GB802021A - Improvements in or relating to landing gear for aircraft - Google Patents

Improvements in or relating to landing gear for aircraft

Info

Publication number
GB802021A
GB802021A GB35804/55A GB3580455A GB802021A GB 802021 A GB802021 A GB 802021A GB 35804/55 A GB35804/55 A GB 35804/55A GB 3580455 A GB3580455 A GB 3580455A GB 802021 A GB802021 A GB 802021A
Authority
GB
United Kingdom
Prior art keywords
arm
aircraft
leg
wheel
plunger
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
GB35804/55A
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.)
Societe dInventions Aeronautiques et Mechaniques SIAM SA
Original Assignee
Societe dInventions Aeronautiques et Mechaniques SIAM SA
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 Societe dInventions Aeronautiques et Mechaniques SIAM SA filed Critical Societe dInventions Aeronautiques et Mechaniques SIAM SA
Publication of GB802021A publication Critical patent/GB802021A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/20Operating mechanisms mechanical

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)

Abstract

802,021. Aircraft undercarriages. SOC. D'INVENTIONS AERONAUTIQUES ET MECANIQUES S.I.A.M. Dec. 13, 1955 [Jan. 13, 1955], No. 35804/55. Class 4. In a retractable undercarriage for aircraft wherein means are provided to adjust the position of the wheel with respect to the leg to avoid obstacles during retraction, the leg J contains an inner sleeve C which carries at its lower end an arm C<SP>1</SP> to which is pivoted a further arm B carrying the wheel R. A shock absorber 1 is connected at its lower end to arm B and at its upper end to a plunger 3 within sleeve C, said plunger having a connection with a link 6 pivotally connected at 8 to a bell-crank 7 mounted on a pivot 5 carried by an extension of the leg J. One arm of bell-crank 7 is formed with a cam-slot 9 which co-operates with a pin 10 on the lower end of an arm 11 which is fixed in the aircraft and carries the retraction pivot 12 of the undercarriage. During retraction of the undercarriage, co-operation between pin 10 and cam slot 9 causes the bell crank to rotate with respect to leg J and thereby draw plunger 3 and shock absorber 1 upwardly within sleeve C to cause the axis of wheel R to follow the path T in order that the wheel may avoid the structural obstacles N.
GB35804/55A 1955-01-13 1955-12-13 Improvements in or relating to landing gear for aircraft Expired GB802021A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR802021X 1955-01-13

Publications (1)

Publication Number Publication Date
GB802021A true GB802021A (en) 1958-09-24

Family

ID=9246101

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35804/55A Expired GB802021A (en) 1955-01-13 1955-12-13 Improvements in or relating to landing gear for aircraft

Country Status (1)

Country Link
GB (1) GB802021A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140365A (en) * 1983-05-25 1984-11-28 Messier Hispano Sa Landing gear for an aircraft structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2140365A (en) * 1983-05-25 1984-11-28 Messier Hispano Sa Landing gear for an aircraft structure

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