公开(公告)号：USD762157S1

公开(公告)日：2016-07-26

申请号：US29498517

申请日：2014-08-05

Applicant: Airbus Defence and Space SAS

Designer： Benjamin Faure ,  Angélique Santerre ,  Jean Philippe Dutheil ,  Christophe Chavagnac ,  Eugénio Ferreira ,  Thierry Pichard

公开(公告)号：US10046868B2

公开(公告)日：2018-08-14

申请号：US14781938

申请日：2014-03-28

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Eugénio Ferreira ,  Angélique Santerre ,  Benjamin Faure ,  Samuel Chevrollier ,  Pierre Parpaite ,  Christophe Favre

IPC: B64G1/62 ,  B64C9/32 ,  B64G1/14 ,  B64C25/10 ,  B64C25/16

Abstract: A spaceplane suitable for aeronautical flight comprising a body and a wing defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters disposed under the lower airfoil surface of same and maneuverable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.

公开(公告)号：US09938025B2

公开(公告)日：2018-04-10

申请号：US14765399

申请日：2014-02-04

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Benjamin Faure ,  Jérôme Bertrand ,  Yohann Coraboeuf ,  Samuel Chevrollier ,  Robert Abadie-La-Haille ,  Pascal Mezieres ,  Angélique Santerre

IPC: B64G1/40 ,  B64D37/30 ,  F17C13/00 ,  B64D37/04 ,  B64D37/06

CPC classification number: B64G1/402 ,  B64D37/04 ,  B64D37/06 ,  B64D37/30 ,  F17C13/00 ,  F17C13/008 ,  F17C2201/0119 ,  F17C2201/054 ,  F17C2205/0192 ,  F17C2221/08 ,  F17C2223/0161 ,  F17C2270/0194 ,  F17C2270/0197

Abstract: A device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first retaining rods for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second retaining rod for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third retaining rod for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank.

公开(公告)号：USD762548S1

公开(公告)日：2016-08-02

申请号：US29498519

申请日：2014-08-05

Applicant: Airbus Defence and Space SAS

Designer： Benjamin Faure ,  Angélique Santerre ,  Jean Philippe Dutheil ,  Christophe Chavagnac ,  Eugénio Ferreira ,  Thierry Pichard

公开(公告)号：US20160069299A1

公开(公告)日：2016-03-10

申请号：US14786143

申请日：2014-04-22

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Fabrice Ruffino ,  Benjamin Faure

IPC: F02K9/84

CPC classification number: F02K9/84 ,  F02K9/56 ,  F05B2240/9121 ,  F05B2250/43

Abstract: A system allowing for the tilting of the rocket motor such that, in the tilted position, the centre of the nozzle is located at least approximately on the neutral orientation axis of said rocket motor.

Abstract translation: 一种允许火箭发动机倾斜的系统，使得在倾斜位置，喷嘴的中心至少位于所述火箭发动机的中立方位轴线上。