FR2547270B1 - EXTENSION AND RETRACTION MECHANISM FOR AN ATTACK SHUTTER OF AN AIRCRAFT WING - Google Patents

EXTENSION AND RETRACTION MECHANISM FOR AN ATTACK SHUTTER OF AN AIRCRAFT WING

Info

Publication number
FR2547270B1
FR2547270B1 FR8309681A FR8309681A FR2547270B1 FR 2547270 B1 FR2547270 B1 FR 2547270B1 FR 8309681 A FR8309681 A FR 8309681A FR 8309681 A FR8309681 A FR 8309681A FR 2547270 B1 FR2547270 B1 FR 2547270B1
Authority
FR
France
Prior art keywords
shutter
attack
extension
aircraft wing
retraction mechanism
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
FR8309681A
Other languages
French (fr)
Other versions
FR2547270A1 (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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority to FR8309681A priority Critical patent/FR2547270B1/en
Publication of FR2547270A1 publication Critical patent/FR2547270A1/en
Application granted granted Critical
Publication of FR2547270B1 publication Critical patent/FR2547270B1/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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • 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
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
FR8309681A 1983-06-10 1983-06-10 EXTENSION AND RETRACTION MECHANISM FOR AN ATTACK SHUTTER OF AN AIRCRAFT WING Expired FR2547270B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8309681A FR2547270B1 (en) 1983-06-10 1983-06-10 EXTENSION AND RETRACTION MECHANISM FOR AN ATTACK SHUTTER OF AN AIRCRAFT WING

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8309681A FR2547270B1 (en) 1983-06-10 1983-06-10 EXTENSION AND RETRACTION MECHANISM FOR AN ATTACK SHUTTER OF AN AIRCRAFT WING

Publications (2)

Publication Number Publication Date
FR2547270A1 FR2547270A1 (en) 1984-12-14
FR2547270B1 true FR2547270B1 (en) 1985-09-06

Family

ID=9289683

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8309681A Expired FR2547270B1 (en) 1983-06-10 1983-06-10 EXTENSION AND RETRACTION MECHANISM FOR AN ATTACK SHUTTER OF AN AIRCRAFT WING

Country Status (1)

Country Link
FR (1) FR2547270B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4753402A (en) * 1985-12-30 1988-06-28 The Boeing Company Biased leading edge slat apparatus
US6802475B2 (en) * 2002-07-04 2004-10-12 Smiths Wolverhampton Limited Flight surface actuator
GB201011378D0 (en) * 2010-07-06 2010-08-18 Ultra Electronics Ltd Linkage for guiding a flexible cable

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2916040C2 (en) * 1979-04-20 1986-01-02 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Wing for an aircraft with movable slats

Also Published As

Publication number Publication date
FR2547270A1 (en) 1984-12-14

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Legal Events

Date Code Title Description
ST Notification of lapse