GB1028669A - Retractable aircraft undercarriages - Google Patents

Retractable aircraft undercarriages

Info

Publication number
GB1028669A
GB1028669A GB4288962A GB4288962A GB1028669A GB 1028669 A GB1028669 A GB 1028669A GB 4288962 A GB4288962 A GB 4288962A GB 4288962 A GB4288962 A GB 4288962A GB 1028669 A GB1028669 A GB 1028669A
Authority
GB
United Kingdom
Prior art keywords
leg
aircraft
jack
nov
hinge
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
GB4288962A
Inventor
Reginald James Brown
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.)
Dowty Rotol Ltd
Original Assignee
Dowty Rotol 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 Dowty Rotol Ltd filed Critical Dowty Rotol Ltd
Priority to GB4288962A priority Critical patent/GB1028669A/en
Publication of GB1028669A publication Critical patent/GB1028669A/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
    • B64C25/14Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

1,028,669. Aircraft undercarriages. DOWTY ROTOL Ltd. Nov. 12, 1963 [Nov. 13, 1962; Nov. 16, 1962], Nos. 42889/62 and 43475/62. Heading B7G. A retractable aircraft undercarriage has a leg pivotally connected to the aircraft structure by links 16, 17 and a fluid pressure operated jack 26 pivotally connected to the aircraft structure and the leg for raising or lowering the aircraft by pivoting the leg about a hinge 18, to facilitate loading. A separate retraction jack 20 and the jack 26 is then connected to the leg by a link 30 which allows the leg to pivot about the hinge 18. The jack 26 contains an internal lock, and the link 30 is secured to the leg by locking means 33, 34 when the leg is not retracted. The leg may also be telescopic, and may be shortened or extended to vary the aircraft height further by withdrawing liquid from or introducing liquid into a shock absorber of the leg. As described, the undercarriage retracts forwardly (to the left in the figure), and pivots rearwardly to lower the aircraft, and the retraction jack has some lost motion so that it does not restrict the lowering operation. The invention may be applied to nose or main landing wheels. The movement of the tail of the aircraft may be accentuated by extending the main wheels and shortening the nose wheel, or vice versa.
GB4288962A 1962-11-13 1962-11-13 Retractable aircraft undercarriages Expired GB1028669A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4288962A GB1028669A (en) 1962-11-13 1962-11-13 Retractable aircraft undercarriages

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4288962A GB1028669A (en) 1962-11-13 1962-11-13 Retractable aircraft undercarriages

Publications (1)

Publication Number Publication Date
GB1028669A true GB1028669A (en) 1966-05-04

Family

ID=10426406

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4288962A Expired GB1028669A (en) 1962-11-13 1962-11-13 Retractable aircraft undercarriages

Country Status (1)

Country Link
GB (1) GB1028669A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4720063A (en) * 1985-09-30 1988-01-19 The Boeing Company Main landing gear with variable length drag brace
GB2410728A (en) * 2004-02-07 2005-08-10 Rolls Royce Plc Landing arrangement for an aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4720063A (en) * 1985-09-30 1988-01-19 The Boeing Company Main landing gear with variable length drag brace
GB2410728A (en) * 2004-02-07 2005-08-10 Rolls Royce Plc Landing arrangement for an aircraft
GB2410728B (en) * 2004-02-07 2006-03-29 Rolls Royce Plc A landing arrangement for an aircraft
US7143975B2 (en) 2004-02-07 2006-12-05 Rolls-Royce Plc Landing arrangement for an aircraft

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