US2931299A - Impeller - Google Patents

Impeller Download PDF

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Publication number
US2931299A
US2931299A US639125A US63912557A US2931299A US 2931299 A US2931299 A US 2931299A US 639125 A US639125 A US 639125A US 63912557 A US63912557 A US 63912557A US 2931299 A US2931299 A US 2931299A
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United States
Prior art keywords
gas pressure
primer
housing
impeller
nipple
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Expired - Lifetime
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US639125A
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Henry A Sokolowski
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Individual
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Priority to US639125A priority Critical patent/US2931299A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • B64D25/08Ejecting or escaping means
    • B64D25/10Ejector seats

Definitions

  • an impeller that is, an electrically red device capable of generating enough gas pressure for driving a firing pin and actuating a cartridge responsive device especially such as are used on aircraft and elsewhere.
  • an impeller that is, an electrically red device capable of generating enough gas pressure for driving a firing pin and actuating a cartridge responsive device especially such as are used on aircraft and elsewhere.
  • One explosive may provide gas pressure for driving a firing pin to set off a cartridge actuated thruster for opening a canopy and another tiring pin for actuating a cartridge responsive catapult.
  • the rst explosive to be red may have its gas pressure transmitted through a flexible hose/or tubing to a subsequent cartridge actuated device.
  • a substantial length of hose may lower the ternperature as well as consume time for firing subsequent devices from a rst.
  • the desirability of electrically ring cartridges for actuation of many such devices is known.
  • eliminating tlexible tubing or hoses in transmitting gas pressure for initiating actuation of a cartridge responsive device it has been thought necessary to dismantle some of the catapults or thrusters or other devices and send them back to the factory for installation of the individually electrically fired equipment.
  • An object of this invention is to reduce the cost and save valuable time in making such conversion from gas pressure fired to electrically fired equipment for planes and enable the changeover to be accomplished economically and expeditiously in the iield without having to send any equipment back to the factory. Another object is to effect a slight saving in time of response and enable remote control of cartridge actuated devices to be performed from a greater distance.
  • the saine nipple to which a hose has been connected is still used for the admission of gas under pressure generated in response to the passage of an electric current.
  • an electrical connector leads into the main housing of a two-part impeller for generation of gas pressure.
  • a conductor leads to a second part of this invention called a primer housing in which is located a conductive charge, which generates suicient pressure to move the same firing pin used under the gas pressure system for setting off the cartridge for actuation of the catapult or the thruster for removal of the canopy or for other purposes.
  • Fig. 1 disclosesthe impeller of this invention connected to the nipple for propelling the firing pin there disclosed.
  • Fig. 2 shows the impeller of Fig. 1 in cross sectional and exploded view.
  • a block contains a firing pin 11 ice which is actuated by gas pressure within the space 12, such gas pressure being supplied through the nipple 13.
  • gas pressure has been supplied to the nipple 13 through hoses and the like.
  • the mpeller 14 of the present invention is attached to the nipple 13.
  • the irnpeller of Fig. 1 includes a primer housing 15, a main housing 16, and a connector 17.
  • the wires illustrated leading to the connector 17, one of them is grounded and the other leads to a conductor 18 as illustrated.
  • the conductor 18 leads through the main housing and makes contact with a primer 19 inclosed within a conductive housing 20 around it.
  • the primer material is of the sort constituting suicient resistance so that upon passage of a current through it, it becomes heated and ignited. Gas pressure from this ignited primer then enters the space 12 through the nipple 13 and actuates the ring pin 11 in the same manner that was accomplished previously by connected hose line.
  • the right side of the main housing 16 is provided with outside threads 21 which cooperate with inside threads illustrated on the connector 17.
  • the conductor 18 is long enough to extend through the hole in the wall 22 of the main housing 16l and yieldably engage the conductive housing 20 around the primer 19.
  • This conductor 18 is yieldably mounted by means of the spring illustrated so that its pressure is more nearly uniform than would be the case if no such spring were used.
  • Inside threads 23 on the main housing engage outside threads 24 on the primer housing.
  • Inside threads 25v on the primer housing 15 engage the threads on the outside of the nipple 13.

