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GB2311969B - Variable camber wing mechanism - Google Patents

Variable camber wing mechanism

Info

Publication number
GB2311969B
GB2311969B GB9621194A GB9621194A GB2311969B GB 2311969 B GB2311969 B GB 2311969B GB 9621194 A GB9621194 A GB 9621194A GB 9621194 A GB9621194 A GB 9621194A GB 2311969 B GB2311969 B GB 2311969B
Authority
GB
United Kingdom
Prior art keywords
wing mechanism
variable camber
camber wing
variable
wing
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 - Fee Related
Application number
GB9621194A
Other versions
GB2311969A (en
GB9621194D0 (en
Inventor
Michael Craig Broadbent
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB9621194D0 publication Critical patent/GB9621194D0/en
Priority to JP9536833A priority Critical patent/JPH11509804A/en
Priority to US08/973,260 priority patent/US6015117A/en
Priority to PCT/GB1997/000979 priority patent/WO1997038900A1/en
Publication of GB2311969A publication Critical patent/GB2311969A/en
Application granted granted Critical
Publication of GB2311969B publication Critical patent/GB2311969B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB9621194A 1996-04-13 1996-10-11 Variable camber wing mechanism Expired - Fee Related GB2311969B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP9536833A JPH11509804A (en) 1996-04-13 1997-04-09 Variable camber wing mechanism
US08/973,260 US6015117A (en) 1996-04-13 1997-04-09 Variable camber wing mechanism
PCT/GB1997/000979 WO1997038900A1 (en) 1996-04-13 1997-04-09 Variable camber wing mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9607707.8A GB9607707D0 (en) 1996-04-13 1996-04-13 A self-sealing parallelogram slat mechanism

Publications (3)

Publication Number Publication Date
GB9621194D0 GB9621194D0 (en) 1996-11-27
GB2311969A GB2311969A (en) 1997-10-15
GB2311969B true GB2311969B (en) 1999-09-22

Family

ID=10792032

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9607707.8A Pending GB9607707D0 (en) 1996-04-13 1996-04-13 A self-sealing parallelogram slat mechanism
GB9621194A Expired - Fee Related GB2311969B (en) 1996-04-13 1996-10-11 Variable camber wing mechanism

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB9607707.8A Pending GB9607707D0 (en) 1996-04-13 1996-04-13 A self-sealing parallelogram slat mechanism

Country Status (1)

Country Link
GB (2) GB9607707D0 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0012176D0 (en) * 2000-05-20 2000-07-12 Broadbent Michael C Deployment system for a moveable wing surface
GB0810724D0 (en) 2008-06-12 2008-07-16 Airbus Uk Ltd Slat assembly
GB201121447D0 (en) 2011-12-14 2012-01-25 Airbus Operations Ltd Translating cable device sealing
GB201214143D0 (en) 2012-08-08 2012-09-19 Airbus Operations Ltd Slat support and deployment coupling

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB298508A (en) * 1927-07-09 1928-10-09 Frederick Handley Page Improvements in means for controlling aeroplanes
US3847369A (en) * 1973-03-08 1974-11-12 Us Navy Control surface deployment mechanism
EP0188823A1 (en) * 1984-12-31 1986-07-30 The Boeing Company Closing device for an airfoil
GB2186849A (en) * 1986-02-19 1987-08-26 British Aerospace Leading edge arrangements for aircraft wings
GB2204538A (en) * 1987-05-06 1988-11-16 British Aerospace Wing leading edge arrangements
EP0322172A2 (en) * 1987-12-19 1989-06-28 British Aerospace Public Limited Company Wing leading edge arrangements for aircraft
US5044580A (en) * 1989-05-09 1991-09-03 British Aerospace Plc Flexible closing device for a wing leading edge
GB2260521A (en) * 1991-10-19 1993-04-21 British Aerospace An aircraft wing leading edge arrangement
WO1996009955A1 (en) * 1994-09-29 1996-04-04 West-Walker, Francis, Nigel Linkage to deploy a surface relative to a wing

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB298508A (en) * 1927-07-09 1928-10-09 Frederick Handley Page Improvements in means for controlling aeroplanes
US3847369A (en) * 1973-03-08 1974-11-12 Us Navy Control surface deployment mechanism
EP0188823A1 (en) * 1984-12-31 1986-07-30 The Boeing Company Closing device for an airfoil
GB2186849A (en) * 1986-02-19 1987-08-26 British Aerospace Leading edge arrangements for aircraft wings
GB2204538A (en) * 1987-05-06 1988-11-16 British Aerospace Wing leading edge arrangements
EP0322172A2 (en) * 1987-12-19 1989-06-28 British Aerospace Public Limited Company Wing leading edge arrangements for aircraft
US5044580A (en) * 1989-05-09 1991-09-03 British Aerospace Plc Flexible closing device for a wing leading edge
GB2260521A (en) * 1991-10-19 1993-04-21 British Aerospace An aircraft wing leading edge arrangement
WO1996009955A1 (en) * 1994-09-29 1996-04-04 West-Walker, Francis, Nigel Linkage to deploy a surface relative to a wing

Also Published As

Publication number Publication date
GB9607707D0 (en) 1996-06-19
GB2311969A (en) 1997-10-15
GB9621194D0 (en) 1996-11-27

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Legal Events

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

Effective date: 20001011