GB1181254A - Improvements in or relating to Undercarriages for Aircraft - Google Patents

Improvements in or relating to Undercarriages for Aircraft

Info

Publication number
GB1181254A
GB1181254A GB2127267A GB2127267A GB1181254A GB 1181254 A GB1181254 A GB 1181254A GB 2127267 A GB2127267 A GB 2127267A GB 2127267 A GB2127267 A GB 2127267A GB 1181254 A GB1181254 A GB 1181254A
Authority
GB
United Kingdom
Prior art keywords
aircraft
undercarriage
undercarriages
relating
ram
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
GB2127267A
Inventor
Rene Lucien
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.)
Messier SA
Original Assignee
Messier 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 Messier SA filed Critical Messier SA
Publication of GB1181254A publication Critical patent/GB1181254A/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
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft

Abstract

1,181,254. Retractable aircraft undercarriages. MESSIER. 8 May, 1967 [3 June, 1966], No. 21272/67. Heading B7G. An aircraft undercarriage comprises a main -eg 4 attached to the aircraft by a strut 7 and a lever 11 as shown, the undercarriage being retracted by a ram 13. The ram 13 may be pivoted to the aircraft at 14 so that on being extended the undercarriage is raised and a body C slung under the fuselage is cleared. The wheel 2 may be carried on a lever 3 attached via a link 5 to a shock-absorber 6 in the leg 4. The undercarriage may be held in the extended and retracted positions by locks 19 and 17, respectively.
GB2127267A 1966-06-03 1967-05-08 Improvements in or relating to Undercarriages for Aircraft Expired GB1181254A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR64197A FR1488435A (en) 1966-06-03 1966-06-03 Front landing gear

Publications (1)

Publication Number Publication Date
GB1181254A true GB1181254A (en) 1970-02-11

Family

ID=8610162

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2127267A Expired GB1181254A (en) 1966-06-03 1967-05-08 Improvements in or relating to Undercarriages for Aircraft

Country Status (3)

Country Link
DE (1) DE1506600A1 (en)
FR (1) FR1488435A (en)
GB (1) GB1181254A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6811116B1 (en) 1999-09-10 2004-11-02 Airbus Uk Limited Aircraft landing gear

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6811116B1 (en) 1999-09-10 2004-11-02 Airbus Uk Limited Aircraft landing gear

Also Published As

Publication number Publication date
DE1506600A1 (en) 1969-08-28
FR1488435A (en) 1967-07-13

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