T
Thierry Druot
Researcher at Airbus
Publications - 23
Citations - 123
Thierry Druot is an academic researcher from Airbus. The author has contributed to research in topics: Fuselage & Airplane. The author has an hindex of 7, co-authored 20 publications receiving 115 citations. Previous affiliations of Thierry Druot include Airbus Operations S.A.S. & École nationale de l'aviation civile.
Papers
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Patent
Aircraft with yaw control by differential drag
Olivier Cazals,Thierry Druot +1 more
TL;DR: In this paper, an aircraft with an elongated fuselage and a lifting surface fastened to the fuselage has a device for controlling the torque around the yaw axis GZ of the aircraft in which aerodynamic forms that have devices to generate aerodynamic drag are fastened on each end of the lifting surface at non-zero distances from each side of a vertical plane of symmetry XZ.
Patent
Aircraft with its fuselage suspended under the wing
Olivier Cazals,Thierry Druot +1 more
TL;DR: In this paper, an aircraft displaying a fuselage, a wing attached to the fuselage in an upper part and in a middle part along the length of the aircraft, a set of airfoils situated behind the wing and propulsion engines mounted on the wing.
Patent
Aircraft with a wing movable along the longitudinal axis of the fuselage
Olivier Cazals,Thierry Druot +1 more
TL;DR: In this paper, the wing is mounted to be movable longitudinally in translation relative to the fuselage between an extreme forward position Xav and an extreme rearward position Xar, so that the center of gravity of the aircraft can be displaced longitudeally to be positioned precisely at any time relative to point of application of the resultant of the aerodynamic lift forces.
Proceedings ArticleDOI
Aero-structural approach coupled with direct operative cost optimization for new aircraft concept in preliminary design
Patent
Airplane with pitch and yaw command by propulsion system
Olivier Cazals,Thierry Druot +1 more
TL;DR: In this paper, two swiveling engines are attached to the fuselage of an aircraft by struts to generate pitch and yaw torques, and the engines also include pods provided with jet deflection flaps.