公开(公告)号：US20160167796A1

公开(公告)日：2016-06-16

申请号：US14966028

申请日：2015-12-11

Applicant: AIRBUS GROUP SAS

Inventor： Emmanuel JOUBERT ,  Benoit FERRAN ,  Antonin SANITAS ,  Germain MORIN

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

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.

Abstract translation: 飞机（10）包括：至少一个电动机（135）; 向所述电动马达供电的至少一个独立电源（110,120）; 被称为“辅助推进元件”的推进元件（130）包括：向电动机供电的独立电源（130），将热能转换成电能并将电力供应到 电动机和内燃机; 以及构造成将每个电动机，每个独立电源和辅助推进元件集成的结构（100），所述结构的参数基本上相同，而与辅助推进元件无关。 还描述了装配这种飞行器的方法。