FR924050A - Perfectionnements aux avions - Google Patents

Perfectionnements aux avions

Info

Publication number
FR924050A
FR924050A FR924050DA FR924050A FR 924050 A FR924050 A FR 924050A FR 924050D A FR924050D A FR 924050DA FR 924050 A FR924050 A FR 924050A
Authority
FR
France
Prior art keywords
upgrades
aircraft
aircraft upgrades
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
Other languages
English (en)
Inventor
Marius-Georges-Henri Girodin
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 filed Critical
Application granted granted Critical
Publication of FR924050A publication Critical patent/FR924050A/fr
Expired legal-status Critical Current

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
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B64C23/076—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. flaps
    • 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)
FR924050D 1946-02-21 1946-02-21 Perfectionnements aux avions Expired FR924050A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR924050T 1946-02-21

Publications (1)

Publication Number Publication Date
FR924050A true FR924050A (fr) 1947-07-24

Family

ID=9439136

Family Applications (1)

Application Number Title Priority Date Filing Date
FR924050D Expired FR924050A (fr) 1946-02-21 1946-02-21 Perfectionnements aux avions

Country Status (1)

Country Link
FR (1) FR924050A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1010380B (de) * 1954-11-22 1957-06-13 Siegfried Ruhnke Leitwerk, insbesondere fuer Flugzeuge
DE1133984B (de) * 1957-06-18 1962-07-26 Snecma Durch Rueckstoss angetriebenes Luftfahrzeug mit ringfoermigem Leitwerk
WO1996040554A1 (fr) * 1995-06-07 1996-12-19 Sundstrand Corporation Turbine a vortex deployable, montee en bout d'aile
WO2011146021A1 (fr) * 2010-05-18 2011-11-24 Pipistrel Podjetje Za Alternativno Letalstvo D.O.O. Commande de lacet autonome et dispositif anti-vrille pour un aéronef à aile fixe

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1010380B (de) * 1954-11-22 1957-06-13 Siegfried Ruhnke Leitwerk, insbesondere fuer Flugzeuge
DE1133984B (de) * 1957-06-18 1962-07-26 Snecma Durch Rueckstoss angetriebenes Luftfahrzeug mit ringfoermigem Leitwerk
WO1996040554A1 (fr) * 1995-06-07 1996-12-19 Sundstrand Corporation Turbine a vortex deployable, montee en bout d'aile
WO2011146021A1 (fr) * 2010-05-18 2011-11-24 Pipistrel Podjetje Za Alternativno Letalstvo D.O.O. Commande de lacet autonome et dispositif anti-vrille pour un aéronef à aile fixe

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