GB428265A - Cantilever type of landing gear for flying machines - Google Patents

Cantilever type of landing gear for flying machines

Info

Publication number
GB428265A
GB428265A GB24248/34A GB2424834A GB428265A GB 428265 A GB428265 A GB 428265A GB 24248/34 A GB24248/34 A GB 24248/34A GB 2424834 A GB2424834 A GB 2424834A GB 428265 A GB428265 A GB 428265A
Authority
GB
United Kingdom
Prior art keywords
strut
landing
fuselage
aug
shock
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
GB24248/34A
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
Publication of GB428265A publication Critical patent/GB428265A/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
    • B64C25/06—Undercarriages fixed
    • 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)
  • General Details Of Gearings (AREA)

Abstract

428,265. Aircraft landing - gear. MESSERSCHMITT, W., 118a, Haunstetterstrasse, Augsburg, Germany. Aug. 22, 1934, No. 24248. Convention date, Aug. 23, 1933. [Class 4] [See also Group XXXIV] A cantilever strut carrying a wheel, float or skid is arranged to break under excessive landing shock at a rupturing zone provided where the strut protrudes from the fuselage, wing or nacelle in which it is fixed. The strut c, provided with a shock-absorbing arrangement, is fixed to a conical tube f, forming part of the wing attachment frame of the fuselage, by an intermediate member e in which the rupturing zone is formed. The cross-section of the member e may have the same or different movements of resistance about longitudinal and transverse axes. An additional rupturing zone h may be formed where the stub-axle of the landing wheel d is joined to the strut c to avoid excess stresses in the axial direction of the strut.
GB24248/34A 1933-08-23 1934-08-22 Cantilever type of landing gear for flying machines Expired GB428265A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE428265X 1933-08-23

Publications (1)

Publication Number Publication Date
GB428265A true GB428265A (en) 1935-05-09

Family

ID=6477440

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24248/34A Expired GB428265A (en) 1933-08-23 1934-08-22 Cantilever type of landing gear for flying machines

Country Status (1)

Country Link
GB (1) GB428265A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110576966A (en) * 2019-09-29 2019-12-17 中国直升机设计研究所 Strut type undercarriage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110576966A (en) * 2019-09-29 2019-12-17 中国直升机设计研究所 Strut type undercarriage

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