Treffer 1 - 20 von 271 für Suche 'GALLANT GUILLAUME', Suchdauer: 0,81s Treffer weiter einschränken
  1. 1
    New Methodology for Robust-Optimal Design with Acceptable Risks: An Application to Blended/Wing/Body Aircraft

    New Methodology for Robust-Optimal Design with Acceptable Risks: An Application to Blended/Wing/Body Aircraft von Aubeelack, Hema, Segonds, Stéphane, Bes, Christian, Druot, Thierry, Bérard, Adrien, Duffau, Marylène, Gallant, Guillaume

    Veröffentlicht in AIAA journal

    Volltext
    Artikel

    Zu den Favoriten
    Gespeichert in:
  2. 2
    Surrogate model development for optimized blended-wing-body aerodynamics

    Surrogate model development for optimized blended-wing-body aerodynamics von Aubeelack, Hema, Segonds, Stéphane, Bes, Christian, Druot, Thierry, Brezillon, Joël, Bérard, Adrien, Duffau, Marylène, Gallant, Guillaume

    Veröffentlicht in Journal of aircraft

    Volltext
    Artikel

    Zu den Favoriten
    Gespeichert in:
  3. 3
    Surrogate Model Development for Optimized Blended-Wing-Body Aerodynamics

    Surrogate Model Development for Optimized Blended-Wing-Body Aerodynamics von Aubeelack, Hema, Segonds, Stéphane, Bes, Christian, Druot, Thierry, Brezillon, Joël, Bérard, Adrien, Duffau, Marylène, Gallant, Guillaume

    Veröffentlicht in Journal of aircraft

    Volltext
    Artikel

    Zu den Favoriten
    Gespeichert in:
  4. 4
    STRUCTURE PRIMAIRE D'UN MAT POUR GROUPE PROPULSEUR D'AERONEF COMPORTANT UNE PARTIE PYRAMIDALE A MONTANTS CONVERGENTS

    STRUCTURE PRIMAIRE D'UN MAT POUR GROUPE PROPULSEUR D'AERONEF COMPORTANT UNE PARTIE PYRAMIDALE A MONTANTS CONVERGENTS von GALLANT, GUILLAUME, GLEIZE, OLIVIER

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  5. 5
    Flying wing with side cargo compartment

    Flying wing with side cargo compartment von Delahaye, Romain, Gallant, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  6. 6
    AIRCRAFT ENGINE HAVING AT LEAST ONE REVERSE THRUST SYSTEM ACTUATOR ARRANGED IN A GAS EXHAUST CONE

    AIRCRAFT ENGINE HAVING AT LEAST ONE REVERSE THRUST SYSTEM ACTUATOR ARRANGED IN A GAS EXHAUST CONE von GALLANT, Guillaume, CAZALS, Olivier

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  7. 7
    ENGINE ASSEMBLY FOR AN AIRCRAFT, COMPRISING A FRONT ENGINE MOUNT INCORPORATED WITH THE BOX OF THE MOUNTING PYLON

    ENGINE ASSEMBLY FOR AN AIRCRAFT, COMPRISING A FRONT ENGINE MOUNT INCORPORATED WITH THE BOX OF THE MOUNTING PYLON von GLEIZE, Olivier, GALLANT, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  8. 8
    AIRCRAFT COMPRISING A LINK ROD ONE PART OF WHICH IS MADE OF COMPOSITE

    AIRCRAFT COMPRISING A LINK ROD ONE PART OF WHICH IS MADE OF COMPOSITE von GUILLEMAUT, Julien, GALLANT, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  9. 9
    PRIMARY STRUCTURE OF A PYLON FOR AN AIRCRAFT ENGINE ASSEMBLY COMPRISING A PYRAMIDAL PART WITH CONVERGING UPRIGHT MEMBERS

    PRIMARY STRUCTURE OF A PYLON FOR AN AIRCRAFT ENGINE ASSEMBLY COMPRISING A PYRAMIDAL PART WITH CONVERGING UPRIGHT MEMBERS von Gallant, Guillaume, Gleize, Olivier

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  10. 10
    AIRCRAFT COMPRISING A COMMON STRUCTURE FOR SUPPORTING A POWER PLANT AND A LANDING GEAR ELEMENT

    AIRCRAFT COMPRISING A COMMON STRUCTURE FOR SUPPORTING A POWER PLANT AND A LANDING GEAR ELEMENT von BELLET, Daniel, GALLANT, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  11. 11
    DISPOSITIVO DE FIXAÇÃO DE UM ELEMENTO DE SUSTENTAÇÃO NA FUSELAGEM DE UM AVIÃO

    DISPOSITIVO DE FIXAÇÃO DE UM ELEMENTO DE SUSTENTAÇÃO NA FUSELAGEM DE UM AVIÃO von GUILLAUME GALLANT

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  12. 12
    Device for intermediate fastening between an aircraft fuselage and an aircraft undercarriage

    Device for intermediate fastening between an aircraft fuselage and an aircraft undercarriage von Bellet, Daniel, Gallant, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  13. 13
    Propeller for an aircraft turbomachine, including a blade retaining structure through which the aerodynamic part of each blade passes

    Propeller for an aircraft turbomachine, including a blade retaining structure through which the aerodynamic part of each blade passes von Gallant Guillaume, Guillemaut Julien

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  14. 14
    Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje

    Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje von GALLANT, Guillaume, BIENNES, Hervé

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  15. 15
    Aircraft nose provided with a connecting frame between the landing gear housing and the outer skin of the fuselage

    Aircraft nose provided with a connecting frame between the landing gear housing and the outer skin of the fuselage von Gallant Guillaume, Biennes Herve

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  16. 16
    Current retour network element for aircraft

    Current retour network element for aircraft von Charon, Pierre, Gallant, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  17. 17
    Fish joint device having an improved mechanical hold

    Fish joint device having an improved mechanical hold von Gallant Guillaume, Guillemaut Julien

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  18. 18
    AIRCRAFT WITH REDUCED ENVIRONMENTAL IMPACT

    AIRCRAFT WITH REDUCED ENVIRONMENTAL IMPACT von GALL, Pierre-Emmanuel, GALLANT, Guillaume

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  19. 19
    Method of constructing a fixed-wing aircraft

    Method of constructing a fixed-wing aircraft von Gallant Guillaume, Delahaye Romain

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:
  20. 20
    Device for attaching a lift member to the fuselage of an aircraft

    Device for attaching a lift member to the fuselage of an aircraft von GALLANT GUILLAUME

    Volltext bestellen
    Patent

    Zu den Favoriten
    Gespeichert in:

Suchwerkzeuge: