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发明公开
CN107264788A 一种高伸展稳定性的多旋翼飞行器主体 无效 - 撤回

一种高伸展稳定性的多旋翼飞行器主体
摘要：
本发明公开了一种高伸展稳定性的多旋翼飞行器主体，属于飞行器技术领域，其目的在于提供一种传动轴伸展时稳定性较高的高伸展稳定性的多旋翼飞行器主体。该飞行器主体包括底盘、底盘中部的顶盖，所述底盘的边缘处设置有轴端连接件，所述轴端连接件的一端连接有传动轴，所述轴端连接件的另一端设置有用于使轴端连接件保持伸展状态的内撑机构。本发明适用于多旋翼飞行器。
摘要（英）：

The invention discloses a multi-rotor aircraft body with high extension stability and belongs to the technical field of aircrafts. The multi-rotor aircraft body with high extension stability is high in stability during extension of a transmission shaft. The aircraft body comprises a chassis and a top cover in the middle of the chassis; the edge of the chassis is provided with a shaft-end connector; one end of the shaft-end connector is connected with a transmission shaft; and the other end of the shaft-end connector is provided with an inner-supporting mechanism used for enabling the shaft-end connector to keep an extension state. The multi-rotor aircraft body with high extension stability is suitable for multi-rotor aircrafts.

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