GB2096551B - A method of optimizing the cruising conditions of aircraft with supercritical wings and an arrangement for carrying out the method - Google Patents

A method of optimizing the cruising conditions of aircraft with supercritical wings and an arrangement for carrying out the method

Info

Publication number
GB2096551B
GB2096551B GB8209016A GB8209016A GB2096551B GB 2096551 B GB2096551 B GB 2096551B GB 8209016 A GB8209016 A GB 8209016A GB 8209016 A GB8209016 A GB 8209016A GB 2096551 B GB2096551 B GB 2096551B
Authority
GB
United Kingdom
Prior art keywords
supercritical
wings
optimizing
aircraft
arrangement
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
GB8209016A
Other languages
English (en)
Other versions
GB2096551A (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.)
Vereinigte Flugtechnische Werke GmbH
Vereinigte Flugtechnische Werke Fokker GmbH
Original Assignee
Vereinigte Flugtechnische Werke GmbH
Vereinigte Flugtechnische Werke Fokker GmbH
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 Vereinigte Flugtechnische Werke GmbH, Vereinigte Flugtechnische Werke Fokker GmbH filed Critical Vereinigte Flugtechnische Werke GmbH
Publication of GB2096551A publication Critical patent/GB2096551A/en
Application granted granted Critical
Publication of GB2096551B publication Critical patent/GB2096551B/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
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/28—Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Control Of Turbines (AREA)
GB8209016A 1981-04-08 1982-03-26 A method of optimizing the cruising conditions of aircraft with supercritical wings and an arrangement for carrying out the method Expired GB2096551B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19813114143 DE3114143A1 (de) 1981-04-08 1981-04-08 "verfahren zur optimierung des reiseflugzustandes von flugzeugen mit transsonischen tragfluegeln sowie vorrichtung zur durchfuehrung des verfahrens"

Publications (2)

Publication Number Publication Date
GB2096551A GB2096551A (en) 1982-10-20
GB2096551B true GB2096551B (en) 1984-07-04

Family

ID=6129655

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8209016A Expired GB2096551B (en) 1981-04-08 1982-03-26 A method of optimizing the cruising conditions of aircraft with supercritical wings and an arrangement for carrying out the method

Country Status (4)

