GB565331A - Improvements in or relating to the control of swivelling tail wheels for aircraft - Google Patents
Improvements in or relating to the control of swivelling tail wheels for aircraftInfo
- Publication number
- GB565331A GB565331A GB7649/41A GB764941A GB565331A GB 565331 A GB565331 A GB 565331A GB 7649/41 A GB7649/41 A GB 7649/41A GB 764941 A GB764941 A GB 764941A GB 565331 A GB565331 A GB 565331A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spindle
- brake
- swivelling
- fixed
- aircraft
- 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
- B64C25/50—Steerable undercarriages; Shimmy-damping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
565,331. Aircraft tail wheels. FAIREY AVIATION CO., Ltd., CHAPLIN, H. E., and FORSTER, F. W. June 17, 1941, No. 7649. [Class 4] To prevent undue oscillation of a swivelling tail wheel, particularly when heavily loaded, the spindle c of the oleo leg c, d is acted upon by a brake applied by jointed links m, pq which connect the brake member to the fixed part d of the oleo leg so that the braking pressure is increased as the parts c, d telescope under load. For this purpose the link m is fixed to a spindle h, Fig. 3, having a bearing in a brake blockf, the ends of the spindle having eccentrics k engaging the ends of a brake band j. As the angle between the jointed links decreases, the block f and band are tightened on a drum e fixed to the spindle c. The link pq can telescope against the action of an enclosed spring should further telescoping movement of the spindle c take place after the brake is fully applied.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7649/41A GB565331A (en) | 1941-06-17 | 1941-06-17 | Improvements in or relating to the control of swivelling tail wheels for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7649/41A GB565331A (en) | 1941-06-17 | 1941-06-17 | Improvements in or relating to the control of swivelling tail wheels for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB565331A true GB565331A (en) | 1944-11-07 |
Family
ID=9837143
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7649/41A Expired GB565331A (en) | 1941-06-17 | 1941-06-17 | Improvements in or relating to the control of swivelling tail wheels for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB565331A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2690888A (en) * | 1950-07-19 | 1954-10-05 | Lockheed Aircraft Corp | Aircraft landing gear mechanism |
-
1941
- 1941-06-17 GB GB7649/41A patent/GB565331A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2690888A (en) * | 1950-07-19 | 1954-10-05 | Lockheed Aircraft Corp | Aircraft landing gear mechanism |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1006522A (en) | Retractable undercarriages for aircraft | |
GB1061296A (en) | Improvements relating to brakes | |
GB492179A (en) | Improvements in or relating to brake mechanism | |
GB565331A (en) | Improvements in or relating to the control of swivelling tail wheels for aircraft | |
GB619140A (en) | Improvements in or relating to a truck for rail-type vehicles | |
GB1131871A (en) | Device for raising one pair of wheels of a tandem axle suspension in lorry bogies | |
GB906848A (en) | A shock absorbing strut | |
US2555182A (en) | Airplane wheel brake | |
US2133531A (en) | Railway brake rigging | |
GB664548A (en) | Improvements in or relating to bogie undercarriages for aircraft | |
GB598636A (en) | Improvements in or relating to drum brake and stub-axle assemblies for vehicles | |
GB791101A (en) | Improvements in or relating to steering mechanism for aircraft nose wheels, or the like | |
GB623609A (en) | Improvements in brakes for railway vehicles | |
GB643636A (en) | Improvements relating to aircraft retractable undercarriages | |
GB901499A (en) | Self-contained brake arrangement | |
GB825332A (en) | Improvements in or relating to landing gear of aircraft | |
GB649753A (en) | Improvements relating to track braking devices | |
GB787470A (en) | Improvements in and relating to aircraft braking mechanism | |
GB259776A (en) | Improvements in or relating to shock absorbers | |
GB750598A (en) | Improvements in or relating to internal shoe-drum brakes | |
GB559817A (en) | Improvements in braking systems for use in conjunction with the landing wheels of aircraft | |
GB473768A (en) | Improvements relating to aircraft undercarriages | |
GB583963A (en) | Improvements in aircraft landing gear | |
GB621633A (en) | Improvements in tricycle undercarriages for aircraft | |
GB1104069A (en) | Improvements in or relating to aircraft landing gear |