GB530561A - Aeroplane landing gear - Google Patents

Aeroplane landing gear

Info

Publication number
GB530561A
GB530561A GB18743/39A GB1874339A GB530561A GB 530561 A GB530561 A GB 530561A GB 18743/39 A GB18743/39 A GB 18743/39A GB 1874339 A GB1874339 A GB 1874339A GB 530561 A GB530561 A GB 530561A
Authority
GB
United Kingdom
Prior art keywords
struts
landing gear
inwardly directed
alighting gear
aeroplane landing
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
GB18743/39A
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 GB18743/39A priority Critical patent/GB530561A/en
Publication of GB530561A publication Critical patent/GB530561A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

530,561. Aircraft alighting gear. WITTMAN, S. J. June 27, 1938, No. 18743. [Class 4] Aircraft alighting gear includes diverging struts 11, 12 formed from resilient material having inwardly directed ends 13, 14 which carry the landing wheels 16. In one form the struts 11, 12 and a body-portion 10 are formed in one piece which is secured to the fuselage framework. The struts have the cross-section shown in Fig. 7. In a. modification, the two are separate and formed with inwardly directed body-portions which are connected to the fuselage framework.
GB18743/39A 1939-06-27 1939-06-27 Aeroplane landing gear Expired GB530561A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18743/39A GB530561A (en) 1939-06-27 1939-06-27 Aeroplane landing gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18743/39A GB530561A (en) 1939-06-27 1939-06-27 Aeroplane landing gear

Publications (1)

Publication Number Publication Date
GB530561A true GB530561A (en) 1940-12-13

Family

ID=10117632

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18743/39A Expired GB530561A (en) 1939-06-27 1939-06-27 Aeroplane landing gear

Country Status (1)

Country Link
GB (1) GB530561A (en)

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