The invention provides a jettisonable battery compartment structure of an electric aircraft and the electric aircraft. The jettisonable battery compartment structure comprises a compartment body, a battery pack, a limiting control system and a wire harness. The cabin body comprises a cabin door and a cabin body frame, the battery pack comprises a movement assembly and a wire harness connecting piece, and the limiting control system comprises a battery pack limiter. The cabin body frame comprises a sliding rail, the battery pack is arranged in the cabin body and can move along the sliding rail along with the moving assembly, and the battery pack can be separated from the cabin body in the direction from the sliding rail to the cabin door. The battery pack limiter can limit the battery pack in the cabin body, and the battery pack limiter can release the limit of the battery pack when the battery pack is abnormal. The wire harness is connected to the battery pack through the wire harness connector, and the wire harness can be disconnected from the battery pack when the battery pack is abnormal.
提供了一种电动飞机的可抛式电池舱结构及电动飞机,可抛式电池舱结构包括舱体、电池包、限位控制系统和线束。舱体包括舱门和舱体框架,电池包包括运动组件和线束连接件,限位控制系统包括电池包限位器。舱体框架包括滑轨,电池包设置于舱体内并能够随运动组件沿滑轨运动,电池包能够沿滑轨向舱门的方向脱离舱体。电池包限位器能够形成对电池包在舱体内的限位,并且电池包限位器能够在电池包异常时解除其对电池包的限位。线束经由线束连接件连接到电池包,线束能够在电池包异常时解除其与电池包的连接。
Jettisonable battery compartment structure of electric aircraft and electric aircraft
电动飞机的可抛式电池舱结构及电动飞机
2024-08-16
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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