GB562371A - Improvements in or relating to air brakes for aircraft - Google Patents
Improvements in or relating to air brakes for aircraftInfo
- Publication number
- GB562371A GB562371A GB922042A GB922042A GB562371A GB 562371 A GB562371 A GB 562371A GB 922042 A GB922042 A GB 922042A GB 922042 A GB922042 A GB 922042A GB 562371 A GB562371 A GB 562371A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- venturi
- flaps
- tube
- lowered
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
- B64C9/323—Air braking surfaces associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/32—Air braking surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Of Braking Force In Braking Systems (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Abstract
562,371. Coutrolling aircraft. FAIREY AVIATION CO., Ltd., and YOUNGMAN, R. T. July 3, 1942, No. 9220. [Class 4] An aircraft having an air brake of the kind described in Specification 562,365, wherein a flap is adapted to be projected into or withdrawn from the airstream by a bellows device in communication with the throat of a venturi-tube fitted with a butterfly valve, has a pipe g from a venturi-tube f connected to the front end of a second venturi-tube, the throat of which is connected by a pipe to a bellows device for actuating a flap a, while another passage n leads from the rear end of the second venturitube to a bellows device for actuating a second flap c opposite to the first flap. A butterfly valve 12 in the venturi-tube f enables the bellows devices to be put under pressure or suction at will. The two flaps a, c may, as shown, be mounted above and below the trailing portion of a wing and the lower flap c may be on an auxiliary surface d normally nested within a recess beneath the wing and adapted to' be lowered as described in Specifications 461,157, 467,465 or 493,391. A soft rubber ring m normally seals the joint between the passage n and the second venturi-tube and when the surface d is lowered the joint is broken and the two flaps a, c are withdrawn to inoperative position. Alternatively, the passage n may have a flexible connection to the second venturitube so that both flaps a, c may be kept projected if required. To prevent unequal movement of the flaps they are connected by cables p, q, Fig. 5, to two spring-urged slides r, s of insulating material carrying contacts v, w. Should the movements be unequal, the circuit of a solenoid x is closed to cause its armature y to open the butterfly valve 12 and retract both flaps, for which purpose the armature is linked to the control lever 11 which actuates the valve 12. Alternatively, the slides r, s may actuate hydraulic or pneumatic valves controlling a jack device for moving the lever 11. The cable q in the case of a flap on the movable surface d, is led alongside one of the links by which the surface is raised and lowered.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB922042A GB562371A (en) | 1942-07-03 | 1942-07-03 | Improvements in or relating to air brakes for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB922042A GB562371A (en) | 1942-07-03 | 1942-07-03 | Improvements in or relating to air brakes for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB562371A true GB562371A (en) | 1944-06-29 |
Family
ID=9867727
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB922042A Expired GB562371A (en) | 1942-07-03 | 1942-07-03 | Improvements in or relating to air brakes for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB562371A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8511620B2 (en) | 2009-02-18 | 2013-08-20 | Airbus Operations Limited | Aircraft wing load alleviation system |
-
1942
- 1942-07-03 GB GB922042A patent/GB562371A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8511620B2 (en) | 2009-02-18 | 2013-08-20 | Airbus Operations Limited | Aircraft wing load alleviation system |
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