一种飞行器

Aircraft

许振宇; 单肖文; 王浩

许振宇

南方科技大学

南方科技大学

518055 广东省深圳市南山区西丽学苑大道1088号

南方科技大学

518055 广东省深圳市南山区西丽学苑大道1088号 (广东,深圳,南山区)

南方科技大学

518055 广东省深圳市南山区西丽学苑大道1088号 (广东,深圳,南山区)

CN201711000229.5

2017-10-24

CN107757876A

2018-03-06

实质审查 ; 一案双申

2018-03-30

发明申请

First

本发明涉及飞行器设计技术领域，提供了一种飞行器，包括机身、前机翼、后机翼、第一动力组和第二动力组，后机翼与前机翼在x轴方向和z轴方向上均相互错开，第一动力组和第二动力组沿y轴方向对称设置，前机翼上设置有前俯仰调节装置，后机翼上设置有后俯仰调节装置，该前俯仰调节装置和后俯仰调节装置协同工作，用于调节飞行器绕x轴的滚转运动和绕y轴的俯仰运动，使得飞行器可在飞行过程中切换竖直或水平的飞行状态。无论飞行器所带的载荷如何布置，整机重心相对x、y、z任何一个方向都处于上述前、后机翼与前、后俯仰调节装置之间，可提高其操控性和稳定性，以及对不同载荷的适应性，适用于重量分布不均匀的任务载荷。

The invention relates to the technical field of aircraft design and provides an aircraft which comprises a body, a front wing, a rear wing, a first power package, wherein the rear wing and the front wing are staggered in an x-axis direction and a z-axis direction; the first power package and the second power package are arranged symmetrically along a y-axis direction; a front pitching adjustment device is arranged on the front wing; a rear pitching adjustment device is arranged on the rear wing; the front pitching adjustment device and the rear pitching adjustment device cooperate to adjust the rolling motion of the aircraft around the x axis and the pitching motion around the y axis, so that the aircraft can switch between a vertical flight regime and a horizontal flight regime during flight. No matter how the load is allocated on the aircraft, the gravity center of the whole aircraft is located between the front and rear wings and the front and rear pitching adjustment devices, relative to any direction of the x axis, y axis and z axis; thus, the controllability and stability as well as the adaptability to different loads can be improved, and the aircraft is applicable to the mission payloads with non-uniform weight distribution.

B64C3/38 ; B64C1/00

（ENTRY INTO FORCE OF REQUEST FOR SUBSTANTIVE EXAMINATION）[2018-03-30][CN]

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2017-10-24

唐致明

广州嘉权专利商标事务所有限公司

PatSnap

许振宇,单肖文,王浩. 一种飞行器.