GB787470A - Improvements in and relating to aircraft braking mechanism - Google Patents
Improvements in and relating to aircraft braking mechanismInfo
- Publication number
- GB787470A GB787470A GB298455A GB298455A GB787470A GB 787470 A GB787470 A GB 787470A GB 298455 A GB298455 A GB 298455A GB 298455 A GB298455 A GB 298455A GB 787470 A GB787470 A GB 787470A
- Authority
- GB
- United Kingdom
- Prior art keywords
- contact
- aircraft
- exerted
- pressure
- strut
- 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
Abstract
787,470. Aircraft brakes. DOWTY EQUIPMENT Ltd. May 31, 1956 [March 1, 1955], No. 2984/55. Class 103 (1). [Also in Group XXXIII] In an aircraft braking system of the type described in Specification 728,176, it has been found that if too great a pressure is exerted on the friction shoe 17, the force of contact of the wheels with the runway may be reduced to such an extent that it may be difficult to maintain directional control of the aircraft on landing. To avoid this condition the load exerted on the wheels is made to operate, through contraction of the strut 8, 9 and the deflection of torque links 11, 12 and link members 42, 43, a potentiometer 41, shown also in the circuit of Fig. 2. A further similar potentiometer 47 is operated in accordance with the pressure exerted by the pilot on his brake pedal. Thus according to the relation between the load carried by the strut 8, 9 and the pilot's pedal pressure, a contact 63 of a relay B will be moved to make operative either a contact 52 or a contact 56 to supply a relay A. Specification 694,059, [Group XXIX], also is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB298455A GB787470A (en) | 1955-03-01 | 1955-03-01 | Improvements in and relating to aircraft braking mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB298455A GB787470A (en) | 1955-03-01 | 1955-03-01 | Improvements in and relating to aircraft braking mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB787470A true GB787470A (en) | 1957-12-11 |
Family
ID=9749716
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB298455A Expired GB787470A (en) | 1955-03-01 | 1955-03-01 | Improvements in and relating to aircraft braking mechanism |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB787470A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9745054B2 (en) | 2014-09-04 | 2017-08-29 | Safran Landing Systems Uk Ltd | Aircraft landing gear assembly |
| CN117401205A (en) * | 2023-12-13 | 2024-01-16 | 西安天成益邦电子科技有限公司 | Unmanned aerial vehicle landing gear shock absorption structure and method |
-
1955
- 1955-03-01 GB GB298455A patent/GB787470A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9745054B2 (en) | 2014-09-04 | 2017-08-29 | Safran Landing Systems Uk Ltd | Aircraft landing gear assembly |
| CN117401205A (en) * | 2023-12-13 | 2024-01-16 | 西安天成益邦电子科技有限公司 | Unmanned aerial vehicle landing gear shock absorption structure and method |
| CN117401205B (en) * | 2023-12-13 | 2024-03-19 | 西安天成益邦电子科技有限公司 | Unmanned aerial vehicle landing gear shock absorption structure and method |
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