GB709340A - Improvements in and relating to aircraft undercarriages - Google Patents
Improvements in and relating to aircraft undercarriagesInfo
- Publication number
- GB709340A GB709340A GB5981/51A GB598151A GB709340A GB 709340 A GB709340 A GB 709340A GB 5981/51 A GB5981/51 A GB 5981/51A GB 598151 A GB598151 A GB 598151A GB 709340 A GB709340 A GB 709340A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- unit
- piston
- valve
- liquid
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
709,340. Hydro-pneumatic shock-absorbers. BOULTON PAUL AIRCRAFT, Ltd. March 12, 1952 [March 13, 1951J, No. 5981/51. Class 108(3) A wheel-mounting unit for an aircraft t undercarriage comprises a combination of cantilever and articulated type units in which the normally-fixed member of one unit constitutes or carries the movable member of the other unit. In the construction 'shown in Fig. 2, the articulated unit comprises a cylinder 1 in which a piston 18 works. The piston rod 19 is linked to an intermediate point of an arm 15 which carries the aircraft wheel (not shown) at one end, and is fulcrummed at 16 to a bracket 14 rigid with the cylinder I. Liquid in the cylinder 1 is displaced by upward piston movement, through a valvecontrolled orifice 21 to displace a floating piston 22 against air pressure in the hollow piston rod. The cantilever unit is formed by the cylinder 1 and an outer cylinder 2. A head 4 on the cylinder 1 acts on liquid 8 and displaces it through an orifice n and a valve 13 to act on a floating piston 23 loaded by air pressure in an extension 60 of the cylinder 1. The valve 13 may be a valve of the kind described in Specification 707,970, [Group XXIX], and maintains a constant pressure across itself. In a modification, Fig. 1 (not shown), extension 60 is solid and carries a piston which has merely a dashpot action in the liquid 8. This piston may have an orifice, or controlled leakage may occur around its periphery. It also has a valve corresponding to the valve 13 of Fig. 2. In the construction shown in Fig. 3, the liquid space of both articulated and cantilever units are in communication tnrough orifices 110, and this liquid acts on a single floating piston 22. The leverage of the arm 15 and the ratio of areas of the pistons 4, 18 may be selected to cause closing of the articulated unit before the cantilever unit, or vice versa. Air may be charged into the hollow piston rod 19 through a valve which is slidable in a slot in the cylinder 1. A liquid-spring unit may be used instead of the hydro-pneumatic arrangements described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5981/51A GB709340A (en) | 1951-03-13 | 1951-03-13 | Improvements in and relating to aircraft undercarriages |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5981/51A GB709340A (en) | 1951-03-13 | 1951-03-13 | Improvements in and relating to aircraft undercarriages |
Publications (1)
Publication Number | Publication Date |
---|---|
GB709340A true GB709340A (en) | 1954-05-19 |
Family
ID=9806218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5981/51A Expired GB709340A (en) | 1951-03-13 | 1951-03-13 | Improvements in and relating to aircraft undercarriages |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB709340A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1117396B (en) * | 1960-03-30 | 1961-11-16 | Cleveland Pneumatic Ind Inc | Landing gear for airplanes with shock absorbing means |
US3112102A (en) * | 1961-11-02 | 1963-11-26 | Messerschmitt Ag | Telescopic strut |
US3290038A (en) * | 1965-01-14 | 1966-12-06 | Bendix Corp | Extensible shock absorber |
FR2598676A1 (en) * | 1986-05-13 | 1987-11-20 | Messier Hispano Sa | AIRCRAFT TILLER WITH TILTING BEAM AND REDUCED SIZE |
GB2220462A (en) * | 1988-07-02 | 1990-01-10 | British Petroleum Co Plc | Apparatus and method for landing and retrieval of subsea modules |
-
1951
- 1951-03-13 GB GB5981/51A patent/GB709340A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1117396B (en) * | 1960-03-30 | 1961-11-16 | Cleveland Pneumatic Ind Inc | Landing gear for airplanes with shock absorbing means |
US3112102A (en) * | 1961-11-02 | 1963-11-26 | Messerschmitt Ag | Telescopic strut |
US3290038A (en) * | 1965-01-14 | 1966-12-06 | Bendix Corp | Extensible shock absorber |
FR2598676A1 (en) * | 1986-05-13 | 1987-11-20 | Messier Hispano Sa | AIRCRAFT TILLER WITH TILTING BEAM AND REDUCED SIZE |
EP0246949A1 (en) * | 1986-05-13 | 1987-11-25 | Messier-Hispano-Bugatti (S.A) | Aircraft landing gear provided with a swivelling beam and having small overall dimensions |
US4749152A (en) * | 1986-05-13 | 1988-06-07 | Messier-Hispano-Bugatti | Aircraft undercarriage of tilting-beam type and of reduced bulk |
GB2220462A (en) * | 1988-07-02 | 1990-01-10 | British Petroleum Co Plc | Apparatus and method for landing and retrieval of subsea modules |
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