[go: up one dir, main page]

GB2079688A - Aircraft fitted with wing trailing edge flaps actuated by six-bar mechanisms. - Google Patents

Aircraft fitted with wing trailing edge flaps actuated by six-bar mechanisms. Download PDF

Info

Publication number
GB2079688A
GB2079688A GB8034756A GB8034756A GB2079688A GB 2079688 A GB2079688 A GB 2079688A GB 8034756 A GB8034756 A GB 8034756A GB 8034756 A GB8034756 A GB 8034756A GB 2079688 A GB2079688 A GB 2079688A
Authority
GB
United Kingdom
Prior art keywords
flap
wing
bar mechanism
aircraft according
cruise
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.)
Withdrawn
Application number
GB8034756A
Other languages
English (en)
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.)
Fokker BV
Original Assignee
Fokker BV
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 Fokker BV filed Critical Fokker BV
Publication of GB2079688A publication Critical patent/GB2079688A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
GB8034756A 1980-07-09 1980-10-29 Aircraft fitted with wing trailing edge flaps actuated by six-bar mechanisms. Withdrawn GB2079688A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL8003951A NL8003951A (nl) 1980-07-09 1980-07-09 Vliegtuig, voorzien van vleugels met door middel van zesstangenmechanismen beweegbare kleppen.

Publications (1)

Publication Number Publication Date
GB2079688A true GB2079688A (en) 1982-01-27

Family

ID=19835595

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8034756A Withdrawn GB2079688A (en) 1980-07-09 1980-10-29 Aircraft fitted with wing trailing edge flaps actuated by six-bar mechanisms.

Country Status (4)

Country Link
DE (1) DE3039615A1 (nl)
FR (1) FR2486490A1 (nl)
GB (1) GB2079688A (nl)
NL (1) NL8003951A (nl)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984001343A1 (en) * 1982-09-29 1984-04-12 Boeing Co Folding truss mechanism for trailing edge flaps
US4448375A (en) * 1982-09-29 1984-05-15 The Boeing Company Folding truss mechanism for trailing edge flaps
EP0154047A1 (en) * 1984-03-09 1985-09-11 The Boeing Company Wing flap mechanism
US8070106B2 (en) 2007-11-15 2011-12-06 Airbus Operations Limited Aircraft wing and flap deployment system
US8220755B2 (en) 2008-02-29 2012-07-17 Airbus Operations Limited Hinge rib
CN110294102A (zh) * 2019-04-26 2019-10-01 庆安集团有限公司 一体式襟副翼的复合运动机构
US10864950B2 (en) 2017-12-08 2020-12-15 Mclaren Automotive Limited Moveable underslung wing
CN114455067A (zh) * 2021-11-23 2022-05-10 北京航空航天大学 一种适用于超长襟翼的新型增升装置
CN116374161A (zh) * 2023-05-19 2023-07-04 四川傲势科技有限公司 襟翼收放装置和飞行器
EP4311765A1 (en) * 2022-07-29 2024-01-31 Airbus Operations GmbH Wing assembly comprising a connecting assembly with a first and a second connecting element, wing, and aircraft
CN118494746A (zh) * 2024-07-16 2024-08-16 壹通无人机系统有限公司 一种双铰链襟翼收放机构

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2184342C2 (ru) * 2000-08-15 2002-06-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Аэродинамический руль (варианты)
DE102005016638B4 (de) * 2005-04-11 2010-12-30 Eads Deutschland Gmbh Flügelklappen-Mechanismus zur Verstellung einer einem Tragflügel zugeordneten aerodynamischen Flügelklappe
CN113135283B (zh) * 2021-04-18 2023-01-20 西北工业大学 一种小体积高精度的富勒襟翼作动机构

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984001343A1 (en) * 1982-09-29 1984-04-12 Boeing Co Folding truss mechanism for trailing edge flaps
US4448375A (en) * 1982-09-29 1984-05-15 The Boeing Company Folding truss mechanism for trailing edge flaps
EP0154047A1 (en) * 1984-03-09 1985-09-11 The Boeing Company Wing flap mechanism
US8070106B2 (en) 2007-11-15 2011-12-06 Airbus Operations Limited Aircraft wing and flap deployment system
US8220755B2 (en) 2008-02-29 2012-07-17 Airbus Operations Limited Hinge rib
US10864950B2 (en) 2017-12-08 2020-12-15 Mclaren Automotive Limited Moveable underslung wing
CN110294102A (zh) * 2019-04-26 2019-10-01 庆安集团有限公司 一体式襟副翼的复合运动机构
CN110294102B (zh) * 2019-04-26 2023-05-23 庆安集团有限公司 一体式襟副翼的复合运动机构
CN114455067A (zh) * 2021-11-23 2022-05-10 北京航空航天大学 一种适用于超长襟翼的新型增升装置
CN114455067B (zh) * 2021-11-23 2024-02-09 北京航空航天大学 一种适用于超长襟翼的增升装置
EP4311765A1 (en) * 2022-07-29 2024-01-31 Airbus Operations GmbH Wing assembly comprising a connecting assembly with a first and a second connecting element, wing, and aircraft
US12377960B2 (en) 2022-07-29 2025-08-05 Airbus Operations Gmbh Wing assembly comprising a connecting assembly with a first and a second connecting element, wing, and aircraft
CN116374161A (zh) * 2023-05-19 2023-07-04 四川傲势科技有限公司 襟翼收放装置和飞行器
CN118494746A (zh) * 2024-07-16 2024-08-16 壹通无人机系统有限公司 一种双铰链襟翼收放机构

Also Published As

Publication number Publication date
NL8003951A (nl) 1982-02-01
FR2486490A1 (fr) 1982-01-15
DE3039615A1 (de) 1982-02-11

Similar Documents

Publication Publication Date Title
US3666209A (en) V/stol aircraft with variable tilt wing
EP0407159B1 (en) A flap assembly
US4360176A (en) Wing leading edge slat
US4434959A (en) Airfoil flap assembly with flap track member
US4381093A (en) Flap assembly for aircraft wing
Rudolph High-lift systems on commercial subsonic airliners
US3539133A (en) Inherently stable tapered wing flaperon airplane
US4705236A (en) Aileron system for aircraft and method of operating the same
US5836550A (en) Mechanism for streamwise fowler deployment of the wing trailing or leading edge
EP0100775B1 (en) Wing leading edge slat
US3941334A (en) Variable camber airfoil
US4353517A (en) Flap assembly for aircraft wing
EP2727826B1 (en) Hinged raked wing tip
US20130099060A1 (en) Hinged Raked Wing Tip
GB2038737A (en) Mechanization of expanding radius of usb flap
GB2079688A (en) Aircraft fitted with wing trailing edge flaps actuated by six-bar mechanisms.
US3586262A (en) Foreflapped airfoil
US5495999A (en) Retractable canard wing surfaces for airplanes
US2961196A (en) Folding wing aircraft
US11753149B2 (en) Landing gear door system for a landing gear compartment
USRE32907E (en) Airfoil flap assembly with flap track member
GB2569535A (en) Passively actuated fluid foil
US4132375A (en) Vortex-lift roll-control device
US3799474A (en) Bi-directional deflectible control flap for airfoils
CA3046256A1 (en) Aircraft wing with deployable flap

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)