IT7829799A0 - Dispositivo per guidare aerei mediante controllo delle correnti turbolente staccate dai bordi anteriori delle ali. - Google Patents

Dispositivo per guidare aerei mediante controllo delle correnti turbolente staccate dai bordi anteriori delle ali.

Info

Publication number
IT7829799A0
IT7829799A0 IT7829799A IT2979978A IT7829799A0 IT 7829799 A0 IT7829799 A0 IT 7829799A0 IT 7829799 A IT7829799 A IT 7829799A IT 2979978 A IT2979978 A IT 2979978A IT 7829799 A0 IT7829799 A0 IT 7829799A0
Authority
IT
Italy
Prior art keywords
wings
detached
leading edges
guiding aircraft
turbulent currents
Prior art date
Application number
IT7829799A
Other languages
English (en)
Other versions
IT1100244B (it
Original Assignee
Messerschmitt Boelkow Blohm
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 Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Publication of IT7829799A0 publication Critical patent/IT7829799A0/it
Application granted granted Critical
Publication of IT1100244B publication Critical patent/IT1100244B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
IT29799/78A 1977-11-17 1978-11-15 Dispositivo per guidare aerei mediante controllo delle correnti turbolente staccate dai bordi anteriori delle ali IT1100244B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2751361A DE2751361C2 (de) 1977-11-17 1977-11-17 Verfahren zur Flugzeugsteuerung durch Steuerung abgelöster Flügelvorderkanten-Wirbelströme

Publications (2)

Publication Number Publication Date
IT7829799A0 true IT7829799A0 (it) 1978-11-15
IT1100244B IT1100244B (it) 1985-09-28

Family

ID=6023947

Family Applications (1)

Application Number Title Priority Date Filing Date
IT29799/78A IT1100244B (it) 1977-11-17 1978-11-15 Dispositivo per guidare aerei mediante controllo delle correnti turbolente staccate dai bordi anteriori delle ali

Country Status (6)

Country Link
US (1) US4267990A (it)
JP (1) JPS5477999A (it)
DE (1) DE2751361C2 (it)
FR (1) FR2409193A1 (it)
GB (1) GB2008046B (it)
IT (1) IT1100244B (it)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3122137A1 (de) * 1981-06-04 1982-12-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorderkantenklappensystem fuer flugzeugfluegel
JPS58500892A (ja) * 1981-06-10 1983-06-02 ザ　ボ−イング　コンパニ− 翼のための前縁渦フラップ
US4485992A (en) * 1981-09-10 1984-12-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge flap system for aircraft control augmentation
US5114102A (en) * 1989-10-06 1992-05-19 The Boeing Company Boundary layer control
US5255881A (en) * 1992-03-25 1993-10-26 Vigyan, Inc. Lift augmentation for highly swept wing aircraft
US5282591A (en) * 1992-12-21 1994-02-01 The United States Of America As Represented By The Secretary Of The Navy Active vortex control for a high performance wing
US7243881B2 (en) * 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7246770B2 (en) * 2005-02-25 2007-07-24 Northrop Grumman Corporation Aircraft with rotatable leading edge of fuselage and wings
US7216835B2 (en) * 2005-02-25 2007-05-15 Northrop Grumman Corporation Aircraft with extendable leading edge of fuselage and wings
US7204454B2 (en) * 2005-02-25 2007-04-17 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
US7309043B2 (en) * 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7475854B2 (en) * 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US8991768B1 (en) * 2007-10-16 2015-03-31 Aerion Corporation Highly efficient transonic laminar flow wing
US9233755B1 (en) * 2007-10-16 2016-01-12 Aerion Corporation Highly efficient supersonic laminar flow wing structure
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
FR2951434B1 (fr) * 2009-10-20 2012-03-09 Airbus Operations Sas Empennage horizontal d'aeronef muni d'un apex de bord d'attaque
FI122848B (fi) * 2009-11-27 2012-07-31 Raimo Hirvinen Lentolaite

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1290136A (en) * 1917-07-20 1919-01-07 Warren S Eaton Aeroplane.
DE699157C (de) * 1938-07-23 1940-11-23 Dr Paul Hartmann Verschwenkbarer Fluegel
US2503585A (en) * 1945-04-18 1950-04-11 Alfred C Loedding Lift control for aircraft
US3090584A (en) * 1956-08-15 1963-05-21 Power Jets Res & Dev Ltd Aircraft
DE1506598A1 (de) * 1967-05-12 1969-08-07 Lanier Edward Munroe Vorrichtung zur Erhoehung des Auftri?bs bei Luftfahrzeugen
US3480234A (en) * 1967-08-18 1969-11-25 Lockheed Aircraft Corp Method and apparatus for modifying airfoil fluid flow
DE1917532C3 (de) * 1969-04-05 1974-05-30 Dornier Gmbh, 7990 Friedrichshafen Spaltklappenanordnung an Tragflügeln für Luftfahrzeuge
GB1332026A (en) * 1971-08-07 1973-10-03 British Aircraft Corp Ltd Aircraft
US3831885A (en) * 1972-07-11 1974-08-27 W Kasper Aircraft wing with vortex generation
DE2656692C2 (de) * 1976-12-15 1982-07-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Entenflugzeug

Also Published As

Publication number Publication date
JPS5477999A (en) 1979-06-21
GB2008046B (en) 1982-02-24
DE2751361C2 (de) 1984-09-27
IT1100244B (it) 1985-09-28
FR2409193B1 (it) 1983-10-07
DE2751361A1 (de) 1979-05-23
US4267990A (en) 1981-05-19
FR2409193A1 (fr) 1979-06-15
GB2008046A (en) 1979-05-31

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