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：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：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.