无人直升机伺服驱动载荷携带和投放机构

Umair Iqbal, Syed Irtiza Ali Shah, Muhammad Salman Sadiq
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引用次数: 2

摘要

无人驾驶飞行器(uav)现在更经常用于民用目的,如监视,测量,监控和运输。无人直升机系统越来越多地用于灾害调查和监测。为了给无人救援直升机的载荷携带和投放提供便利,本文提出了一种伺服驱动的无人救援直升机载荷投放机构设计。提出的有效载荷下降机构由两个伺服电机操作,并使用基于金属齿轮的机构来携带和下降高达9公斤的有效载荷。利用SolidWorks虚拟计算机辅助设计(CAD)平台对所提出的机构进行了建模和跌落试验仿真。提议的机制是专门为CopterWorks直升机平台设计的,可以用于民用操作,携带和投放高达9公斤的有效载荷。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Servo actuated payload carry and drop mechanism for unmanned helicopter
Unmanned Aerial Vehicles (UAVs) are more often used now a days for the civilian purposes such as surveillance, surveying, monitoring, and transportation. Unmanned helicopter systems has been used more often for the disaster surveying and monitoring. In order to provide the facility of carrying and dropping the payload from the helicopter, this paper presents a servo actuated payload drop mechanism design for the unmanned disaster relief helicopter. The proposed payload drop mechanism is operated with two servo motors and uses metallic gears based mechanism to carry and drop the payload of up to 9kg. SolidWorks Virtual Computer Aided Design (CAD) platform has been used for the modelling and drop test simulations of proposed mechanism. The proposed mechanism has been designed specifically for the CopterWorks helicopter platform and can be utilized in civilian operations for the carrying and dropping the payload of up to 9kg.
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