GB537234A - Improvements in closure devices for storage compartments of aircraft - Google Patents
Improvements in closure devices for storage compartments of aircraftInfo
- Publication number
- GB537234A GB537234A GB3196339A GB3196339A GB537234A GB 537234 A GB537234 A GB 537234A GB 3196339 A GB3196339 A GB 3196339A GB 3196339 A GB3196339 A GB 3196339A GB 537234 A GB537234 A GB 537234A
- Authority
- GB
- United Kingdom
- Prior art keywords
- closure
- aircraft
- compartment
- brackets
- pivot
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/16—Fairings movable in conjunction with undercarriage elements
Abstract
537,234. Bomb-dropging apparatus. GENERAL AIRCRAFT, Ltd., and LEATHER, G. B. Dec. 11, 1939, No. 31963. [Class 9 (ii)] [Also in Group XXXIII] A closure 7 for the stowage compartment 5 for a retractable undercarriage, bomb racks &c. in an aircraft is swingable about a pivot 8 within the aircraft structure so that the closure is within the structure when the compartment is in a fully open condition whereas it is able in the closed condition to seal the compartment effectively. The closure is suspended from laterally spaced pivots 8 by brackets 9 and is preferably operated by a remotely controllable jack 10 the plunger 12 of which is pivoted to an arm of one of the brackets 9. In the open condition, part of the closure 7<SP>1</SP> may be arranged to project below the aircraft so that the jack action is assisted in closure by the airflow over the skin 6. The pivot 8 may be arranged longitudinally to the structure so that the closure swings transversely thereto. The closure may be of interrupted drum form so as to provide a number of alternate openings and closed spaces. Specification 576,824, [Group XXXIII], is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3196339A GB537234A (en) | 1939-12-11 | 1939-12-11 | Improvements in closure devices for storage compartments of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3196339A GB537234A (en) | 1939-12-11 | 1939-12-11 | Improvements in closure devices for storage compartments of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB537234A true GB537234A (en) | 1941-06-13 |
Family
ID=10330988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3196339A Expired GB537234A (en) | 1939-12-11 | 1939-12-11 | Improvements in closure devices for storage compartments of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB537234A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2445235A (en) * | 1944-02-15 | 1948-07-13 | Joseph C Myers | Aircraft with blast or like tube and closure therefor |
WO2003089297A1 (en) * | 2002-04-19 | 2003-10-30 | Bae Systems Plc | Landing gear door assembly |
US7243880B2 (en) | 2002-06-19 | 2007-07-17 | Airbus Uk Limited | Landing gear door assembly |
FR2956645A1 (en) * | 2010-02-23 | 2011-08-26 | Airbus Operations Sas | Aerodynamic device for reduction of vibrations of rear trap doors of front landing gear of transport aircraft, has aerodynamic element formed arranged upstream of front trap door and deflecting flow of air on level of front landing gear |
-
1939
- 1939-12-11 GB GB3196339A patent/GB537234A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2445235A (en) * | 1944-02-15 | 1948-07-13 | Joseph C Myers | Aircraft with blast or like tube and closure therefor |
WO2003089297A1 (en) * | 2002-04-19 | 2003-10-30 | Bae Systems Plc | Landing gear door assembly |
US7287726B2 (en) | 2002-04-19 | 2007-10-30 | Airbus Uk Limited | Landing gear door assembly |
US7243880B2 (en) | 2002-06-19 | 2007-07-17 | Airbus Uk Limited | Landing gear door assembly |
FR2956645A1 (en) * | 2010-02-23 | 2011-08-26 | Airbus Operations Sas | Aerodynamic device for reduction of vibrations of rear trap doors of front landing gear of transport aircraft, has aerodynamic element formed arranged upstream of front trap door and deflecting flow of air on level of front landing gear |
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