GB709340A - Improvements in and relating to aircraft undercarriages - Google Patents

Improvements in and relating to aircraft undercarriages

Info

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
Application number
GB5981/51A
Inventor
Peter Jack Palmer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boulton Paul Aircraft Ltd
Original Assignee
Boulton Paul Aircraft Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boulton Paul Aircraft Ltd filed Critical Boulton Paul Aircraft Ltd
Priority to GB5981/51A priority Critical patent/GB709340A/en
Publication of GB709340A publication Critical patent/GB709340A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60Oleo 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.
GB5981/51A 1951-03-13 1951-03-13 Improvements in and relating to aircraft undercarriages Expired GB709340A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (7)

* Cited by examiner, † Cited by third party
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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