes through the axis of pivot 33 while the axis of the other rod 42 will pass in over-center relationship to the pivot 38. Thus, any forces imposed axially on the rods 42 in a direction toward pivot 38- are solidly resisted. Only when the lever 37 is rocked in a clockwise direction, as shown in FIG. 9, is the means 12 unlocked.
The actuating means 13 for the mechanism 12 is best seen in FIGS. 3, 4 and 6, the same being powered by the pressure gas flowing into the passage 34. Said means 13 comprises a.- fitting 43a that has a cylinder bore 44 that opens into passage 34 and a connecting rod bore 45, a piston 46 in the cylinder bore and subject to the pressure in passage 34 to be projected into the cylinder bore, a rod 47 on the piston and extending through the bore 45, an adjustable stop nut 48 on said rod, an actuator 49 engaged against the nut 48 and provided with ends 50 (seen in FIG. 3 and shown dotted in FIG. 6) that slide in horizontal slots 51 in the side plates 25 (FIG. 3), an extension rod 52 carried by the actuator 49 and guided in a bracket 53, and a spring 54 around rod 52 having abutment, at one end, against bracket 53 and, at the other end, in biasing engagement with the actuator 49.
It will be seen, particularly from FIG. 3, that the lever 37 is forked at its upper end so that the rod 52 may be disposed between the sides of said lever, the sides having bearing engagement against the edge of the actuator 49. The pressure of gases on piston 46 projects the actuator 49 against the bias of spring 54 and rocks lever 37 from the locked position of FIG. 4 to the released position of FIG. 9, thereby unlocking the mechanism 12.
The safety locking means 14 is shown as electrical and comprises a solenoid 56 that has a spring projected floating core 57, and a bell crank lever 58 that is moved by said solenoid around a pivot 59. An arm 69 of lever 58 normally has interfering engagement, as shown, with arm 37 and is withdrawn from such engagement upon retraction of the core 57 and clockwise rocking of the lever 58. Only when the arm 37 is freed can the mechanism operate. Hence, inadvertent firing of the explosive cannot cause unlocking of the means 12. Under certain circumstances physical or mechanical safety locks may be used instead of the means 14 or in addition thereto. For instance, a cross pin may lock the end of lever 37 to the frame and be withdrawn when ejection is to be instituted.
The hanger means 15 .each comprises hooks 61 and 62 on respective pivots 63 and 64 and connected by a link 65 so as to move together on their respective pivots. Said link is shown with an opening 66 to accommodate the unit 16 that is disposed between the hooks. The book 61 of each pair of hooks is connected by a pivot 67 to the rod 42. It will be evident that when the means 12 is locked, the ledges 68 and 69 of the respective hooks 61 and 62 are horizontal and constitute level supports that engage loops 70 and 71 of stores 72 and 73.
The hooks 61 may carry one size of store and the hooks 62 a larger store. Or, all four hooks may be used to carry one store. In any case, the four hooks shown, being simultaneously movable by reason of their connecting links 65 and substantially simultaneously operable to store-releasing position, may be used together or in pairs, as the case may be.
It will be noted that the loops 7t and 71 engage the hook ledges 68 and 69 to one side of and below the hook pivots 63 and 64. Thus, the weight of a store on said hooks, at all times, seeks to force the hooks toward release position. This movement tendency is, of course, counteracted by the locked means 12 but becomes effective, when the means 12 is unlocked to the position of FIG. 9. Since one thousand or more pounds may be hanging on each hook, the latter are laterally displaced on their pivots when the means 12 is unlocked.
Each store ejector unit is shown as a vertical housing 74 having a cylinder bore 75 therein and formed to have a closed end 76 and an open end 77, mounting ears 78 provided on the upper end of housing 74 and by means of which the rack is fastened in operative position on or in an aircraft, and a saddle-shaped end fitting 79 secured to the lower end of housing 74 and designed as laterally extending means that engage the store and hold the same against lateral movement while held suspended by the hanger means 15.
As best seen in FIG. 2, said fitting 79 is provided with means 17 that comprise a plurality of individually adjustable shoes 80 that are swivelly carried on ball joints 81 by adjustable screw plugs 82. It will be evident that said means 17, when adjusted according to the outer contours of the store, hold said store steady on its hooks.
