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：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：US09776740B2

公开(公告)日：2017-10-03

申请号：US14899096

申请日：2014-06-11

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Eugénio Ferreira ,  Christophe Chavagnac

IPC: B64G1/14 ,  B64D27/02 ,  B64G1/48 ,  B64G1/52 ,  B64G1/60 ,  B64D13/06

CPC classification number: B64G1/14 ,  B64D27/023 ,  B64D2013/0618 ,  B64D2013/0681 ,  B64D2027/026 ,  B64D2231/00 ,  B64D2231/02 ,  B64G1/48 ,  B64G1/52 ,  B64G1/60 ,  Y02T50/56

Abstract: An aircraft is capable of passing from the aerial domain to the spatial domain and method for automatically adapting the configuration of same. An additional breathable gas supply is provided to be activated only during a flight phase during which aerobic propulsion is interrupted, and is capable of supplying the control system of the manned cabin environment instead of the system associated with the aerobic propulsion means.

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。