GB686953A - Improvements in and relating to retractable undercarriages of aircraft - Google Patents

Improvements in and relating to retractable undercarriages of aircraft

Info

Publication number
GB686953A
GB686953A GB1381951A GB1381951A GB686953A GB 686953 A GB686953 A GB 686953A GB 1381951 A GB1381951 A GB 1381951A GB 1381951 A GB1381951 A GB 1381951A GB 686953 A GB686953 A GB 686953A
Authority
GB
United Kingdom
Prior art keywords
leg
pivot
aircraft
retracted
wing
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
GB1381951A
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.)
Blackburn and General Aircraft Ltd
Original Assignee
Blackburn and General Aircraft Ltd
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 Blackburn and General Aircraft Ltd filed Critical Blackburn and General Aircraft Ltd
Priority to GB1381951A priority Critical patent/GB686953A/en
Publication of GB686953A publication Critical patent/GB686953A/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
    • B64C25/12Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways

Abstract

686,953. Aircraft undercarriages. BLACKBURN & GENERAL AIRCRAFT, Ltd., and THIHSK, W. H. June 11, 1951. No. 13819/51. Class 4. In a retractable undercarriage for an aircraft, each main wheel 1 is carried by an arm 2 attached to the leg 4 by a pivot 3 and con nected to a shock ab sorber 7 by a pivot 8 The upper end 9 of the shock absorber is pivotally connected to a swinging link 10 which is mounted on a pivot 11 fast with the leg 4 and inter mediate its ends is connected at 14 to the piston rod 13 of a hydraulic ja,ck 12. A single door 15 fo closing the space in the wing into which the wheel and leg are retracted is attached to the leg by brackets (not shown), such that on actuation of the jack 12 the arm 2 is rocked about the pivot 3 to bring the wheel 13 within the area of the door 15, whereafter the leg 4 may be retracted into the space in the wing for the door to completely close the same. The retracting mechanism Fig. 2, (not shown) comprises for each undercarriage a pair of transversely disposed interconnected toggle links, one attached to the wing structure and the other to the leg 4, the links being "broken" and retracted by a hydraulic jack which connects one link to the wing structure.
GB1381951A 1951-06-11 1951-06-11 Improvements in and relating to retractable undercarriages of aircraft Expired GB686953A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1381951A GB686953A (en) 1951-06-11 1951-06-11 Improvements in and relating to retractable undercarriages of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1381951A GB686953A (en) 1951-06-11 1951-06-11 Improvements in and relating to retractable undercarriages of aircraft

Publications (1)

Publication Number Publication Date
GB686953A true GB686953A (en) 1953-02-04

Family

ID=10029964

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1381951A Expired GB686953A (en) 1951-06-11 1951-06-11 Improvements in and relating to retractable undercarriages of aircraft

Country Status (1)

Country Link
GB (1) GB686953A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2511338A1 (en) * 1981-08-12 1983-02-18 Messier Hispano Sa LANDING TRAIN FOR AIRCRAFT

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2511338A1 (en) * 1981-08-12 1983-02-18 Messier Hispano Sa LANDING TRAIN FOR AIRCRAFT
EP0072720A1 (en) * 1981-08-12 1983-02-23 Messier-Hispano-Bugatti (S.A) Aircraft landing gear

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