Each ejector piston 18 is provided with a piston part 83 that fits the cylinder bore 75, and a ram part 84 that extends through the open end 77 of the housing 74 and is guided at said end in a bearing 85 carried by the housing. In this case, the piston 18 is shown as lower end and as provided in the hollow thereof with an adjustable foot 86. The drawings clearly show that said foot may be retracted or extended, as desired, so the same firmly bears against a store while the piston is in its retracted position. Since the pistons 18 are projected to cause ejection of a store from the rack by pushing against said store and because the forces involved are quite great, as above mentioned, it is important to have the foot in contact with the store to prevent shock or damage, as may be caused by a piston that has a percussive impact rather than a pushing effort on the store.
The gas released into pipes 36 project the pistons 18. Since it is essential to control the ejection angle of the store to obviate damage or failure during ejection, one or both units 16 may be provided with the means 19 for varying the ejection pressures reaching the ejection piston 18 of one unit 16 with respect to that of the piston of the other unit. In this instance, the means 19 is shown as a fitting 86 that is disposed across a passage 87 in the housing end 76 and which receives gases under pressure from the pipe 36. Said fitting is provided with an orifice 8 8 that is smaller than the passage 87, the size of said orifice lowering the fiow of gases from said passage 87 into the inlet 89 to the cylinder bore 75.
In the above manner, one piston may have a lesser operating pressure thereon than the other, or the pressures on the two pistons may be equalized. Thus, exact ejection control is afforded by the means 19.
While the foregoing specification illustrates and describes what I now contemplate to be the best mode of carrying out my invention, the construction is, of course, subject to modification without departing from the spirit and scope of my invention. Therefore, I do not desire to restrict the invention to the particular form of construction illustrated and described, but desire to cover all modifications that may fall within the scope of the appended claims.
Having thus described the invention, what is claimed and desired to be secured by Letters Patent is:
1. An explosively operated ejector rack comprising: a pair of single hook means to suspend a store at longitudinally spaced points; a single pivoted lever of inverted T form; rods pivotally connected between the ends of the cross head of said lever and said hooks; a fixed stop effective to prevent rotation of said lever through an angle, in one direction, greater than required to hold the hooks in locked position; resilient means urging said lever against said stop; at least two store ejector means operated by pressure gas; a pressure chamber adapted to receive explosive means; pressure gas operated means effective when operated to rotate said lever against the effort of said resilient means in a direction to move said hooks to released position; and conduits directly connecting said pressure chamber with said ejector means and said means rotating said lever to ensure simultaneous flow of pressure gas into, and operation of, said ejector means and means rotating said lever.
2. An explosively operated ejector rack as set forth in claim 1 and in addition comprising: fittings adapted to be placed in the conduits adjacent the point of delivery of pressure gas into the ejector means, each said fitting being provided with an orifice for the fiow of gas therethrough, said orifice being effective to lower the rate of flow of pressure gas into the ejector means sufiiciently to establish a required rate of flow of gas into one ejector means with respect to another of said means while not materially restricting said flow during a simultaneous operation of the hook releasing and ejector means.
3. An explosively operated ejector rack as set forth in claim 1 and in addition having safety stop means engaging against said inverted T shaped lever to prevent movement thereof in a direction to effect release of said hooks, said stop means comprising: a bell crank lever having one arm engaging against said T-shaped lever on the side opposite to said fixed stop; a solenoid having its core pivotally connected to the other arm of said lever, and resilient means acting normally to hold one arm of the bell crank lever against said inverted T lever, the energization of said solenoid being effective to move said one arm out of the path of movement of said in- References Cited in the file of this patent Verted T lever- UNITED STATES PATENTS 4. In a store-ejecting rack as set forth in claim 1, a pair of pivotal hooks for suspending a store and a second 2,822,207 Steinmetz at 1958 pair of pivotal hooks, a link connecting one hook of each 5 2,869,523 Murphy 201 1959 2,889,746 Glassrnan et a1. June 9, 1959 air with an ad'acent hook of the other air. p 1 p 2,937,899 Murphy May 24, 1960
US838288A 1959-09-04 1959-09-04 Store ejector rack Expired - Lifetime US3056623A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US838288A US3056623A (en) 1959-09-04 1959-09-04 Store ejector rack

