GB462963A - Improvements in tail skids or tail wheels for aeroplanes - Google Patents
Improvements in tail skids or tail wheels for aeroplanesInfo
- Publication number
- GB462963A GB462963A GB30525/36A GB3052536A GB462963A GB 462963 A GB462963 A GB 462963A GB 30525/36 A GB30525/36 A GB 30525/36A GB 3052536 A GB3052536 A GB 3052536A GB 462963 A GB462963 A GB 462963A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tail
- pivoted
- aeroplanes
- skids
- wheels
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
- B64C2025/005—Tail skids for fuselage tail strike protection on tricycle landing gear aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
462,963. Aircraft alighting gear. SAULNIER, R. Nov. 9, 1936, No. 30525. Convention date, Nov. 9, 1935. [Class 4] An aeroplane tail wheel, roller, runner, or skid 1 is carried by a tube 2, mounted for rotation, but not axial movement, in collars 3, 4 pivoted, respectively, to levers 7, 13 which are pivoted to the aircraft structure ; a shockabsorber 11 is pivoted to the aircraft structure and to an extension of the lever 7. The shock-absorber may be connected between any point on or extension of the levers 7, 13 and the aircraft structure.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR462963X | 1935-11-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB462963A true GB462963A (en) | 1937-03-18 |
Family
ID=8901871
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30525/36A Expired GB462963A (en) | 1935-11-09 | 1936-11-09 | Improvements in tail skids or tail wheels for aeroplanes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB462963A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0001344A1 (en) * | 1977-09-21 | 1979-04-04 | Diafil International S.A. | Suspension for a wheeled vehicle |
FR2953197A1 (en) * | 2009-11-30 | 2011-06-03 | Eurocopter France | STAND FOR PROTECTING A STRUCTURAL ELEMENT OF AN AIRCRAFT, AIRCRAFT PROVIDED WITH SUCH A STAND, AND ANTI-TIPPING METHOD USED BY THE SAME |
US20150102165A1 (en) * | 2012-03-09 | 2015-04-16 | The Boeing Company | Method and apparatus for changing a deployed position for a tail skid assembly |
-
1936
- 1936-11-09 GB GB30525/36A patent/GB462963A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0001344A1 (en) * | 1977-09-21 | 1979-04-04 | Diafil International S.A. | Suspension for a wheeled vehicle |
FR2953197A1 (en) * | 2009-11-30 | 2011-06-03 | Eurocopter France | STAND FOR PROTECTING A STRUCTURAL ELEMENT OF AN AIRCRAFT, AIRCRAFT PROVIDED WITH SUCH A STAND, AND ANTI-TIPPING METHOD USED BY THE SAME |
EP2332831A1 (en) | 2009-11-30 | 2011-06-15 | Eurocopter | Tail skid for an aircraft, aircraft and method to avoid the tipping of the aircraft by the use of said tail skid |
US8430357B2 (en) | 2009-11-30 | 2013-04-30 | Eurocopter | Tail skid for protecting a structural element of an aircraft, an aircraft provided with such a tail skid, and an anti-overturning method implemented by said tail skid |
US20150102165A1 (en) * | 2012-03-09 | 2015-04-16 | The Boeing Company | Method and apparatus for changing a deployed position for a tail skid assembly |
US9248906B2 (en) * | 2012-03-09 | 2016-02-02 | The Boeing Company | Method and apparatus for changing a deployed position for a tail skid assembly |
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