GB961644A - Aircraft landing gear - Google Patents

Aircraft landing gear

Info

Publication number
GB961644A
GB961644A GB36473/62A GB3647362A GB961644A GB 961644 A GB961644 A GB 961644A GB 36473/62 A GB36473/62 A GB 36473/62A GB 3647362 A GB3647362 A GB 3647362A GB 961644 A GB961644 A GB 961644A
Authority
GB
United Kingdom
Prior art keywords
sections
fixed
aircraft
cylinders
pistons
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
GB36473/62A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB36473/62A priority Critical patent/GB961644A/en
Publication of GB961644A publication Critical patent/GB961644A/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

961,644. Aircraft undercarriages. G. E. HORNSBY. Sept. 26, 1962, No. 36473/62. Heading B7G. An aircraft undercarriage includes two parallel rigid sections 15, 17, 18, 19, 20 mounted at 14, 16 to the aircraft wing or fuselage 10, a wheel 25 being positioned between these sections on an axle whose square section ends 23a are guided for movement in slots 22 in plates 21 fixed to the two sections. The ends 23a extend into bosses 45 connecting the rods 44 of pistons 40 which move in cylinders 30 fixed to section members 18, 19. The pistons have an orifice through which a fluid is forced on relative movements of the wheel and the rigid sections to absorb the energy of landing impact and rebound. The fluid may be air in the upper cylinders 30 and liquid in the lower cylinders and the undercarriage may be fixed or retractable.
GB36473/62A 1962-09-26 1962-09-26 Aircraft landing gear Expired GB961644A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB36473/62A GB961644A (en) 1962-09-26 1962-09-26 Aircraft landing gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB36473/62A GB961644A (en) 1962-09-26 1962-09-26 Aircraft landing gear

Publications (1)

Publication Number Publication Date
GB961644A true GB961644A (en) 1964-06-24

Family

ID=10388479

Family Applications (1)

Application Number Title Priority Date Filing Date
GB36473/62A Expired GB961644A (en) 1962-09-26 1962-09-26 Aircraft landing gear

Country Status (1)

Country Link
GB (1) GB961644A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105179551A (en) * 2015-09-17 2015-12-23 十堰民乐液压机械有限公司 Single-piston-rod double-cylinder-barrel hydro-pneumatic spring cylinder
US10946952B2 (en) 2017-03-17 2021-03-16 Safran Landing Systems Uk Ltd Aircraft landing gear assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105179551A (en) * 2015-09-17 2015-12-23 十堰民乐液压机械有限公司 Single-piston-rod double-cylinder-barrel hydro-pneumatic spring cylinder
US10946952B2 (en) 2017-03-17 2021-03-16 Safran Landing Systems Uk Ltd Aircraft landing gear assembly

Similar Documents

Publication Publication Date Title
GB961644A (en) Aircraft landing gear
GB505263A (en) Improvements relating to aircraft undercarriages
GB1139915A (en) Aircraft retractable undercarriages
GB984775A (en) Improvements in or relating to retractable undercarriages for aircraft
GB524929A (en) Improvements relating to aircraft undercarriages with resiliently mounted landing elements
GB630183A (en) Improvements in aircraft landing elements
GB604223A (en) Improvements in and relating to shock absorbing and damping devices more especially for facilitating the landing of aircraft
GB1104069A (en) Improvements in or relating to aircraft landing gear
GB687903A (en) Improvements relating to aircraft retractable landing gear
GB458187A (en) Improvements relating to retractable undercarriages for aircraft
GB1423895A (en) Air-craft fuselage-mounted undercarriages
GB452324A (en) A system of retractable landing gear for aeroplanes
US2185802A (en) Oleo device for landing gears and the like
GB589450A (en) Improvements in and relating to landing gear for aircraft
GB1011830A (en) Aircraft undercarriages
GB338690A (en) Improvements in aircraft
GB616141A (en) Improvements in retractable undercarriages, in particular for heavy aircraft
GB866974A (en) Improvements in or relating to aircraft undercarriages
GB326705A (en) Improvements in and relating to landing gear for aircraft
GB503789A (en) Improvements relating to retractable undercarriages for aircraft
GB690111A (en) Improvements in aircraft alighting gear
GB456139A (en) Improvements in undercarriages for aeroplanes
GB1070487A (en) Under-carriage with wheels in tandem
GB1450253A (en) Aircraft undercarriages
GB540776A (en) Improvements in telescopic shock-absorbers