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US838288A US3056623A (en) 1959-09-04 1959-09-04 Store ejector rack

Publications (1)

Publication Number Publication Date
US3056623A true US3056623A (en) 1962-10-02

Family

ID=25276736

Family Applications (1)

Application Number Title Priority Date Filing Date
US838288A Expired - Lifetime US3056623A (en) 1959-09-04 1959-09-04 Store ejector rack

Country Status (1)

Country Link
US (1) US3056623A (en)

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3266834A (en) * 1964-04-22 1966-08-16 Rocket Power Inc Store ejecting rack
US3273459A (en) * 1964-08-31 1966-09-20 Arthur R Lardin Launcher for stores
DE1506084B1 (en) * 1966-03-18 1972-05-31 Rocket Power Inc Holding and dropping device for loads on aircraft
FR2156425A1 (en) * 1971-10-18 1973-06-01 France Etat
FR2219871A1 (en) * 1973-03-05 1974-09-27 Ml Aviation Co Ltd
US3871604A (en) * 1972-11-02 1975-03-18 Pierre Fernand Coutin Retractable jettisoning ejector for aircrafts
US4043525A (en) * 1976-03-31 1977-08-23 Mcdonnell Douglas Corporation Variable orificing device
US4089250A (en) * 1977-02-24 1978-05-16 Mcdonnell Douglas Corporation Cartridge holder with extractor/indicator
US4129271A (en) * 1977-03-09 1978-12-12 R. Alkan & Cie Automatic hanging and wedging device for aircraft loads
US4183480A (en) * 1978-06-22 1980-01-15 Mcdonnell Douglas Corporation Automatic sway bracing rack
US4196879A (en) * 1977-02-15 1980-04-08 M.L. Aviation Company Limited Ejector release unit for airborne stores having lockable sway brace assembly
US4202576A (en) * 1977-12-30 1980-05-13 R. Alkan & Cie Device for locking to fixed supports loads carried under aircraft
US4318561A (en) * 1978-10-17 1982-03-09 R. Alkan & Cie Central-controlled devices for carrying and wedging loads under aircraft
US4355832A (en) * 1980-12-04 1982-10-26 The United States Of America As Represented By The Secretary Of The Air Force Load balancer for multiple loads
US4388853A (en) * 1980-07-24 1983-06-21 Frazer-Nash Limited Missile launchers
DE3446452A1 (en) 1984-12-20 1986-07-03 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for releasing and ejecting aircraft loads
DE3448201C2 (en) * 1984-12-20 1989-04-20 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Device for releasing and ejecting (launching) aircraft loads
US5685590A (en) * 1996-01-03 1997-11-11 The United States Of America As Represented By The Secretary Of The Navy Carriage for selectively and remote positively suspendingly engaging and disengaging a load in transporting same from one location to another
US5904323A (en) * 1997-04-28 1999-05-18 Mcdonnell Douglas Corporation Constrained store release system
US6119982A (en) * 1998-04-03 2000-09-19 Mcdonnell Douglas Corporation Pre-loaded stores ejection ram system and method
US6250195B1 (en) * 1999-11-09 2001-06-26 Northrop Grumman Corporation Compact universal ejection/rail launching system
EP0955236A3 (en) * 1998-05-07 2001-07-18 McDonnell Douglas Corporation Single hook ejector rack for miniature munitions
US20030107277A1 (en) * 2001-12-12 2003-06-12 Ruey-Shan Liu Weight release mechanism for underwater object
US20050279890A1 (en) * 2004-03-23 2005-12-22 Walter Holemans Latching separation system
US20070272800A1 (en) * 2004-04-04 2007-11-29 Ervin Edelstein Extendible Sway Brace For An Airborne Payload Rack And A Rack Containing Same
US7966921B1 (en) * 2009-04-01 2011-06-28 The United States Of America As Represented By The Secretary Of The Navy Aircraft wing-pylon interface mounting apparatus
US8127655B1 (en) * 2009-03-11 2012-03-06 Exelis, Inc. Low force bomb rack release mechanism
KR20160050374A (en) * 2014-10-29 2016-05-11 현대위아 주식회사 Weapn station
KR101621146B1 (en) * 2014-06-27 2016-05-13 이엠코리아주식회사 Weapn station
WO2016199132A1 (en) * 2015-06-11 2016-12-15 Israel Aerospace Industries Ltd. Rack