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  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Description

April 5, 1960 H. A. soKoLowsKl 2,931,299
IMPELLER Filed Feb. a, 1957 IN VEN TOR. HENRY A. SOKOLOWSKI Wawy/@WAM United States Patent O IMPELLER Henry A. Sokolowski, Philadelphia, Pa., assignor to the United States of America as represented by the Secretary of the Army Application February 8, 1957, Serial No. 639,125 1 Claim. (Cl. 102-70.2) (Granted under Title 35, U.S. Code (1952), see. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes without payment of any royalty thereon.
'I'his invention relates to an impeller, that is, an electrically red device capable of generating enough gas pressure for driving a firing pin and actuating a cartridge responsive device especially such as are used on aircraft and elsewhere. Heretofore, it has been a common practice to eject a pilot's seat by a catapult after opening a canopy on high-speed planes in response to one or more tired cartridges as a source of gas pressure. One explosive may provide gas pressure for driving a firing pin to set off a cartridge actuated thruster for opening a canopy and another tiring pin for actuating a cartridge responsive catapult. The rst explosive to be red may have its gas pressure transmitted through a flexible hose/or tubing to a subsequent cartridge actuated device. A substantial length of hose may lower the ternperature as well as consume time for firing subsequent devices from a rst. The desirability of electrically ring cartridges for actuation of many such devices is known. However, when a change is to be made, eliminating tlexible tubing or hoses in transmitting gas pressure for initiating actuation of a cartridge responsive device, it has been thought necessary to dismantle some of the catapults or thrusters or other devices and send them back to the factory for installation of the individually electrically fired equipment.
An object of this invention is to reduce the cost and save valuable time in making such conversion from gas pressure fired to electrically fired equipment for planes and enable the changeover to be accomplished economically and expeditiously in the iield without having to send any equipment back to the factory. Another object is to effect a slight saving in time of response and enable remote control of cartridge actuated devices to be performed from a greater distance.
According to this invention, the saine nipple to which a hose has been connected is still used for the admission of gas under pressure generated in response to the passage of an electric current. More specifically, an electrical connector leads into the main housing of a two-part impeller for generation of gas pressure. A conductor leads to a second part of this invention called a primer housing in which is located a conductive charge, which generates suicient pressure to move the same firing pin used under the gas pressure system for setting off the cartridge for actuation of the catapult or the thruster for removal of the canopy or for other purposes.
Referring to the drawing, Fig. 1 disclosesthe impeller of this invention connected to the nipple for propelling the firing pin there disclosed.
Fig. 2 shows the impeller of Fig. 1 in cross sectional and exploded view.
Referring to Fig. 1, a block contains a firing pin 11 ice which is actuated by gas pressure within the space 12, such gas pressure being supplied through the nipple 13. Under the prior art gas pressure has been supplied to the nipple 13 through hoses and the like. Under the present invention it is no longer necessary to send the apparatus illustrated back to a factory for conversion of this apparatus from gas tired to electrically tired equipment. Instead, the mpeller 14 of the present invention is attached to the nipple 13.
As shown in Fig.-2, the irnpeller of Fig. 1 includes a primer housing 15, a main housing 16, and a connector 17. The wires illustrated leading to the connector 17, one of them is grounded and the other leads to a conductor 18 as illustrated. When the parts are assembled the conductor 18 leads through the main housing and makes contact with a primer 19 inclosed within a conductive housing 20 around it. As is known in the art, the primer material is of the sort constituting suicient resistance so that upon passage of a current through it, it becomes heated and ignited. Gas pressure from this ignited primer then enters the space 12 through the nipple 13 and actuates the ring pin 11 in the same manner that was accomplished previously by connected hose line. The right side of the main housing 16 is provided with outside threads 21 which cooperate with inside threads illustrated on the connector 17. The conductor 18 is long enough to extend through the hole in the wall 22 of the main housing 16l and yieldably engage the conductive housing 20 around the primer 19. This conductor 18 is yieldably mounted by means of the spring illustrated so that its pressure is more nearly uniform than would be the case if no such spring were used. Inside threads 23 on the main housing engage outside threads 24 on the primer housing. Inside threads 25v on the primer housing 15 engage the threads on the outside of the nipple 13.
In operation current is supplied to the insulated conductor 18 within the connector 17. On contact with the wall 20a of the primer housing, current passes through the primer material 19 heating and igniting it. Gas pressure breaks down the frangible wall 26 allowing such pressure to actuate the firing pin 11. In heating the primer material current ows through such material 19 to the side walls 20 of the conductive housing. Such walls 20 are insulated from the wall 20a as shown. The side walls 20 are grounded to the primer housing 15, main housing 16, and the metallic connector 17 through which current flows in heating the conductive primer material 19.
Among the advantages of this invention may be mentioned the saving of time and cost of returning parts of a catapult or other cartridge actuated device to a factory for conversion from gas pressure to electric firing. The same nipple 13 is used and does not require changing from gas to electric ring. Electric tiring is better adapted for remote control of devices which are substantially separated in distance.
I claim: In combination with means forming a cylinder and ,a firing pin movable in said cylinder upon the applica- 3 said opening, laid afa'i'g'yildably urging Sad conluctor into contact with -said electrically r`insulated walL References Cited in the le of this patent UNITED STATES PATENTS 1,858,969 Ruhlemann May 17, 1932 I lJ4 Al1en`et `a`1. Nov. l7, 1933 ..Mil1er,et.a1. July Y24,195.1 Rockwell Nov. 13, 1951 Crawford ....'IaIL 20, 1959 FOREIGN PATENTS France Mar. 11, 1921
US639125A 1957-02-08 1957-02-08 Impeller Expired - Lifetime US2931299A (en)

