SE9802900D0 - flap mechanism - Google Patents

flap mechanism

Info

Publication number
SE9802900D0
SE9802900D0 SE9802900A SE9802900A SE9802900D0 SE 9802900 D0 SE9802900 D0 SE 9802900D0 SE 9802900 A SE9802900 A SE 9802900A SE 9802900 A SE9802900 A SE 9802900A SE 9802900 D0 SE9802900 D0 SE 9802900D0
Authority
SE
Sweden
Prior art keywords
link
flap
fixed
pivotably secured
console
Prior art date
Application number
SE9802900A
Other languages
Swedish (sv)
Other versions
SE9802900L (en
SE515029C2 (en
Inventor
Jacob Ancker
Krister Karling
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Priority to SE9802900A priority Critical patent/SE515029C2/en
Publication of SE9802900D0 publication Critical patent/SE9802900D0/en
Publication of SE9802900L publication Critical patent/SE9802900L/en
Publication of SE515029C2 publication Critical patent/SE515029C2/en

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

The flap (1) is mounted on top of a cam with two arms (3, 4) formed by a front link (3) pivotably secured at its top end to a fixed top link (5) in a wing console (11) fixed to the wing (2), and a rear link (4) pivotably secured at its top end to a top link (6) movable with respect to the wing console. The bottom ends of the front and rear links are pivotably secured by bottom links (8, 9) to the lower part of a cam body forming a flap console (7) fixed to the flap.
SE9802900A 1998-08-31 1998-08-31 Lowering control mechanism for flap on aircraft wing, comprising cam with pair of link arms pivotably secured via top and bottom links to flap and wing consoles SE515029C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SE9802900A SE515029C2 (en) 1998-08-31 1998-08-31 Lowering control mechanism for flap on aircraft wing, comprising cam with pair of link arms pivotably secured via top and bottom links to flap and wing consoles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9802900A SE515029C2 (en) 1998-08-31 1998-08-31 Lowering control mechanism for flap on aircraft wing, comprising cam with pair of link arms pivotably secured via top and bottom links to flap and wing consoles

Publications (3)

Publication Number Publication Date
SE9802900D0 true SE9802900D0 (en) 1998-08-31
SE9802900L SE9802900L (en) 2000-03-01
SE515029C2 SE515029C2 (en) 2001-05-28

Family

ID=20412402

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9802900A SE515029C2 (en) 1998-08-31 1998-08-31 Lowering control mechanism for flap on aircraft wing, comprising cam with pair of link arms pivotably secured via top and bottom links to flap and wing consoles

Country Status (1)

Country Link
SE (1) SE515029C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10133920B4 (en) 2001-07-12 2004-05-13 Eads Deutschland Gmbh Lift flap mechanism
GB0708334D0 (en) 2007-04-30 2007-06-06 Airbus Uk Ltd Method and apparatus for deploying an auxiliary airfoil

Also Published As

Publication number Publication date
SE9802900L (en) 2000-03-01
SE515029C2 (en) 2001-05-28

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Legal Events

Date Code Title Description
NUG Patent has lapsed