JPS51126700A - Aeroplane trailing edge flap mounting mechanism - Google Patents

Aeroplane trailing edge flap mounting mechanism

Info

Publication number
JPS51126700A
JPS51126700A JP51032368A JP3236876A JPS51126700A JP S51126700 A JPS51126700 A JP S51126700A JP 51032368 A JP51032368 A JP 51032368A JP 3236876 A JP3236876 A JP 3236876A JP S51126700 A JPS51126700 A JP S51126700A
Authority
JP
Japan
Prior art keywords
aeroplane
trailing edge
mounting mechanism
edge flap
flap mounting
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.)
Pending
Application number
JP51032368A
Other languages
Japanese (ja)
Inventor
Bairon Kooru Jieemuzu
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 JPS51126700A publication Critical patent/JPS51126700A/en
Pending 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
JP51032368A 1975-03-24 1976-03-24 Aeroplane trailing edge flap mounting mechanism Pending JPS51126700A (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
JPS51126700A true JPS51126700A (en) 1976-11-04

Family

ID=24240613

Family Applications (1)

Application Number Title Priority Date Filing Date
JP51032368A Pending JPS51126700A (en) 1975-03-24 1976-03-24 Aeroplane trailing edge flap mounting mechanism

Country Status (5)

Country Link
JP (1) JPS51126700A (en)
DE (1) DE2611918A1 (en)
FR (1) FR2305342A1 (en)
GB (5) GB1547903A (en)
IT (1) IT1057415B (en)

Cited By (1)

* 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

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Cited By (2)

* 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
JPH0378319B2 (en) * 1985-11-14 1991-12-13 Nippon Kokuki Kaihatsu Kyokai

Also Published As

Publication number Publication date
GB1547902A (en) 1979-06-27
GB1547904A (en) 1979-06-27
FR2305342A1 (en) 1976-10-22
GB1547901A (en) 1979-06-27
DE2611918A1 (en) 1976-11-11
IT1057415B (en) 1982-03-10
GB1547905A (en) 1979-06-27
GB1547903A (en) 1979-06-27

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