GB467415A - Improvements relating to undercarriages for aircraft - Google Patents
Improvements relating to undercarriages for aircraftInfo
- Publication number
- GB467415A GB467415A GB34513/35A GB3451335A GB467415A GB 467415 A GB467415 A GB 467415A GB 34513/35 A GB34513/35 A GB 34513/35A GB 3451335 A GB3451335 A GB 3451335A GB 467415 A GB467415 A GB 467415A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shock
- tubes
- guide
- tube
- leg
- 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
- B64C25/60—Oleo legs
-
- 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)
- Fluid-Damping Devices (AREA)
- Vibration Dampers (AREA)
Abstract
467,415. Shock-absorbers. DOWTY, G. H. Dec. 12, 1935, Nos. 34513 /35 and 17906 /36. [Class 108 (iii)] In an aircraft undercarriage of the kind in which alignment of a landing-wheel or equivalent in its appropriate track is maintainec by the torsional stiffness of a tele scopic, shock-absorbing leg carry ing the wheel &c., the leg consists of two telescopic structures, the landing-wheel &c. being carriec by one of the telescoping, tubular parts 7, 9 of one of the structures the other part 7 of which is secured to the aircraft, while the telescoping parts 14, 15 of the other structure are offset from those of the main structure anc act as a guide therefor. As showr the tubes 7, 9 are separatec by a spring 11 which absorbs the landing-shock and the parts 14, 15 comprise tubes rigidly secured to the tubes 7, 9 respec tively, at least at two points, by members 12, 13. The structure 14, 15 incorporates a hydraulic or pneumatic dashpot consisting of a rod 16 which passes through a plug 17 closing the upper end of the tube 15, and carries a piston 18 of smaller diameter than the internal diameter of the tube 15, relative longitudinal movement of the tubes 14, 15 being resisted by flow of fluid through the restricted annular passage around the piston 18. Either structure may act as a shock-absorber and/or as a fluid or friction damper. In a modification, the guide structure comprises a rod pivoted at its lower end to the tube 9 and slidable in a sleeve pivoted to the tube 7. In another construction, the guide structure, comprising telescoping tubes incorporating dampers and shock-absorbing means, is mounted inside the main structure. The guide may consist of a rod fixed to one part of the leg and having a cross-head engaging a slot in a plate fixed to the other part. When arranged outside the main structure, the guide may be hidden by a fairing. To afford increasing resistance to torsion proportionally with compression of the leg, the two structures may be arranged so as not to be parallel with one another.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34513/35A GB467415A (en) | 1935-12-12 | 1935-12-12 | Improvements relating to undercarriages for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34513/35A GB467415A (en) | 1935-12-12 | 1935-12-12 | Improvements relating to undercarriages for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB467415A true GB467415A (en) | 1937-06-14 |
Family
ID=10366583
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34513/35A Expired GB467415A (en) | 1935-12-12 | 1935-12-12 | Improvements relating to undercarriages for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB467415A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2487548A (en) * | 1947-04-11 | 1949-11-08 | Lockheed Aircraft Corp | Main landing gear |
-
1935
- 1935-12-12 GB GB34513/35A patent/GB467415A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2487548A (en) * | 1947-04-11 | 1949-11-08 | Lockheed Aircraft Corp | Main landing gear |
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