FR2314097A1 - Aircraft wing with leading edge flaps - has interlinked flaps operated by same jack to rotate through different angles - Google Patents

Aircraft wing with leading edge flaps - has interlinked flaps operated by same jack to rotate through different angles

Info

Publication number
FR2314097A1
FR2314097A1 FR7517910A FR7517910A FR2314097A1 FR 2314097 A1 FR2314097 A1 FR 2314097A1 FR 7517910 A FR7517910 A FR 7517910A FR 7517910 A FR7517910 A FR 7517910A FR 2314097 A1 FR2314097 A1 FR 2314097A1
Authority
FR
France
Prior art keywords
flaps
leading edge
aircraft wing
interlinked
rotate
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.)
Granted
Application number
FR7517910A
Other languages
French (fr)
Other versions
FR2314097B1 (en
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR7517910A priority Critical patent/FR2314097A1/en
Publication of FR2314097A1 publication Critical patent/FR2314097A1/en
Application granted granted Critical
Publication of FR2314097B1 publication Critical patent/FR2314097B1/fr
Granted 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/26—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by multiple flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members

Abstract

The flap (15), when in its r tracted position forms part of the upper surface of the leading edge of the aircraft wing. The flap (9) is retracted to form part of the lower surface of the leading edge of the aircraft wing. A hydraulic jack actuates the rod (17) which rotates the lever (19) in a clockwise direction which in turn operates the links (23, 35, 7, 29). This operation results in the flap (15) being pushed forwards and rotated through 5 from its retracted position. At the same time the flap (9) is swung from its retracted position through an angle of 150 so that an aerodynamic slot is formed between the two flaps.
FR7517910A 1975-06-09 1975-06-09 Aircraft wing with leading edge flaps - has interlinked flaps operated by same jack to rotate through different angles Granted FR2314097A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7517910A FR2314097A1 (en) 1975-06-09 1975-06-09 Aircraft wing with leading edge flaps - has interlinked flaps operated by same jack to rotate through different angles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7517910A FR2314097A1 (en) 1975-06-09 1975-06-09 Aircraft wing with leading edge flaps - has interlinked flaps operated by same jack to rotate through different angles

Publications (2)

Publication Number Publication Date
FR2314097A1 true FR2314097A1 (en) 1977-01-07
FR2314097B1 FR2314097B1 (en) 1980-01-25

Family

ID=9156209

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7517910A Granted FR2314097A1 (en) 1975-06-09 1975-06-09 Aircraft wing with leading edge flaps - has interlinked flaps operated by same jack to rotate through different angles

Country Status (1)

Country Link
FR (1) FR2314097A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11192631B2 (en) 2018-06-19 2021-12-07 Airbus Operations Gmbh Connection assembly for transmitting loads between two wing elements

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11192631B2 (en) 2018-06-19 2021-12-07 Airbus Operations Gmbh Connection assembly for transmitting loads between two wing elements

Also Published As

Publication number Publication date
FR2314097B1 (en) 1980-01-25

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Legal Events

Date Code Title Description
ST Notification of lapse