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：US09981757B2

公开(公告)日：2018-05-29

申请号：US14901328

申请日：2014-07-04

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Yohann Coraboeuf ,  Jean-Philippe Dutheil

IPC: B64G1/00 ,  B64G1/40 ,  B64G1/14 ,  B64G5/00 ,  F02K9/97 ,  B64F5/50 ,  B64G1/64

CPC classification number: B64G1/401 ,  B64F5/50 ,  B64G1/14 ,  B64G1/641 ,  B64G5/00 ,  F02K9/97 ,  F05D2240/90

Abstract: The invention relates to a propulsion unit for a reusable launch vehicle including a rocket engine supported by a cradle. According to the invention, the cradle includes at least three attachment elements for assembling the unit on the structure of the vehicle to which the unit is to be connected, the at least three attachment elements defining a plane for removing the unit, and in which the unit includes one or more fluid and/or electric links of the engine, each one of the links including a free end to be assembled with a corresponding circuit for supplying the vehicle, to which the unit is to be connected, the tip of at least some of the free ends being contained in the removal plane.

公开(公告)号：US20150344158A1

公开(公告)日：2015-12-03

申请号：US14763299

申请日：2014-01-17

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Eugénio Ferreira ,  Marco Prampolini ,  Yohann Coraboeuf

IPC: B64G1/40 ,  B64G1/14

CPC classification number: B64D33/02 ,  B64D2033/0253 ,  B64D2033/026 ,  B64G1/14 ,  B64G1/40 ,  F02C7/042 ,  F02C7/05

Abstract: According to the invention, said space aircraft comprises, at the front of each of the air inlets of the turbo engines, a mobile flap that can move, in both directions, between a first position for which said flap opens said air inlet and a second position for which said flap prevents air from entering said air inlet.

Abstract translation: 根据本发明，所述太空飞行器在涡轮发动机的每个空气入口的前部包括可移动的翼片，其能够在两个方向上在所述翼片打开所述空气入口的第一位置和第二位置之间移动， 所述挡板防止空气进入所述空气入口的位置。