DE3101847A1 - Flugzeugtragfluegel mit klappenanordnung - Google Patents

Flugzeugtragfluegel mit klappenanordnung

Info

Publication number
DE3101847A1
DE3101847A1 DE19813101847 DE3101847A DE3101847A1 DE 3101847 A1 DE3101847 A1 DE 3101847A1 DE 19813101847 DE19813101847 DE 19813101847 DE 3101847 A DE3101847 A DE 3101847A DE 3101847 A1 DE3101847 A1 DE 3101847A1
Authority
DE
Germany
Prior art keywords
flap
cam
upper skin
skin
fixed 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.)
Granted
Application number
DE19813101847
Other languages
German (de)
English (en)
Other versions
DE3101847C2 (US20110009641A1-20110113-C00256.png
Inventor
David Peter Warton Aerodrome Preston Lancashire Halliday
Barry Sharrock
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
Publication of DE3101847A1 publication Critical patent/DE3101847A1/de
Application granted granted Critical
Publication of DE3101847C2 publication Critical patent/DE3101847C2/de
Granted 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
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single 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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Golf Clubs (AREA)
DE19813101847 1980-01-22 1981-01-21 Flugzeugtragfluegel mit klappenanordnung Granted DE3101847A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8002176 1980-01-22

Publications (2)

Publication Number Publication Date
DE3101847A1 true DE3101847A1 (de) 1981-12-24
DE3101847C2 DE3101847C2 (US20110009641A1-20110113-C00256.png) 1990-05-23

Family

ID=10510821

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19813101847 Granted DE3101847A1 (de) 1980-01-22 1981-01-21 Flugzeugtragfluegel mit klappenanordnung

Country Status (4)

Country Link
US (1) US4395008A (US20110009641A1-20110113-C00256.png)
DE (1) DE3101847A1 (US20110009641A1-20110113-C00256.png)
FR (1) FR2473982A1 (US20110009641A1-20110113-C00256.png)
IT (1) IT1170636B (US20110009641A1-20110113-C00256.png)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2767111A1 (fr) 1997-07-31 1999-02-12 Daimler Benz Ag Aile d'avion equipee d'un volet d'atterrissage

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69718659T2 (de) 1996-10-22 2003-05-22 Boeing Co Flugzeug mit ungepfeiltem schlitzflügel für den reiseflug
US6601801B1 (en) 2002-04-24 2003-08-05 The Boeing Company Gapped trailing-edge control surface for an airfoil
DE102005045759A1 (de) 2005-09-23 2007-04-12 Airbus Deutschland Gmbh Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US9789073B2 (en) 2013-03-14 2017-10-17 Pathak Holdings, Llc Compositions, methods and devices for local drug delivery
US10624865B2 (en) 2013-03-14 2020-04-21 Pathak Holdings Llc Methods, compositions, and devices for drug/live cell microarrays

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2003098A (en) * 1977-07-07 1979-03-07 British Aircraft Corp Ltd Aircraft wings

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836380A (en) * 1955-04-25 1958-05-27 Boeing Co Airplane wing with slotted flap, cove lip door, and spoiler
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
US4015787A (en) * 1975-11-17 1977-04-05 Fairchild Industries Inc. Aircraft wing
US4120470A (en) * 1976-09-28 1978-10-17 The Boeing Company Efficient trailing edge system for an aircraft wing
US4283029A (en) * 1979-01-02 1981-08-11 Rudolph Peter K C Actuating apparatus for a flap system having an upper surface blowing powered lift system

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2003098A (en) * 1977-07-07 1979-03-07 British Aircraft Corp Ltd Aircraft wings

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2767111A1 (fr) 1997-07-31 1999-02-12 Daimler Benz Ag Aile d'avion equipee d'un volet d'atterrissage
US6076775A (en) * 1997-07-31 2000-06-20 Daimlerchrysler Ag Airfoil with a landing flap having a flexible trailing edge

Also Published As

Publication number Publication date
FR2473982B1 (US20110009641A1-20110113-C00256.png) 1984-10-26
DE3101847C2 (US20110009641A1-20110113-C00256.png) 1990-05-23
US4395008A (en) 1983-07-26
IT1170636B (it) 1987-06-03
IT8147595A1 (it) 1982-07-20
IT8147595A0 (it) 1981-01-20
FR2473982A1 (fr) 1981-07-24

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee