FR2305342A1 - Mecanisme de montage et de manoeuvre des volets de bord de fuite des ailes d'un avion - Google Patents

Mecanisme de montage et de manoeuvre des volets de bord de fuite des ailes d'un avion

Info

Publication number
FR2305342A1
FR2305342A1 FR7608552A FR7608552A FR2305342A1 FR 2305342 A1 FR2305342 A1 FR 2305342A1 FR 7608552 A FR7608552 A FR 7608552A FR 7608552 A FR7608552 A FR 7608552A FR 2305342 A1 FR2305342 A1 FR 2305342A1
Authority
FR
France
Prior art keywords
airplane
mounting
operating
wing edge
edge flaps
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.)
Withdrawn
Application number
FR7608552A
Other languages
English (en)
French (fr)
Inventor
James Byron Cole
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
Publication of FR2305342A1 publication Critical patent/FR2305342A1/fr
Withdrawn legal-status Critical Current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
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear 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
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
    • 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
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Jib Cranes (AREA)
FR7608552A 1975-03-24 1976-03-24 Mecanisme de montage et de manoeuvre des volets de bord de fuite des ailes d'un avion Withdrawn FR2305342A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US56109675A 1975-03-24 1975-03-24

Publications (1)

Publication Number Publication Date
FR2305342A1 true FR2305342A1 (fr) 1976-10-22

Family

ID=24240613

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7608552A Withdrawn FR2305342A1 (fr) 1975-03-24 1976-03-24 Mecanisme de montage et de manoeuvre des volets de bord de fuite des ailes d'un avion

Country Status (5)

Country Link
JP (1) JPS51126700A (de)
DE (1) DE2611918A1 (de)
FR (1) FR2305342A1 (de)
GB (5) GB1547905A (de)
IT (1) IT1057415B (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62113697A (ja) * 1985-11-14 1987-05-25 財団法人　日本航空機開発協会 飛行機翼後縁フラツプのリンク式作動機構
GB8915487D0 (en) * 1989-07-06 1989-08-23 Short Brothers Plc A flap assembly
DE10133920B4 (de) * 2001-07-12 2004-05-13 Eads Deutschland Gmbh Auftriebsklappen-Mechanismus
DE10328540B4 (de) * 2003-06-24 2008-02-14 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
DE10328717B3 (de) 2003-06-25 2004-12-02 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
DE10339030B4 (de) 2003-08-25 2005-11-03 Man Technologie Ag Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung
GB0921007D0 (en) 2009-11-30 2010-01-13 Airbus Operations Ltd Trailing edge flap
CN109367761B (zh) * 2018-10-11 2022-05-31 西北工业大学 一种用于旋转机翼的襟翼收放操纵机构

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3009668A (en) * 1958-05-12 1961-11-21 Lockheed Aircraft Corp Displacement type airfoil flap with boundary layer control
FR2076043A1 (de) * 1970-01-12 1971-10-15 Hawker Siddeley Aviat
US3874617A (en) * 1974-07-17 1975-04-01 Mc Donnell Douglas Corp Stol flaps

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3009668A (en) * 1958-05-12 1961-11-21 Lockheed Aircraft Corp Displacement type airfoil flap with boundary layer control
FR2076043A1 (de) * 1970-01-12 1971-10-15 Hawker Siddeley Aviat
US3874617A (en) * 1974-07-17 1975-04-01 Mc Donnell Douglas Corp Stol flaps

Also Published As

Publication number Publication date
GB1547904A (en) 1979-06-27
GB1547903A (en) 1979-06-27
GB1547905A (en) 1979-06-27
DE2611918A1 (de) 1976-11-11
IT1057415B (it) 1982-03-10
JPS51126700A (en) 1976-11-04
GB1547901A (en) 1979-06-27
GB1547902A (en) 1979-06-27

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Legal Events

Date Code Title Description
ST Notification of lapse