Country Link
DE (1) DE3114143A1 (enrdf_load_stackoverflow)
FR (1) FR2503661B1 (enrdf_load_stackoverflow)
GB (1) GB2096551B (enrdf_load_stackoverflow)
NL (1) NL191460C (enrdf_load_stackoverflow)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4718619A (en) * 1983-07-28 1988-01-12 Ministry Of Defence Manoeuverable supercritical wing section
DE3522448A1 (de) * 1985-06-22 1987-01-02 Messerschmitt Boelkow Blohm Antriebs- und fuehrungsvorrichtung fuer eine an einem flugzeugtragfluegel angeordnete klappe
DE3530865A1 (de) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm Antriebs- und fuehrungsvorrichtung fuer ein an einem flugzeugtragfluegel angeordnetes klappensystem
DE3530862A1 (de) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm Klappenanordnung fuer einen flugzeugtragfluegel
EP0218021B1 (de) * 1985-08-29 1988-06-08 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Klappenanordnung für einen Flugzeugtragflügel
DE3530864A1 (de) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm Klappenanordnung fuer einen flugzeugtragfluegel
US4741503A (en) * 1985-09-26 1988-05-03 The Boeing Company Camber control system
DE3636454A1 (de) * 1985-11-06 1987-05-14 Dornier Gmbh Fluggeraet, insbesondere drehfluegelfluggeraet in der art eines flugschraubers fuer hoehere fluggeschwindigkeiten
DE3641247A1 (de) * 1986-12-03 1988-06-16 Messerschmitt Boelkow Blohm Landeklappenfuehrungsschienen-verkleidung fuer luftfahrzeuge
DE3702294C1 (de) * 1987-01-27 1988-04-14 Messerschmitt Boelkow Blohm Stelleinrichtung fuer Tragflaechenklappen von Flugzeugen
JPH01254491A (ja) * 1988-04-04 1989-10-11 Mitsubishi Heavy Ind Ltd 前縁フラップ装置
JP3180115B2 (ja) 1989-02-27 2001-06-25 良雄 野崎 Ｓｔｏｌ航空機
WO1994026588A1 (en) * 1993-05-06 1994-11-24 Grumman Aerospace Corporation Apparatus and method for controlling the shape of structures
DE4334680C2 (de) * 1993-10-12 1996-07-11 Daimler Benz Aerospace Airbus Vorrichtung zur Verstellung von Spalt-Steuerklappen
DE4422152C2 (de) * 1994-06-27 2000-02-03 Daimler Chrysler Aerospace Verfahren und Anordnung zum Optimieren der aerodynamischen Wirkung eines Tragflügels
US5875998A (en) * 1996-02-05 1999-03-02 Daimler-Benz Aerospace Airbus Gmbh Method and apparatus for optimizing the aerodynamic effect of an airfoil
DE19925560B4 (de) 1999-06-04 2004-04-22 Deutsches Zentrum für Luft- und Raumfahrt e.V. Zusatzflügel für Hauptflügel von Flugzeugen
US6390417B1 (en) * 1999-06-30 2002-05-21 Honda Giken Kogyo Kabushiki Kaisha Drag control system for flying machine, process for estimating drag of flying machine, boundary layer control system, and boundary layer control process
GB0114634D0 (en) 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
DE10351839B3 (de) * 2003-11-06 2005-06-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Minimierung des Widerstands bei einem im Flug befindlichen Flugzeug
DE10361891A1 (de) * 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen
DE102004040313B4 (de) 2004-08-19 2008-02-21 Airbus Deutschland Gmbh System zum Einstellen der spannweitigen Lastverteilung eines Tragflügels
DE102006058650B4 (de) * 2006-12-11 2009-11-19 Eads Deutschland Gmbh Tragflügel eines Flugzeugs
US7641152B2 (en) 2007-04-13 2010-01-05 The Boeing Company Dynamic adjustment of wing surfaces for variable camber
FR2915303B1 (fr) * 2007-04-23 2011-04-29 Airbus France Dispositif et procede de protection contre les intrusions dans les logements de train d'un aeronef
DE102008056655A1 (de) 2008-11-10 2010-05-27 Airbus Deutschland Gmbh Flügel mit einer Stellklappe und einer Spaltabdeckungs-Vorrichtung und Verstellmechanismus für eine Spaltabdeckungs-Vorrichtung
US9108715B2 (en) * 2012-05-29 2015-08-18 The Boeing Company Rotary actuated high lift gapped aileron

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3904152A (en) * 1974-03-13 1975-09-09 Lockheed Aircraft Corp Variable area, variable camber wing for aircraft
US3944170A (en) * 1974-06-20 1976-03-16 Ltv Aerospace Corporation Apparatus for producing pivotal movement
DE2458531A1 (de) * 1974-12-11 1976-06-16 Wolfgang Mehrle Messinstrument zur ermittlung optimaler einstellungen fuer leistungssteigernde systeme bei flugzeugen
FR2374208A1 (fr) * 1976-12-17 1978-07-13 Morin Bernard Aile a profil variable, notamment pour aerodyne
GB2003098B (en) * 1977-07-07 1982-01-27 British Aircraft Corp Ltd Aircraft wings
US4189120A (en) * 1977-12-14 1980-02-19 Boeing Commercial Airplane Company Variable camber leading edge flap
US4247066A (en) * 1978-02-21 1981-01-27 General Dynamics Corporation Airfoil variable cambering device and method
DE2907912C2 (de) * 1979-03-01 1985-06-05 Dornier Gmbh, 7990 Friedrichshafen Quertriebskörper mit veränderbarer Profilierung, insbesondere Nasenteile von Flugzeugtragflügeln
GB2060520B (en) * 1979-10-19 1983-05-05 British Aerospace Variable camber wings

Also Published As

Publication number Publication date
NL191460C (nl) 1995-07-18
DE3114143A1 (de) 1982-10-28
FR2503661A1 (fr) 1982-10-15
DE3114143C2 (enrdf_load_stackoverflow) 1989-04-27
GB2096551A (en) 1982-10-20
NL191460B (nl) 1995-03-16
NL8105237A (nl) 1982-11-01
FR2503661B1 (fr) 1988-04-08

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Legal Events

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

Effective date: 20010326