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发明公开
CN102390531A 一种涵道、机翼组合型微型飞行器 无效 - 撤回

一种涵道、机翼组合型微型飞行器
摘要：
本发明属于一种飞行器，尤其涉及一种可悬停、垂直起降和快速前飞的微型飞行器。包括机体，机翼，起落架，方向舵，飞行驱动装置；所述的机体的机身部布置机翼，机体的尾部布置起落架，机体机尾的后端布置方向舵，飞行驱动装置布置在机体内；其特征在于：所述机体成圆筒形、机体内形成涵道，机体机头的筒径大于机体机尾的筒径；飞行驱动装置布置在机体的涵道内。可以悬停和垂直起降，它在起飞和降落时不需要机场；可以快速前飞，它能在更短时间内到达和离开，可以更好的完成指定任务；具有上述两种飞行方式的控制能力，它能自主完成上述两种不同的飞行方式。
摘要（英）：

The invention belongs to an aircraft, and particularly relates to a micro aircraft which can hover, vertically take off and land and quickly fly forward. The aircraft comprises a body, wings, a takeoff and landing frame, a rudder and a flight driving device, wherein the body part of the body is provided with the wings; the tail part of the body is provided with the takeoff and landing frame; the rear end of the tail of the body is provided with the rudder; the flight driving device is arranged in the body; the aircraft is characterized in that: the body is cylindrical; a duct is formed in the body; drum diameter of head of the body is greater than that of the tail of the body; and the flight driving device is arranged in the duct of the body. The aircraft can hover and vertically take off and land, can take off and land without an airport, can quickly fly forward, can arrive and leave in a shorter time and can better finish a specified task, has a control capacity for the two flight modes and can autonomously finish two different flight modes.

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