GB601718A - Ejecting mechanism for safely launching an escaping occupant from an aeroplane - Google Patents
Ejecting mechanism for safely launching an escaping occupant from an aeroplaneInfo
- Publication number
- GB601718A GB601718A GB1610746A GB1610746A GB601718A GB 601718 A GB601718 A GB 601718A GB 1610746 A GB1610746 A GB 1610746A GB 1610746 A GB1610746 A GB 1610746A GB 601718 A GB601718 A GB 601718A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aeroplane
- cable
- ejecting mechanism
- firing
- martin
- 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
- 238000010304 firing Methods 0.000 abstract 2
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)
- Portable Nailing Machines And Staplers (AREA)
Abstract
601,718. Breech mechanism. MARTIN, J., and MARTIN-BAKER AIRCRAFT CO., Ltd. May 28, 1946, No. 16107. Addition to 583,257, [Group XXXIII]. [Class 92 (ii)] [Also in Group XXXIII] Cartridge - firing mechanism is both cocked and released in a single action immediately before firing. The cable 22 when pulled, withdraws a sear, which by an incline 23 first lifts the firing-pin 9 to compress the spring 13 and is then pulled out of the slotted end of the pin to release it to be impelled by the spring. The pull to the cable may be given by an aeroplane pilot when drawing a faceblind over himself, the cable 22 being interconnected with the blind.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB601718A true GB601718A (en) | 1948-05-11 |
Family
ID=1732065
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1610746A Expired GB601718A (en) | 1946-05-28 | Ejecting mechanism for safely launching an escaping occupant from an aeroplane |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB601718A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2813546A (en) * | 1955-03-11 | 1957-11-19 | Bendix Aviat Corp | Quick release valve actuator |
-
1946
- 1946-05-28 GB GB1610746A patent/GB601718A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2813546A (en) * | 1955-03-11 | 1957-11-19 | Bendix Aviat Corp | Quick release valve actuator |
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