GB767859A - Take off and landing gear for aircraft - Google Patents

Take off and landing gear for aircraft

Info

Publication number
GB767859A
GB767859A GB29386/54A GB2938654A GB767859A GB 767859 A GB767859 A GB 767859A GB 29386/54 A GB29386/54 A GB 29386/54A GB 2938654 A GB2938654 A GB 2938654A GB 767859 A GB767859 A GB 767859A
Authority
GB
United Kingdom
Prior art keywords
ski
aircraft
leg
landing gear
shock absorber
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
GB29386/54A
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.)
DISPOSITIFS OLEO PNEUMATIQUES
Original Assignee
DISPOSITIFS OLEO PNEUMATIQUES
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 DISPOSITIFS OLEO PNEUMATIQUES filed Critical DISPOSITIFS OLEO PNEUMATIQUES
Publication of GB767859A publication Critical patent/GB767859A/en
Expired legal-status Critical Current

Links

Classifications

    • 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 
    • B64C25/52—Skis or runners

Abstract

767,859. Aircraft landing gear. DISPOSITIFS OLEO-PNEUMATIQUES (D.O.P). Oct. 12, 1954 [Oct. 14, 1953], No. 29386/54. Class 4 An aircraft is provided with at least one auxiliary front or rear landing gear including at least one steerable low pressure tyre 1, and with main landing gear constituted by one or more skis 2 pivoted on a horizontal axis 3 located slightly to the rear or front of the centre of gravity of the aircraft. In Fig. 2 (not shown) the ski is provided with a roller for running over hard ground, e.g. concrete. The ski is pivoted to the lower cylinder of a shock absorbing leg, and a further shock absorber extends between the rear part of the ski and the leg. In Figs. 3, the ski is connected to the leg 11 through a vertical shock absorber 12 and by a toggle link 13, 14 and a second shock absorber 15 extending between the centre of the toggle and the leg, the chambers of the two shock absorbers being connected by a pipe 16. The ski is formed in three portions 7, 8, 9 pivotable to facilitate retraction. A hydraulically operated member may be attached to the ski and be adapted to engage the ground to act as a brake. Specification 767,032 is referred to.
GB29386/54A 1953-10-14 1954-10-12 Take off and landing gear for aircraft Expired GB767859A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR767859X 1953-10-14

Publications (1)

Publication Number Publication Date
GB767859A true GB767859A (en) 1957-02-06

Family

ID=9183908

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29386/54A Expired GB767859A (en) 1953-10-14 1954-10-12 Take off and landing gear for aircraft

Country Status (1)

Country Link
GB (1) GB767859A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3208694A (en) * 1964-03-20 1965-09-28 Upshur T Joyner Nose gear steering system for vehicle with main skids

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3208694A (en) * 1964-03-20 1965-09-28 Upshur T Joyner Nose gear steering system for vehicle with main skids

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