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US639125A US2931299A (en) 1957-02-08 1957-02-08 Impeller

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3318244A (en) * 1965-07-01 1967-05-09 Charles E Rostocil Cartridge
US3475572A (en) * 1968-03-05 1969-10-28 Gen Electric Acceleration actuated switch with explosive charge and thermitic material
US3636879A (en) * 1969-11-06 1972-01-25 Avco Corp Airburst and inertia impact fuze assembly for munitions
US3779167A (en) * 1970-01-21 1973-12-18 Olin Corp Electrical initiator
US3905291A (en) * 1973-04-11 1975-09-16 Jr George T Corbin Cartridge-actuated device and launching assembly using same
US4286521A (en) * 1978-07-27 1981-09-01 Redon Trust Device actuated electrically to trigger a mechanical percussion detonator

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR521654A (en) * 1919-07-05 1921-07-18 Vickers Electrical Co Ltd Cartridge type electric rockets
US1575071A (en) * 1925-02-24 1926-03-02 Luman Avie John Door bolt
US1858969A (en) * 1926-06-26 1932-05-17 Rheinische Metallw & Maschf Electric fuse for projectiles
US1933694A (en) * 1930-04-30 1933-11-07 C O Two Fire Equipment Co Electrically controlled actuating device
US2561670A (en) * 1945-07-30 1951-07-24 Aerojet Engineering Corp Ignitor
US2869825A (en) * 1953-10-26 1959-01-20 Phillips Petroleum Co Earth boring

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR521654A (en) * 1919-07-05 1921-07-18 Vickers Electrical Co Ltd Cartridge type electric rockets
US1575071A (en) * 1925-02-24 1926-03-02 Luman Avie John Door bolt
US1858969A (en) * 1926-06-26 1932-05-17 Rheinische Metallw & Maschf Electric fuse for projectiles
US1933694A (en) * 1930-04-30 1933-11-07 C O Two Fire Equipment Co Electrically controlled actuating device
US2561670A (en) * 1945-07-30 1951-07-24 Aerojet Engineering Corp Ignitor
US2869825A (en) * 1953-10-26 1959-01-20 Phillips Petroleum Co Earth boring

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3318244A (en) * 1965-07-01 1967-05-09 Charles E Rostocil Cartridge
US3475572A (en) * 1968-03-05 1969-10-28 Gen Electric Acceleration actuated switch with explosive charge and thermitic material
US3636879A (en) * 1969-11-06 1972-01-25 Avco Corp Airburst and inertia impact fuze assembly for munitions
US3779167A (en) * 1970-01-21 1973-12-18 Olin Corp Electrical initiator
US3905291A (en) * 1973-04-11 1975-09-16 Jr George T Corbin Cartridge-actuated device and launching assembly using same
US4286521A (en) * 1978-07-27 1981-09-01 Redon Trust Device actuated electrically to trigger a mechanical percussion detonator

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