ATE261844T1 - Vorrichtung und verfahren zur beschleunigung der zerstörung von zumindest zwei wirbelschleppen, insbesondere hinter einem flugzeug - Google Patents

Vorrichtung und verfahren zur beschleunigung der zerstörung von zumindest zwei wirbelschleppen, insbesondere hinter einem flugzeug

Info

Publication number
ATE261844T1
ATE261844T1 AT02290329T AT02290329T ATE261844T1 AT E261844 T1 ATE261844 T1 AT E261844T1 AT 02290329 T AT02290329 T AT 02290329T AT 02290329 T AT02290329 T AT 02290329T AT E261844 T1 ATE261844 T1 AT E261844T1
Authority
AT
Austria
Prior art keywords
vortex
destruction
aircraft
volters
trow
Prior art date
Application number
AT02290329T
Other languages
English (en)
Inventor
Alexandre Corjon
Thomas Leweke
Florent Laporte
Original Assignee
Airbus France
Centre Nat Rech Scient
Ile Cerfacs Ct Europ De Rech E
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 Airbus France, Centre Nat Rech Scient, Ile Cerfacs Ct Europ De Rech E filed Critical Airbus France
Application granted granted Critical
Publication of ATE261844T1 publication Critical patent/ATE261844T1/de

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
    • 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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Stored Programmes (AREA)
  • Air Bags (AREA)
  • Looms (AREA)
  • Tires In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AT02290329T 2001-03-01 2002-02-11 Vorrichtung und verfahren zur beschleunigung der zerstörung von zumindest zwei wirbelschleppen, insbesondere hinter einem flugzeug ATE261844T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0102804A FR2821605B1 (fr) 2001-03-01 2001-03-01 Procede et dispositif pour accelerer la destruction d'au moins deux vortex dans le sillage d'un mobile, en particulier d'un avion

Publications (1)

Publication Number Publication Date
ATE261844T1 true ATE261844T1 (de) 2004-04-15

Family

ID=8860614

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02290329T ATE261844T1 (de) 2001-03-01 2002-02-11 Vorrichtung und verfahren zur beschleunigung der zerstörung von zumindest zwei wirbelschleppen, insbesondere hinter einem flugzeug

Country Status (7)

Country Link
US (3) US6719246B2 (de)
EP (1) EP1236641B1 (de)
AT (1) ATE261844T1 (de)
CA (1) CA2370463C (de)
DE (1) DE60200258T2 (de)
ES (1) ES2215973T3 (de)
FR (1) FR2821605B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116176162A (zh) * 2023-01-09 2023-05-30 武汉理工大学 一种动态分裂景观设备

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US20050061921A1 (en) * 2003-09-19 2005-03-24 Egolf Thomas A. Aerodynamic tip protuberances for tip vortex intensity reduction
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DE102005025004B4 (de) * 2005-06-01 2010-05-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zum Abmindern der Zirkulation von Hauptwirbeln in Wirbelschleppen hinter Flugzeugen
EP1746024B1 (de) * 2005-07-22 2007-11-07 Airbus Deutschland GmbH Verfahren zur Steuerung eines Flugzeugs
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US7740206B2 (en) * 2006-04-13 2010-06-22 The Board Of Trustees Of The Leland Stanford Junior University Translating active Gurney flap to alleviate aircraft wake vortex hazard
FR2922189B1 (fr) 2007-10-16 2009-12-18 Airbus France Procede et dispositif pour diminuer les vitesses induites dans des tourbillons de sillage d'un avion.
EP2692632B1 (de) * 2011-03-30 2019-09-04 The Society of Japanese Aerospace Companies Auftriebserhöhende vorrichtung für flugzeuge
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EP3284667B1 (de) * 2016-08-16 2019-03-06 Airbus Operations GmbH Flügelspitzenanordnung mit an einer unterseite befestigten vortilons, flugzeug mit solch einer flügelspitzenanordnung und verwendung von vortilons auf einer flügelspitzenanordnung

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116176162A (zh) * 2023-01-09 2023-05-30 武汉理工大学 一种动态分裂景观设备

Also Published As

Publication number Publication date
ES2215973T3 (es) 2004-10-16
FR2821605B1 (fr) 2003-05-30
EP1236641A1 (de) 2002-09-04
US20050006533A1 (en) 2005-01-13
US20020121576A1 (en) 2002-09-05
FR2821605A1 (fr) 2002-09-06
US20040256521A1 (en) 2004-12-23
CA2370463A1 (fr) 2002-09-01
DE60200258D1 (de) 2004-04-22
DE60200258T2 (de) 2005-03-03
US6719246B2 (en) 2004-04-13
EP1236641B1 (de) 2004-03-17
CA2370463C (fr) 2009-05-12

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