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2822207A (en) * 1953-11-20 1958-02-04 North American Aviation Inc Release ejector
US2869523A (en) * 1954-02-03 1959-01-20 Pastushin Aviat Corp Ejector release mechanism for auxiliary fuel tanks, and the like
US2889746A (en) * 1954-11-10 1959-06-09 Louis H Glassman Explosive bolt type store suspension system for aircraft
US2937899A (en) * 1956-03-08 1960-05-24 Pastushin Aviat Corp Synchronously operated ejector guns for translating a store away from an airborne vehicle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2822207A (en) * 1953-11-20 1958-02-04 North American Aviation Inc Release ejector
US2869523A (en) * 1954-02-03 1959-01-20 Pastushin Aviat Corp Ejector release mechanism for auxiliary fuel tanks, and the like
US2889746A (en) * 1954-11-10 1959-06-09 Louis H Glassman Explosive bolt type store suspension system for aircraft
US2937899A (en) * 1956-03-08 1960-05-24 Pastushin Aviat Corp Synchronously operated ejector guns for translating a store away from an airborne vehicle

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3266834A (en) * 1964-04-22 1966-08-16 Rocket Power Inc Store ejecting rack
US3273459A (en) * 1964-08-31 1966-09-20 Arthur R Lardin Launcher for stores
DE1506084B1 (en) * 1966-03-18 1972-05-31 Rocket Power Inc Holding and dropping device for loads on aircraft
FR2156425A1 (en) * 1971-10-18 1973-06-01 France Etat
US3871604A (en) * 1972-11-02 1975-03-18 Pierre Fernand Coutin Retractable jettisoning ejector for aircrafts
FR2219871A1 (en) * 1973-03-05 1974-09-27 Ml Aviation Co Ltd
US3898909A (en) * 1973-03-05 1975-08-12 Ml Aviation Co Ltd Ejector release unit for use in aircraft
US4043525A (en) * 1976-03-31 1977-08-23 Mcdonnell Douglas Corporation Variable orificing device
US4196879A (en) * 1977-02-15 1980-04-08 M.L. Aviation Company Limited Ejector release unit for airborne stores having lockable sway brace assembly
US4089250A (en) * 1977-02-24 1978-05-16 Mcdonnell Douglas Corporation Cartridge holder with extractor/indicator
US4129271A (en) * 1977-03-09 1978-12-12 R. Alkan & Cie Automatic hanging and wedging device for aircraft loads
US4202576A (en) * 1977-12-30 1980-05-13 R. Alkan & Cie Device for locking to fixed supports loads carried under aircraft
US4183480A (en) * 1978-06-22 1980-01-15 Mcdonnell Douglas Corporation Automatic sway bracing rack
US4318561A (en) * 1978-10-17 1982-03-09 R. Alkan & Cie Central-controlled devices for carrying and wedging loads under aircraft
US4388853A (en) * 1980-07-24 1983-06-21 Frazer-Nash Limited Missile launchers
US4355832A (en) * 1980-12-04 1982-10-26 The United States Of America As Represented By The Secretary Of The Air Force Load balancer for multiple loads
DE3446452A1 (en) 1984-12-20 1986-07-03 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for releasing and ejecting aircraft loads
DE3448201C2 (en) * 1984-12-20 1989-04-20 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Device for releasing and ejecting (launching) aircraft loads
US5685590A (en) * 1996-01-03 1997-11-11 The United States Of America As Represented By The Secretary Of The Navy Carriage for selectively and remote positively suspendingly engaging and disengaging a load in transporting same from one location to another
