Electric propulsion system for aircraft

An electric propulsion system for an aircraft includes a battery, an electric propulsion assembly, and a power distribution circuit. Each battery is coupled with two or more of the electric propulsion assemblies via a respective one of the power distribution circuits. The electric propulsion assembly is positioned on the aircraft and is operable to apply a balancing force to the aircraft such that, in the event of failure, the aircraft does not experience large variations in roll, pitch, and/or yaw. 一种用于航空器的电动推进系统包括电池、电力推进组件和功率分配电路。每个电池经由功率分配电路中的相应的一个与电力推进组件中的两个或更多个联接。电力推进组件定位在航空器上，并且能够操作以将平衡力施加到航空器，使得在失效的情况下，航空器不会经历横滚、俯仰和/或偏航上的大变化。