IT1057415B - ASSEMBLY MECHANISM OF AILERS ON THE OUTLET OF THE WINGS OF AN AIRPLANE - Google Patents

ASSEMBLY MECHANISM OF AILERS ON THE OUTLET OF THE WINGS OF AN AIRPLANE

Info

Publication number
IT1057415B
IT1057415B IT48684/76A IT4868476A IT1057415B IT 1057415 B IT1057415 B IT 1057415B IT 48684/76 A IT48684/76 A IT 48684/76A IT 4868476 A IT4868476 A IT 4868476A IT 1057415 B IT1057415 B IT 1057415B
Authority
IT
Italy
Prior art keywords
ailers
airplane
wings
outlet
assembly mechanism
Prior art date
Application number
IT48684/76A
Other languages
Italian (it)
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
Application granted granted Critical
Publication of IT1057415B publication Critical patent/IT1057415B/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
    • 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)
IT48684/76A 1975-03-24 1976-03-23 ASSEMBLY MECHANISM OF AILERS ON THE OUTLET OF THE WINGS OF AN AIRPLANE IT1057415B (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
IT1057415B true IT1057415B (en) 1982-03-10

Family

ID=24240613

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48684/76A IT1057415B (en) 1975-03-24 1976-03-23 ASSEMBLY MECHANISM OF AILERS ON THE OUTLET OF THE WINGS OF AN AIRPLANE

Country Status (5)

Country Link
JP (1) JPS51126700A (en)
DE (1) DE2611918A1 (en)
FR (1) FR2305342A1 (en)
GB (5) GB1547902A (en)
IT (1) IT1057415B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62113697A (en) * 1985-11-14 1987-05-25 財団法人　日本航空機開発協会 Link type operation mechanism of aircraft wing rear-edge flap
GB8915487D0 (en) * 1989-07-06 1989-08-23 Short Brothers Plc A flap assembly
DE10133920B4 (en) 2001-07-12 2004-05-13 Eads Deutschland Gmbh Lift flap mechanism
DE10328540B4 (en) * 2003-06-24 2008-02-14 Eads Deutschland Gmbh Actuating device for a rudder flap arranged on the trailing edge of the wing of an aircraft
DE10328717B3 (en) 2003-06-25 2004-12-02 Eads Deutschland Gmbh Operating device for control flap on rear edge of aircraft wing has pyramid transmission device connected on one side to wing structure and on other to flap
DE10339030B4 (en) 2003-08-25 2005-11-03 Man Technologie Ag Support structure for an extendable and retractable flap and its use
GB0921007D0 (en) 2009-11-30 2010-01-13 Airbus Operations Ltd Trailing edge flap
CN109367761B (en) * 2018-10-11 2022-05-31 西北工业大学 Flap retraction control mechanism for rotary wing

Family Cites Families (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
DE2100733A1 (en) * 1970-01-12 1971-07-15 Hawker Siddeley Aviation Ltd., Kingston-Upon-Thames, Surrey (Grossbritannien) Device on aircraft wings
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
DE2611918A1 (en) 1976-11-11
GB1547901A (en) 1979-06-27
JPS51126700A (en) 1976-11-04
GB1547903A (en) 1979-06-27
GB1547905A (en) 1979-06-27
FR2305342A1 (en) 1976-10-22
GB1547902A (en) 1979-06-27

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