GB1365168A - Device for extending and retracting flaps of aircraft wings - Google Patents

Device for extending and retracting flaps of aircraft wings

Info

Publication number
GB1365168A
GB1365168A GB6090471A GB6090471A GB1365168A GB 1365168 A GB1365168 A GB 1365168A GB 6090471 A GB6090471 A GB 6090471A GB 6090471 A GB6090471 A GB 6090471A GB 1365168 A GB1365168 A GB 1365168A
Authority
GB
United Kingdom
Prior art keywords
lever
brackets
extending
flap
aircraft wings
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
GB6090471A
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.)
Hamburger Flugzeugbau GmbH
Original Assignee
Hamburger Flugzeugbau GmbH
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 Hamburger Flugzeugbau GmbH filed Critical Hamburger Flugzeugbau GmbH
Publication of GB1365168A publication Critical patent/GB1365168A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps

Abstract

1365168 Aircraft flaps HAMBURGER FLUGZEUGBAU GmbH 31 Dec 1971 [27 Jan 1971] 60904/71 Heading B7G An aircraft wing 1 has a slotted trailing edge flap 6, the wing and the flap respectively being provided with brackets 10 and 14 which are pivotally connected at 2 and 11 by a lever 5. A two-arm lever 7 is pivoted at 12 to lever 5 and connected to brackets 10 and 14 by rods 8 and 9. Extension and retraction of the flap is effected by a jack 3. In a further embodiment the juxtaposition of the brackets, levers and rods are different and the lever 7 is cranked.
GB6090471A 1971-01-27 1971-12-31 Device for extending and retracting flaps of aircraft wings Expired GB1365168A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19712103639 DE2103639A1 (en) 1971-01-27 1971-01-27 Airfoil for aircraft with one or more one-part or multi-part slotted flaps

Publications (1)

Publication Number Publication Date
GB1365168A true GB1365168A (en) 1974-08-29

Family

ID=5796962

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6090471A Expired GB1365168A (en) 1971-01-27 1971-12-31 Device for extending and retracting flaps of aircraft wings

Country Status (2)

Country Link
DE (1) DE2103639A1 (en)
GB (1) GB1365168A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2233613A (en) * 1989-07-06 1991-01-16 Short Brothers Plc Aircraft flap assembly.
WO1996009955A1 (en) * 1994-09-29 1996-04-04 West-Walker, Francis, Nigel Linkage to deploy a surface relative to a wing

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2425379A1 (en) * 1978-05-08 1979-12-07 Dornier Gmbh Aircraft control surface actuating gear - has quadrilateral linkage with idler replaced by three link unit with T-link coupled to bell-crank

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2233613A (en) * 1989-07-06 1991-01-16 Short Brothers Plc Aircraft flap assembly.
GB2233613B (en) * 1989-07-06 1993-04-07 Short Brothers Plc A flap assembly
WO1996009955A1 (en) * 1994-09-29 1996-04-04 West-Walker, Francis, Nigel Linkage to deploy a surface relative to a wing

Also Published As

Publication number Publication date
DE2103639A1 (en) 1972-09-07

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Legal Events

Date Code Title Description
PS Patent sealed
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee