GB784929A - Closing doors for a bomb bay of an aircraft - Google Patents
Closing doors for a bomb bay of an aircraftInfo
- Publication number
- GB784929A GB784929A GB3368154A GB3368154A GB784929A GB 784929 A GB784929 A GB 784929A GB 3368154 A GB3368154 A GB 3368154A GB 3368154 A GB3368154 A GB 3368154A GB 784929 A GB784929 A GB 784929A
- Authority
- GB
- United Kingdom
- Prior art keywords
- doors
- bay
- door
- aircraft
- remote
- 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; ARRANGEMENT 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
Abstract
784,929. Aircraft fuselages. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., SIR, W. G. July 1, 1955 [Nov. 22, 1954], No. 33681/54. Class 4. In an aircraft provided with a bay, for a bomb or other missile, with an opening at the bottom which is closed by a pair of longitudinally-extending doors, the meeting edges of the doors are supported, both fore and aft of the bay, by levers movable angularly to open the doors, and the remote edges of the doors are guided so as initially to move to a position which is clear of the bay opening and then to slide up the outside of the body skin while the doors are being opened. Fig. 2 shows a crosssection of the bomb bay with the doors open. The meeting face of each door 13, 14 is connected at each end to the long arm of a bell crank lever 17, the short arm of which is connected, with lost motion, to the movable element of a jack 23. The remote edges of the doors may be supported between their ends as well as at their ends, e.g. at five places altogether. At each place of support the remote edge of a door carries a pin 27 adapted to ride in a cam slot 28 shaped so that the initial movement of the jacks will move the remote edge of the door just to the exterior of the body, whilst subsequent movement will cause the door to climb up closely adjacent the skin of the body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3368154A GB784929A (en) | 1954-11-22 | 1954-11-22 | Closing doors for a bomb bay of an aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3368154A GB784929A (en) | 1954-11-22 | 1954-11-22 | Closing doors for a bomb bay of an aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB784929A true GB784929A (en) | 1957-10-16 |
Family
ID=10356060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3368154A Expired GB784929A (en) | 1954-11-22 | 1954-11-22 | Closing doors for a bomb bay of an aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB784929A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3390846A (en) * | 1965-10-20 | 1968-07-02 | Canadian Patents Dev | Socket assembly for releasable device |
| FR3014836A1 (en) * | 2013-12-16 | 2015-06-19 | Airbus Operations Sas | DEVICE FOR OPENING OR CLOSING CONCOMITANTS OF TWO SHUTTERS OF A TRAPPER OF A LANDING TRAIN |
| US20170096223A1 (en) * | 2014-03-23 | 2017-04-06 | Israel Aerospace Industries Ltd. | Aircraft pylon |
| CN113815843A (en) * | 2021-10-27 | 2021-12-21 | 中国商用飞机有限责任公司 | Linkage mechanism for landing gear door and device for opening, closing and locking the door comprising the same |
| CN114313225A (en) * | 2022-01-27 | 2022-04-12 | 中国商用飞机有限责任公司 | Cabin door driving assembly, landing gear cabin door assembly and cabin door driving assembly design method |
| US11370543B2 (en) | 2014-03-23 | 2022-06-28 | Israel Aerospace Industries Ltd. | Aircraft pylon |
-
1954
- 1954-11-22 GB GB3368154A patent/GB784929A/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3390846A (en) * | 1965-10-20 | 1968-07-02 | Canadian Patents Dev | Socket assembly for releasable device |
| FR3014836A1 (en) * | 2013-12-16 | 2015-06-19 | Airbus Operations Sas | DEVICE FOR OPENING OR CLOSING CONCOMITANTS OF TWO SHUTTERS OF A TRAPPER OF A LANDING TRAIN |
| US9499258B2 (en) | 2013-12-16 | 2016-11-22 | Airbus Operations Sas | Device for concomitant opening or closing of two flaps of a landing gear door |
| US20170096223A1 (en) * | 2014-03-23 | 2017-04-06 | Israel Aerospace Industries Ltd. | Aircraft pylon |
| US11370543B2 (en) | 2014-03-23 | 2022-06-28 | Israel Aerospace Industries Ltd. | Aircraft pylon |
| CN113815843A (en) * | 2021-10-27 | 2021-12-21 | 中国商用飞机有限责任公司 | Linkage mechanism for landing gear door and device for opening, closing and locking the door comprising the same |
| CN113815843B (en) * | 2021-10-27 | 2022-07-05 | 中国商用飞机有限责任公司 | Linkage mechanism for landing gear door and device for opening, closing and locking the door comprising the same |
| CN114313225A (en) * | 2022-01-27 | 2022-04-12 | 中国商用飞机有限责任公司 | Cabin door driving assembly, landing gear cabin door assembly and cabin door driving assembly design method |
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