GB941683A - Ejection of airmen from aircraft - Google Patents
Ejection of airmen from aircraftInfo
- Publication number
- GB941683A GB941683A GB232961A GB232961A GB941683A GB 941683 A GB941683 A GB 941683A GB 232961 A GB232961 A GB 232961A GB 232961 A GB232961 A GB 232961A GB 941683 A GB941683 A GB 941683A
- Authority
- GB
- United Kingdom
- Prior art keywords
- seat
- rocket motor
- aircraft
- ejection
- canisters
- 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
Links
- 239000007789 gas Substances 0.000 abstract 2
- 238000010304 firing Methods 0.000 abstract 1
- 230000005484 gravity Effects 0.000 abstract 1
Classifications
-
- 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
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/10—Ejector seats
Landscapes
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
941,683. Aircraft ejection seats. J. MARTIN. Jan. 17, 1962 [Jan. 20, 1961], No. 2329/61. Heading B7G. [Also in Division F3] Means for ejecting a seat from an aircraft comprises a gun for effecting initial ejection of the seat in a predetermined direction relatively to the aircraft, a primary rocket motor independent of the gun for accelerating the seat in the same direction, having a thrust passing through or near the centre of gravity of the seat and occupant, and an auxiliary rocket motor for producing a thrust in a direction such as to affect the flight path of the seat. The apparatus is as described in Specification 920,545, with the addition of the auxiliary rocket motor. In Fig. 2, two (or any number of) canisters 25 are screwed to bosses on the rocket motor pack spine 4, each containing a charge 38 and having a nozzle 27, ignition being by hot gases from a cartridge 30 detonated by a firing pin 34 on a piston 33 impelled against the cartridge by the gases in the spine against a biasing spring 36. The resulting thrust may compensate for a pitching moment occurring on ejection. The canisters 7 and 25 may extend on one side only of the spine. In Fig. 8, two canisters 7e with a nozzle 58 are mounted on the rear upper portion of the seat frame. One canister contains a detonator cartridge, and the nozzle may be adjustable in direction. Specifications 583,257, 640,520, 652,131, 711,234 and 843,269 also are referred to.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB232961A GB941683A (en) | 1961-01-20 | 1961-01-20 | Ejection of airmen from aircraft |
BE612857A BE612857A (en) | 1961-01-20 | 1962-01-19 | Improvements made to devices for ejecting a mass from a machine. |
CH66262A CH393102A (en) | 1961-01-20 | 1962-01-19 | Ejection seat for aircraft or other fast moving missiles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB232961A GB941683A (en) | 1961-01-20 | 1961-01-20 | Ejection of airmen from aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB941683A true GB941683A (en) | 1963-11-13 |
Family
ID=9737625
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB232961A Expired GB941683A (en) | 1961-01-20 | 1961-01-20 | Ejection of airmen from aircraft |
Country Status (3)
Country | Link |
---|---|
BE (1) | BE612857A (en) |
CH (1) | CH393102A (en) |
GB (1) | GB941683A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0132449A1 (en) * | 1983-07-25 | 1985-02-13 | Engineering Patents & Equipment Limited | Aircraft ejection system |
US4613100A (en) * | 1983-08-11 | 1986-09-23 | Engineering Patents & Equipment Limited | Aircraft ejection system |
GB2253597A (en) * | 1991-03-12 | 1992-09-16 | Mashinostroitelny Z Zvezda | Method for ejection of crew member from flying vehicle, and ejection seat to implement it |
-
1961
- 1961-01-20 GB GB232961A patent/GB941683A/en not_active Expired
-
1962
- 1962-01-19 CH CH66262A patent/CH393102A/en unknown
- 1962-01-19 BE BE612857A patent/BE612857A/en unknown
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0132449A1 (en) * | 1983-07-25 | 1985-02-13 | Engineering Patents & Equipment Limited | Aircraft ejection system |
US4613100A (en) * | 1983-08-11 | 1986-09-23 | Engineering Patents & Equipment Limited | Aircraft ejection system |
GB2253597A (en) * | 1991-03-12 | 1992-09-16 | Mashinostroitelny Z Zvezda | Method for ejection of crew member from flying vehicle, and ejection seat to implement it |
Also Published As
Publication number | Publication date |
---|---|
CH393102A (en) | 1965-05-31 |
BE612857A (en) | 1962-05-16 |
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