US5904323A (en) * 1997-04-28 1999-05-18 Mcdonnell Douglas Corporation Constrained store release system
US6119982A (en) * 1998-04-03 2000-09-19 Mcdonnell Douglas Corporation Pre-loaded stores ejection ram system and method
EP0955236A3 (en) * 1998-05-07 2001-07-18 McDonnell Douglas Corporation Single hook ejector rack for miniature munitions
US6250195B1 (en) * 1999-11-09 2001-06-26 Northrop Grumman Corporation Compact universal ejection/rail launching system
US20030107277A1 (en) * 2001-12-12 2003-06-12 Ruey-Shan Liu Weight release mechanism for underwater object
US6670735B2 (en) * 2001-12-12 2003-12-30 Chung-Shan Institute Of Science And Technology Weight release mechanism for underwater object
US20050279890A1 (en) * 2004-03-23 2005-12-22 Walter Holemans Latching separation system
US7861976B2 (en) 2004-03-23 2011-01-04 Planetary Systems Corporation Latching separation system
US20070272800A1 (en) * 2004-04-04 2007-11-29 Ervin Edelstein Extendible Sway Brace For An Airborne Payload Rack And A Rack Containing Same
US8196866B2 (en) * 2004-04-04 2012-06-12 Israel Aerospace Industries Ltd. Extendible sway brace for an airborne payload rack and a rack containing same
US8127655B1 (en) * 2009-03-11 2012-03-06 Exelis, Inc. Low force bomb rack release mechanism
US7966921B1 (en) * 2009-04-01 2011-06-28 The United States Of America As Represented By The Secretary Of The Navy Aircraft wing-pylon interface mounting apparatus
KR101621146B1 (en) * 2014-06-27 2016-05-13 이엠코리아주식회사 Weapn station
KR20160050374A (en) * 2014-10-29 2016-05-11 현대위아 주식회사 Weapn station
WO2016199132A1 (en) * 2015-06-11 2016-12-15 Israel Aerospace Industries Ltd. Rack

Similar Documents

Publication Publication Date Title
US3056623A (en) Store ejector rack
US1235076A (en) Torpedo-guard.
US3610094A (en) Ejector release units for use in aircraft
US4008645A (en) Aircraft supported launchable weapon release assembly
US3597919A (en) Linear gas generator actuated latching and thrusting device
US3037805A (en) Store supporting and ejecting assembly for aircraft
US2393627A (en) Actuating mechanism for gas operated firearms
US2930288A (en) Tandem rocket launcher and firing system
US3598341A (en) Aircraft store carrier
US3487445A (en) Power actuated gyro controlled ejection seat stabilizing system
US3059956A (en) Combined shackle and ejector mechanism for stores
US2400322A (en) Flare pistol installation
US2937899A (en) Synchronously operated ejector guns for translating a store away from an airborne vehicle
US3898909A (en) Ejector release unit for use in aircraft
US1272421A (en) Apparatus for throwing projectiles.
US2410848A (en) Multiple barrel machine gun
GB1088571A (en) Improvements in or relating to combined ejector and release devices for aircraft stores
US3153980A (en) Retractable missile shoes
US2764914A (en) Apparatus for cooling gun barrels
US1734501A (en) Gun
GB1449681A (en) Ejection release unit for use in aircraft
US3027809A (en) Recoilless rifle
US1291690A (en) Gas-operated gun.
US2925754A (en) Single hook bomb release and ejector
US2853975A (en) Actuator for unlocking and removing aircraft canopy