GB393445A - Improvements in or relating to aircraft landing gear - Google Patents

Improvements in or relating to aircraft landing gear

Info

Publication number
GB393445A
GB393445A GB24133/32A GB2413332A GB393445A GB 393445 A GB393445 A GB 393445A GB 24133/32 A GB24133/32 A GB 24133/32A GB 2413332 A GB2413332 A GB 2413332A GB 393445 A GB393445 A GB 393445A
Authority
GB
United Kingdom
Prior art keywords
aircraft landing
struts
extensions
springs
dornier
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
GB24133/32A
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.)
Dornier Metallbauten GmbH
Original Assignee
Dornier Metallbauten GmbH
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 Dornier Metallbauten GmbH filed Critical Dornier Metallbauten GmbH
Publication of GB393445A publication Critical patent/GB393445A/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
    • 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
    • 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)
  • Vibration Dampers (AREA)

Abstract

393,445. Aircraft landing-gear. DORNIER METALLBAUTEN GES. and DORNIER, C., Friedrichshafen, Lake Constance, Germany. Aug. 29, 1932, No. 24133. Convention date, Oct. 28,1931. [Class 4.] An aircraft landing- gear comprises wheels on pivoted struts b, b<1> having normally horizontal extensions d, d<1> connected to springs f, f<1>, a stop g limiting the upward movement of the extensions d, d<1> during flight. The springs f, f<1> may be replaced by compression springs or by hydraulic or pneumatic shock absorbers. The struts and their extensions may be articulated at their pivots and stayed by tension or other members connecting the ends of each pair. When tension members are used the struts b, b<1> are extended beyond their pivots to engage stops to prevent them from drooping during flight.
GB24133/32A 1931-10-28 1932-08-29 Improvements in or relating to aircraft landing gear Expired GB393445A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE393445X 1931-10-28

Publications (1)

Publication Number Publication Date
GB393445A true GB393445A (en) 1933-06-08

Family

ID=6391541

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24133/32A Expired GB393445A (en) 1931-10-28 1932-08-29 Improvements in or relating to aircraft landing gear

Country Status (1)

Country Link
GB (1) GB393445A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479976A (en) * 1946-02-27 1949-08-23 Paul L Shultz Aircraft
US2673732A (en) * 1951-06-05 1954-03-30 Howard H Heston Cross spring action and stabilizing for vehicles
US2717152A (en) * 1953-01-21 1955-09-06 Art L Ketchum Reversed spring suspension for vehicle bodies
JP2019123486A (en) * 2018-01-15 2019-07-25 石川　誠司 Stabilization mechanism of aircraft having two or more rotary wings

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479976A (en) * 1946-02-27 1949-08-23 Paul L Shultz Aircraft
US2673732A (en) * 1951-06-05 1954-03-30 Howard H Heston Cross spring action and stabilizing for vehicles
US2717152A (en) * 1953-01-21 1955-09-06 Art L Ketchum Reversed spring suspension for vehicle bodies
JP2019123486A (en) * 2018-01-15 2019-07-25 石川　誠司 Stabilization mechanism of aircraft having two or more rotary wings

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