GB511153A - Novel or improved means for controlling the operation of brakes on aircraft - Google Patents
Novel or improved means for controlling the operation of brakes on aircraftInfo
- Publication number
- GB511153A GB511153A GB431338A GB431338A GB511153A GB 511153 A GB511153 A GB 511153A GB 431338 A GB431338 A GB 431338A GB 431338 A GB431338 A GB 431338A GB 511153 A GB511153 A GB 511153A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- brakes
- pin
- detent
- screw
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
Abstract
511,153. Control mechanism for brakes. DUNLOP RUBBER CO., Ltd., BEHARRELL, G. E., WRIGHT, J., and TREVASKIS, H. Feb. 11, 1938, No. 4313. [Class 136 (i)] [Also in Groups XXIV and XXXIII] Means for controlling the operation of brakes on aircraft include a manually-operated pivoted lever provided with adjustable means adapted to co-act with a fixed stop for determining the angular movement of the lever, and a pivoted detent or catch for holding the lever at the limit of its angular movement. In the construction shown, a lever 1 is pivotally mounted on a pin 2 fixed to a ring handle 3 provided on a flying control column 4. The lever has two lugs, one having the brake cable 6 secured thereto, the other being apertured to receive a grub screw 5. The cable 6 passes through a sleeve 7 integral with the handle 3 and carrying a pin 9 on which a detent 8 is pivotally mounted. When the lever 1 is moved to tension the cable 6, the screw 5 contacts with a sleeve 7a on the pin 9. The lever is locked in position by means of the detent 8 which is moved so that the surface 10 is behind the rear end of the screw 5. The extent of movement of the lever 1 is determined by the position of the grub screw within the aperture in the lug 1a.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB431338A GB511153A (en) | 1938-02-11 | 1938-02-11 | Novel or improved means for controlling the operation of brakes on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB431338A GB511153A (en) | 1938-02-11 | 1938-02-11 | Novel or improved means for controlling the operation of brakes on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB511153A true GB511153A (en) | 1939-08-11 |
Family
ID=9774810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB431338A Expired GB511153A (en) | 1938-02-11 | 1938-02-11 | Novel or improved means for controlling the operation of brakes on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB511153A (en) |
-
1938
- 1938-02-11 GB GB431338A patent/GB511153A/en not_active Expired
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