GB1496518A - Aircraft wings - Google Patents

Aircraft wings

Info

Publication number
GB1496518A
GB1496518A GB4591574A GB4591574A GB1496518A GB 1496518 A GB1496518 A GB 1496518A GB 4591574 A GB4591574 A GB 4591574A GB 4591574 A GB4591574 A GB 4591574A GB 1496518 A GB1496518 A GB 1496518A
Authority
GB
United Kingdom
Prior art keywords
rollers
aircraft
pivoted
oct
tracks
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
GB4591574A
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.)
British Aircraft Corp Ltd
Original Assignee
British Aircraft Corp Ltd
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 British Aircraft Corp Ltd filed Critical British Aircraft Corp Ltd
Priority to GB4591574A priority Critical patent/GB1496518A/en
Publication of GB1496518A publication Critical patent/GB1496518A/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
    • B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

1496518 Aircraft flaps BRITISH AIRCRAFT CORP Ltd 8 Oct 1975 [17 Oct 1974] 45915/74 Heading B7G An aircraft high-lift flap comprises two portions, one 5 mounted on rollers 3 which engage in spanwise spaced tracks 2, the portion being connected at each side by a pivoted radius rod 8 to a fixed arm depending from wing structure, and another portion 6 pivoted by pivots 7 on portion 5. The portion 5 carries at each side an arm 15 connected by a pivoted link 14 to a carriage 13 which is connected to the pivot of roller 3 and guided on the lower flange of the associated track by rollers 11, 12. In operation a chain drive, not shown, drives rollers 3 along the tracks 2, the portion 5 being caused by rods 8 to assume a high-lift attitude. Simultaneously the links 14 cause portion 6 to incline with respect to portion 5.
GB4591574A 1975-10-08 1975-10-08 Aircraft wings Expired GB1496518A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4591574A GB1496518A (en) 1975-10-08 1975-10-08 Aircraft wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4591574A GB1496518A (en) 1975-10-08 1975-10-08 Aircraft wings

Publications (1)

Publication Number Publication Date
GB1496518A true GB1496518A (en) 1977-12-30

Family

ID=10439084

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4591574A Expired GB1496518A (en) 1975-10-08 1975-10-08 Aircraft wings

Country Status (1)

Country Link
GB (1) GB1496518A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4544118A (en) * 1982-09-30 1985-10-01 The Boeing Company Drive mechanism for combined flap-aileron surface
EP0303458A2 (en) * 1987-08-11 1989-02-15 British Aerospace Public Limited Company Trailing edge flaps for aircraft wings
US4881704A (en) * 1987-04-22 1989-11-21 Messerschmitt-Boelkow-Blohm Gmbh Landing flap system
EP0359481A2 (en) * 1988-09-09 1990-03-21 British Aerospace Public Limited Company Fuselage mounted flap drives for wing trailing edge flaps

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4544118A (en) * 1982-09-30 1985-10-01 The Boeing Company Drive mechanism for combined flap-aileron surface
US4881704A (en) * 1987-04-22 1989-11-21 Messerschmitt-Boelkow-Blohm Gmbh Landing flap system
EP0303458A2 (en) * 1987-08-11 1989-02-15 British Aerospace Public Limited Company Trailing edge flaps for aircraft wings
EP0303458A3 (en) * 1987-08-11 1989-11-29 British Aerospace Public Limited Company Trailing edge flaps for aircraft wings
EP0359481A2 (en) * 1988-09-09 1990-03-21 British Aerospace Public Limited Company Fuselage mounted flap drives for wing trailing edge flaps
EP0359481A3 (en) * 1988-09-09 1990-11-07 British Aerospace Public Limited Company Fuselage mounted flap drives for wing trailing edge flaps

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Legal Events

Date Code Title Description
PS Patent sealed
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee