GB356447A - Landing gear for aircraft - Google Patents

Landing gear for aircraft

Info

Publication number
GB356447A
GB356447A GB25127/30A GB2512730A GB356447A GB 356447 A GB356447 A GB 356447A GB 25127/30 A GB25127/30 A GB 25127/30A GB 2512730 A GB2512730 A GB 2512730A GB 356447 A GB356447 A GB 356447A
Authority
GB
United Kingdom
Prior art keywords
axle
fuselage
oleo
aircraft
frame
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
GB25127/30A
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.)
Sir WG Armstrong Whitworth Aircraft Ltd
Original Assignee
Sir WG Armstrong Whitworth 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 Sir WG Armstrong Whitworth Aircraft Ltd filed Critical Sir WG Armstrong Whitworth Aircraft Ltd
Priority to GB25127/30A priority Critical patent/GB356447A/en
Publication of GB356447A publication Critical patent/GB356447A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/04—Arrangement or disposition on aircraft
    • 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)
  • Tires In General (AREA)

Abstract

356,447. Aircraft landing-gear. ARMSTRONG WHITWORTH AIRCRAFT, Ltd., SIR W. G. and LLOYD, J., Park Side, Coventry. Aug. 22, 1930, No. 25127. [Class 4.] The greater part of the axle, and the oleo-leg of an aircraft landing-gear are arranged within the fuselage and in some cases the oleo-leg may be constituted by a strut of the fuselage frame. A divided axle 4 is shown braced to the frame at its centre by members 13, 15 within the fuselage shell. The oleo-legs 5 are connected to the axle near radius rods 10. The axles carry wheel fairings 9 which have no other support. A modification is described in which a continuous axle passes through the fuselage and is hinged to pistons moving in tubular struts of the fuselage frame, one of the hinged joints having a sliding connection with the axle.
GB25127/30A 1930-08-22 1930-08-22 Landing gear for aircraft Expired GB356447A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB25127/30A GB356447A (en) 1930-08-22 1930-08-22 Landing gear for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25127/30A GB356447A (en) 1930-08-22 1930-08-22 Landing gear for aircraft

Publications (1)

Publication Number Publication Date
GB356447A true GB356447A (en) 1931-09-10

Family

ID=10222638

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25127/30A Expired GB356447A (en) 1930-08-22 1930-08-22 Landing gear for aircraft

Country Status (1)

Country Link
GB (1) GB356447A (en)

Similar Documents

Publication Publication Date Title
GB356447A (en) Landing gear for aircraft
GB505263A (en) Improvements relating to aircraft undercarriages
US2021439A (en) Retractable landing gear
GB510164A (en) Improvements in aircraft landing (or alighting) gear
US2069994A (en) Folding landing gear
GB393445A (en) Improvements in or relating to aircraft landing gear
GB524929A (en) Improvements relating to aircraft undercarriages with resiliently mounted landing elements
GB508211A (en) Improvements relating to landing gear for aircraft
GB506528A (en) Improvements relating to folding wing aircraft
GB418468A (en) Aeroplane undercarriages
GB376634A (en) Elastic seaplane undercarriages
GB556325A (en) Improvements in and relating to aircraft landing gear
GB402675A (en) Improvements in and relating to retractable landing gears for aeroplanes and to brakes for use in conjunction therewith
GB462963A (en) Improvements in tail skids or tail wheels for aeroplanes
GB432868A (en) Improvements in or relating to elastic landing gear for aeroplanes
GB598813A (en) Improvements in or relating to transport-planes
GB543024A (en) A helicopter with revolving wings, power and propeller units
GB371629A (en) Improvements in landing gear for aircraft
GB308950A (en) Improvements in the landing chassis and tail skids of airplanes
US2021325A (en) Wheel fairing
GB339218A (en) Improvements in or relating to aircraft landing chassis
GB961644A (en) Aircraft landing gear
GB247283A (en) Improvements in and relating to snow-landing gear for aeroplanes
GB323644A (en) Alighting gear for aeroplanes
US1901795A (en) Airplane landing gear