GB784930A - Bomb bays for aircraft - Google Patents
Bomb bays for aircraftInfo
- Publication number
- GB784930A GB784930A GB3368254A GB3368254A GB784930A GB 784930 A GB784930 A GB 784930A GB 3368254 A GB3368254 A GB 3368254A GB 3368254 A GB3368254 A GB 3368254A GB 784930 A GB784930 A GB 784930A
- Authority
- GB
- United Kingdom
- Prior art keywords
- platform
- aircraft
- missile
- bell
- underside
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
Abstract
784,930. Aircraft fuselages. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., SIR W. G. July 4, 1955 [Nov. 22, 1954], No. 33682/54. Class 4. An aircraft having a bay, for a bomb or other missile, with an opening along the underside which is normally closed by doors, is provided with a movable platform, adapted on its underside to support the missile, which can be lowered to a position in which the opening is substantially closed by the platform. Fig. 3 shows the platform and operating mechanism in the raised position (firm lines) and in the lowered position (dot-dash lines). The platform 12 is supported by four bell-crank levers 13 arranged in pairs, each pair having their short arms connected by a tie-rod 15 so that it may be operated by a single jack 16. Each long arm of a bell-crank is provided with a side thrust roller 18 to coact with the adjacent side of the aircraft frame to steady the platform during lowering, and in the fully lowered position the long arms are arranged to engage supporting stops 19. To support the platform 12 firmly in its upper position, pins 20 attached to the aircraft frame are engaged by angularly movable catches 21, Fig. 4, mounted on the platform. Each catch 21 is biased by a spring 23 to move to the unlocking position but is held in the locking position by a locking bolt 24 biased by a spring 26. The locking bolt 24 is withdrawn by a trip lever 25 which is actuated by the end 27 of the jack 16. Specification 784,929 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3368254A GB784930A (en) | 1954-11-22 | 1954-11-22 | Bomb bays for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3368254A GB784930A (en) | 1954-11-22 | 1954-11-22 | Bomb bays for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB784930A true GB784930A (en) | 1957-10-16 |
Family
ID=10356078
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3368254A Expired GB784930A (en) | 1954-11-22 | 1954-11-22 | Bomb bays for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB784930A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0499749A1 (en) * | 1991-02-19 | 1992-08-26 | Teleflex Incorporated | Ordnance ejector system for an aircraft |
WO2017017335A1 (en) * | 2015-07-29 | 2017-02-02 | Alkan | Ejector guide device |
US9975635B2 (en) | 2014-01-06 | 2018-05-22 | Mbda Uk Limited | Structure for controlling the aero-acoustic environment in an aircraft weapons bay |
-
1954
- 1954-11-22 GB GB3368254A patent/GB784930A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0499749A1 (en) * | 1991-02-19 | 1992-08-26 | Teleflex Incorporated | Ordnance ejector system for an aircraft |
US9975635B2 (en) | 2014-01-06 | 2018-05-22 | Mbda Uk Limited | Structure for controlling the aero-acoustic environment in an aircraft weapons bay |
US10442534B1 (en) | 2014-01-06 | 2019-10-15 | Mbda Uk Limited | Structure for controlling the aero-acoustic environment in an aircraft weapons bay |
US11220336B2 (en) | 2014-01-06 | 2022-01-11 | Mbda Uk Limited | Structure for controlling the aero-acoustic environment in an aircraft weapons bay |
WO2017017335A1 (en) * | 2015-07-29 | 2017-02-02 | Alkan | Ejector guide device |
FR3039507A1 (en) * | 2015-07-29 | 2017-02-03 | Alkan | GUIDING DEVICE FOR EJECTOR |
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