GB1547904A - Mounting mechanism for an airplane wing trailing-edge flaps - Google Patents

Mounting mechanism for an airplane wing trailing-edge flaps

Info

Publication number
GB1547904A
GB1547904A GB47061/78A GB4706178A GB1547904A GB 1547904 A GB1547904 A GB 1547904A GB 47061/78 A GB47061/78 A GB 47061/78A GB 4706178 A GB4706178 A GB 4706178A GB 1547904 A GB1547904 A GB 1547904A
Authority
GB
United Kingdom
Prior art keywords
mounting mechanism
airplane wing
edge flaps
wing trailing
trailing
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
GB47061/78A
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 GB1547904A publication Critical patent/GB1547904A/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
    • B64C9/16—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)
GB47061/78A 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailing-edge flaps Expired GB1547904A (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
GB1547904A true GB1547904A (en) 1979-06-27

Family

ID=24240613

Family Applications (5)

Application Number Title Priority Date Filing Date
GB47062/78A Expired GB1547905A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailing-edge flaps
GB10509/76A Expired GB1547901A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailling-edge flaps
GB47060/78A Expired GB1547903A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailing-edge flaps
GB47059/78A Expired GB1547902A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailling-edge flaps
GB47061/78A Expired GB1547904A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailing-edge flaps

Family Applications Before (4)

Application Number Title Priority Date Filing Date
GB47062/78A Expired GB1547905A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailing-edge flaps
GB10509/76A Expired GB1547901A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailling-edge flaps
GB47060/78A Expired GB1547903A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailing-edge flaps
GB47059/78A Expired GB1547902A (en) 1975-03-24 1976-03-16 Mounting mechanism for an airplane wing trailling-edge flaps

Country Status (5)

Country Link
JP (1) JPS51126700A (en)
DE (1) DE2611918A1 (en)
FR (1) FR2305342A1 (en)
GB (5) GB1547905A (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
FR2305342A1 (en) 1976-10-22
JPS51126700A (en) 1976-11-04
GB1547902A (en) 1979-06-27
GB1547905A (en) 1979-06-27
GB1547901A (en) 1979-06-27
GB1547903A (en) 1979-06-27
IT1057415B (en) 1982-03-10
DE2611918A1 (en) 1976-11-11

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee