GB2137569B - Leading edge arrangements for aircraft wings - Google Patents

Leading edge arrangements for aircraft wings

Info

Publication number
GB2137569B
GB2137569B GB08407869A GB8407869A GB2137569B GB 2137569 B GB2137569 B GB 2137569B GB 08407869 A GB08407869 A GB 08407869A GB 8407869 A GB8407869 A GB 8407869A GB 2137569 B GB2137569 B GB 2137569B
Authority
GB
United Kingdom
Prior art keywords
leading edge
aircraft wings
edge arrangements
arrangements
wings
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
GB08407869A
Other versions
GB2137569A (en
GB8407869D0 (en
Inventor
John Brooke Clifford-Jones
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 Aerospace PLC filed Critical British Aerospace PLC
Priority to GB08407869A priority Critical patent/GB2137569B/en
Publication of GB8407869D0 publication Critical patent/GB8407869D0/en
Publication of GB2137569A publication Critical patent/GB2137569A/en
Application granted granted Critical
Publication of GB2137569B publication Critical patent/GB2137569B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • 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
    • Y02T50/10—Drag reduction
    • 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
GB08407869A 1983-03-30 1984-03-27 Leading edge arrangements for aircraft wings Expired GB2137569B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08407869A GB2137569B (en) 1983-03-30 1984-03-27 Leading edge arrangements for aircraft wings

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8308821 1983-03-30
GB08407869A GB2137569B (en) 1983-03-30 1984-03-27 Leading edge arrangements for aircraft wings

Publications (3)

Publication Number Publication Date
GB8407869D0 GB8407869D0 (en) 1984-05-02
GB2137569A GB2137569A (en) 1984-10-10
GB2137569B true GB2137569B (en) 1986-03-12

Family

ID=26285685

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08407869A Expired GB2137569B (en) 1983-03-30 1984-03-27 Leading edge arrangements for aircraft wings

Country Status (1)

Country Link
GB (1) GB2137569B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4650140A (en) * 1985-12-30 1987-03-17 The Boeing Company Wind edge movable airfoil having variable camber
US5544847A (en) * 1993-11-10 1996-08-13 The Boeing Company Leading edge slat/wing combination
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
GB201121435D0 (en) 2011-12-14 2012-01-25 Airbus Operations Ltd Aircraft wing assembly

Also Published As

Publication number Publication date
GB2137569A (en) 1984-10-10
GB8407869D0 (en) 1984-05-02

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PE20 Patent expired after termination of 20 years