GB598990A - Improvements in damping devices applicable in particular as landing gears for aircraft and more especially light aircraft - Google Patents
Improvements in damping devices applicable in particular as landing gears for aircraft and more especially light aircraftInfo
- Publication number
- GB598990A GB598990A GB20930/45A GB2093045A GB598990A GB 598990 A GB598990 A GB 598990A GB 20930/45 A GB20930/45 A GB 20930/45A GB 2093045 A GB2093045 A GB 2093045A GB 598990 A GB598990 A GB 598990A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- landing
- lever
- elastic member
- skid
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
- Springs (AREA)
- Vibration Prevention Devices (AREA)
Abstract
598,990. Aircraft landing-gear. SOC. ANON. DES USINES CHAUSSON. Aug. 14, 1945. No. 20930. Convention date, May 24, 1944. [Class 4] A damping device applicable to an aircraft undercarriage comprises an elastic member set in tension by an inclined lever made to turn by the ground reaction to the vertical movement of the craft when landing so that the moment arm of the force applied to the elastic member increases with the angle of movement. An inclined arm 6 carrying a shoe 8 with a friction surface 9 sliding along a skid 2 produces torsion, under the ground pressure on the skid during landing, in a rubber annulus 4 connected between the lever pivot ring 5 and the aircraft body 1, The arrangement is such that the moment arm of the applied force increases with the angular movement imposed on the rubber annulus. Modifications in the arrangements of the arms and in the elastic members acted upon are described ; in one example, a spring acted upon by a bellcrank lever is employed.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR598990X | 1944-05-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB598990A true GB598990A (en) | 1948-03-02 |
Family
ID=8969287
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20930/45A Expired GB598990A (en) | 1944-05-24 | 1945-08-14 | Improvements in damping devices applicable in particular as landing gears for aircraft and more especially light aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB598990A (en) |
-
1945
- 1945-08-14 GB GB20930/45A patent/GB598990A/en not_active Expired
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