GB811300A - Braking system for aircraft - Google Patents
Braking system for aircraftInfo
- Publication number
- GB811300A GB811300A GB1567455A GB1567455A GB811300A GB 811300 A GB811300 A GB 811300A GB 1567455 A GB1567455 A GB 1567455A GB 1567455 A GB1567455 A GB 1567455A GB 811300 A GB811300 A GB 811300A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pressure
- brakes
- rudder bar
- cable
- fluid
- 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
- B64C25/48—Actuating mechanisms differentially operated for steering purposes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
811,300. Aircraft wheel brakes. DUNLOP RUBBER CO. Ltd. May 11, 1956 [June 1, 1955], No. 15674/55. Class 4. An aircraft fluid pressure operated braking system comprises an angularly movable rudder bar, mechanism connected to a source of pressure fluid and operable differentially to vary the volume of pressure-fluid flowing to port and starboard brakes respectively, in accordance with the degree of angular movement of the rudder bar, and means on the rudder bar for controlling the flow of pressure fluid through the mechanism to the brakes. In Fig. 1, the rudder bar 1 is secured at 2 to a vertical spindle 3, and has at each end a foot rest 14 Fig. 2, to which is secured a plate 16a supporting bracket 22. The rest 14 is apertured to receive a foot piston 17 sliding in plate 16a and biased by a spring 18. Depression of the piston 17 rocks a lever 21 pivoted to bracket 22 and pulls on a cable 24. The cables from each end of the rudder bar are joined at a junction member 25, Fig. 1, connected by a cable 26 to a valve mechanism 9, so that operation of either or both pistons 17 pulls cable 26, to increase the pressure in the port and starboard brakes equally. An arm 5 on spindle 3 is connected by link 7 to an arm 8 on the valve mechanism 9, operation of which varies the pressure of the two brakes differentially. Specification 720,178 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1567455A GB811300A (en) | 1955-06-01 | 1955-06-01 | Braking system for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1567455A GB811300A (en) | 1955-06-01 | 1955-06-01 | Braking system for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB811300A true GB811300A (en) | 1959-04-02 |
Family
ID=10063380
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1567455A Expired GB811300A (en) | 1955-06-01 | 1955-06-01 | Braking system for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB811300A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3178961A (en) * | 1961-07-08 | 1965-04-20 | Girling Ltd | Dual pedal actuating mechanism |
FR2371725A1 (en) * | 1976-11-17 | 1978-06-16 | Messerschmitt Boelkow Blohm | AUTOMATIC STEERING STABILIZATION DEVICE FOR RUNNING AIRCRAFT |
US9604720B2 (en) | 2009-04-30 | 2017-03-28 | Goodrich Corporation | Differential emergency/park electric brake system |
-
1955
- 1955-06-01 GB GB1567455A patent/GB811300A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3178961A (en) * | 1961-07-08 | 1965-04-20 | Girling Ltd | Dual pedal actuating mechanism |
FR2371725A1 (en) * | 1976-11-17 | 1978-06-16 | Messerschmitt Boelkow Blohm | AUTOMATIC STEERING STABILIZATION DEVICE FOR RUNNING AIRCRAFT |
US9604720B2 (en) | 2009-04-30 | 2017-03-28 | Goodrich Corporation | Differential emergency/park electric brake system |
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