GB471488A - Improved brake operating means for aircraft - Google Patents
Improved brake operating means for aircraftInfo
- Publication number
- GB471488A GB471488A GB644036A GB644036A GB471488A GB 471488 A GB471488 A GB 471488A GB 644036 A GB644036 A GB 644036A GB 644036 A GB644036 A GB 644036A GB 471488 A GB471488 A GB 471488A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- spring
- fluid
- additional
- pressure
- 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
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
- B64C25/44—Actuating mechanisms
- B64C25/46—Brake regulators for preventing skidding or aircraft somersaulting
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
471,488. Fluid - pressure brakes. FITT, G., and BARBER, P. M. March 3, 1936, No. 6440. [Class 103 (i)] [Also in Group XXXIII] Means for operating landing-wheel brakes for aircraft include a source of fluid under pressure from which branch two channels 18 19, leading, respectively, to a valve 29 adapted to be closed due to contact of a tail landing- member 21 with the ground and a valve 40 adapted to be closed by movement additional to the normal movement of a throttle control lever 23. As shown, the fluid is supplied through a water separator 12 from an electrically driven air compressor, the separator 12 includes a baffle 13 in a chamber 12 provided with a pressure release valve 14 and connected with a pressure gauge 16. The valve 29 is normally held open against a spring 30 by a plunger 28 contacting with a spring 33 on the tail-member 21 which is rotated about an axis 35 against the action of a spring 36 on contact with the ground. The conical valvemember 40 is disposed in a housing open to the atmosphere as at 42 and connected to the brake cylinders. The lever 23 works in a slot provided with a step 45 and an additional slot 45a to accommodate the additional travel. The brake shoes may be toggle-actuated through a manual control for parking.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB644036A GB471488A (en) | 1936-03-03 | 1936-03-03 | Improved brake operating means for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB644036A GB471488A (en) | 1936-03-03 | 1936-03-03 | Improved brake operating means for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB471488A true GB471488A (en) | 1937-09-03 |
Family
ID=9814520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB644036A Expired GB471488A (en) | 1936-03-03 | 1936-03-03 | Improved brake operating means for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB471488A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2777654A (en) * | 1953-08-25 | 1957-01-15 | Westinghouse Air Brake Co | Airplane brake control apparatus |
-
1936
- 1936-03-03 GB GB644036A patent/GB471488A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2777654A (en) * | 1953-08-25 | 1957-01-15 | Westinghouse Air Brake Co | Airplane brake control apparatus |
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