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 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 (en) 1981-04-08 1981-04-08 "METHOD FOR OPTIMIZING THE TRAVEL FLIGHT CONDITION OF AIRCRAFT WITH TRANSPARENT ELBOWS AND DEVICE FOR IMPLEMENTING THE PROCESS"

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 (en)
FR (1) FR2503661B1 (en)
GB (1) GB2096551B (en)
NL (1) NL191460C (en)

Families Citing this family (26)

* 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 (en) * 1985-06-22 1987-01-02 Messerschmitt Boelkow Blohm DRIVE AND GUIDE DEVICE FOR A FLAP ARRANGED ON AN AIRCRAFT WING
DE3530865A1 (en) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm DRIVE AND GUIDE DEVICE FOR A FLAP SYSTEM ARRANGED ON AN AIRCRAFT WING
EP0218021B1 (en) * 1985-08-29 1988-06-08 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Flaps arrangement for an aircraft wing
DE3530862A1 (en) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm FLAP ARRANGEMENT FOR AN AIRCRAFT WING
DE3530864A1 (en) * 1985-08-29 1987-03-12 Messerschmitt Boelkow Blohm Flap arrangement for an aircraft mainplane
US4741503A (en) * 1985-09-26 1988-05-03 The Boeing Company Camber control system
DE3636454A1 (en) * 1985-11-06 1987-05-14 Dornier Gmbh Aircraft, especially a rotary-wing aircraft of the helicopter type, for relatively high airspeeds
DE3641247A1 (en) * 1986-12-03 1988-06-16 Messerschmitt Boelkow Blohm LANDING VALVE GUIDE RAIL FAIRING FOR AIRCRAFT
DE3702294C1 (en) * 1987-01-27 1988-04-14 Messerschmitt Boelkow Blohm Actuator for wing flaps of aircraft
JPH01254491A (en) * 1988-04-04 1989-10-11 Mitsubishi Heavy Ind Ltd Front edge flap device
DE69425654T2 (en) * 1993-05-06 2000-12-28 Northrop Grumman Corp., Los Angeles DEVICE AND METHOD FOR CHANGING THE FORM OF A STRUCTURE
DE4334680C2 (en) * 1993-10-12 1996-07-11 Daimler Benz Aerospace Airbus Device for adjusting gap control flaps
DE4422152C2 (en) * 1994-06-27 2000-02-03 Daimler Chrysler Aerospace Method and arrangement for optimizing the aerodynamic effect of a wing
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 (en) 1999-06-04 2004-04-22 Deutsches Zentrum für Luft- und Raumfahrt e.V. Additional wing for main wing of aircraft
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 (en) * 2003-11-06 2005-06-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for minimizing the resistance of an aircraft in flight
DE10361891A1 (en) * 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Device for controlling and adjusting flaps on aircraft wings
DE102004040313B4 (en) * 2004-08-19 2008-02-21 Airbus Deutschland Gmbh System for adjusting the spanwise load distribution of a wing
DE102006058650B4 (en) * 2006-12-11 2009-11-19 Eads Deutschland Gmbh Wing of an airplane
US7641152B2 (en) * 2007-04-13 2010-01-05 The Boeing Company Dynamic adjustment of wing surfaces for variable camber
FR2915303B1 (en) * 2007-04-23 2011-04-29 Airbus France DEVICE AND METHOD FOR PROTECTION AGAINST INTRUSIONS IN AIR TRAIN HOUSING
DE102008056655A1 (en) 2008-11-10 2010-05-27 Airbus Deutschland Gmbh Wing with a flap and a gap cover device and adjustment mechanism for a gap cover device
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 (en) * 1974-12-11 1976-06-16 Wolfgang Mehrle Aircraft lift coefficient sensor - has speed and area loading input to adjust per-formance of aircraft
FR2374208A1 (en) * 1976-12-17 1978-07-13 Morin Bernard Aircraft wing with variable aerodynamic profile - has flexible wing surface controlled by fuel under pressure pumped between tanks
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 (en) * 1979-03-01 1985-06-05 Dornier Gmbh, 7990 Friedrichshafen Transverse drive body with variable profiling, in particular nose parts of aircraft wings
GB2060520B (en) * 1979-10-19 1983-05-05 British Aerospace Variable camber wings

Also Published As

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

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Legal Events

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

Effective date: 20010326