公开(公告)号：US10017264B2

公开(公告)日：2018-07-10

申请号：US14966028

申请日：2015-12-11

Applicant: AIRBUS GROUP SAS

Inventor： Emmanuel Joubert ,  Benoit Ferran ,  Antonin Sanitas ,  Germain Morin

IPC: B64D41/00 ,  B64D27/24 ,  B64D37/02 ,  F02B61/06 ,  F02B65/00 ,  B64D27/02

CPC classification number: B64D27/24 ,  B64D37/02 ,  B64D41/00 ,  B64D2027/026 ,  F02B61/06 ,  F02B65/00 ,  Y02T50/64 ,  Y10S903/951

Abstract: The aircraft (10) includes: at least one electric motor (135); at least one stand-alone electrical power supply (110, 120) supplying power to the electric motor; propulsion elements (130) referred to as “auxiliary propulsion elements”, included in the group including: a stand-alone electrical power supply (130) supplying power to the electric motor, a power supply converting thermal energy into electrical energy and supplying power to the electric motor, and an internal combustion engine; and a structure (100) configured to integrate each electric motor, each stand-alone electrical power supply and the auxiliary propulsion elements, the parameters of the structure being substantially identical regardless of the auxiliary propulsion elements. A method of fitting out such an aircraft is also described.