The invention relates to an aircraft propulsion assembly comprising: at least one first support (62) supporting an electric propulsion system (46); at least one first attachment (64) configured to connect the first support (62) and a support structure (42) of the aircraft; at least one second support (68), different and separate from the first support (62), supporting a source of electrical energy (50) configured to power the electric propulsion system (46); and at least one second attachment (70) configured to connect the second support (68) and the support structure (42). The invention also relates to an aircraft comprising at least one such propulsion assembly. Since the second support (68) and the first support (62) are distinct and separate from each other, vibrations generated by the electric propulsion system (46) are not transferred to the source (50) of electrical energy.
本发明涉及一种飞行器推进组件,包括:支撑电推进系统(46)的至少一个第一支撑件(62);被构造为连接第一支撑件(62)和飞行器的支撑结构(42)的至少一个第一附接件(64);与第一支撑件(62)不同且分离的至少一个第二支撑件(68),其支撑被构造为向电推进系统(46)供电的电能来源(50);以及被构造为连接第二支撑件(68)和支撑结构(42)的至少一个第二附接件(70)。本发明还涉及一种包括至少一个这种推进组件的飞行器。由于第二支撑件(68)与第一支撑件(62)彼此不同且分离,因而由电推进系统(46)产生的振动不会被传递至电能来源(50)。
Electric propulsion assembly comprising at least two independent supports and aircraft comprising at least one such electric propulsion assembly
包括至少两个独立支撑件的电推进组件和包括至少一个该电推进组件的飞行器
2023-12-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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