System for control aircraft every single move, turn on one's side, yaw

一种控制飞机俯仰、侧翻、偏航的系统

Abstract

The utility model provides a system for control aircraft every single move, turn on one's side, yaw which the ahead of elevator (1) articulates in the notch at wing trailing edge middle part, is equipped with along long and thin breach (2) of centre -line of aircraft in the front portion of this elevator (1) or all and wing trailing edge, be equipped with in this breach (2) with wing fixed connection, drag iron (3) that are located plane of symmetry of aircraft and extend to aircraft top and below, upper portion and lower part behind this drag iron (3) articulate one direction aileron (4) respectively, leave the notch of elevator (1) luffing motion between two direction aileron (4). The utility model has the advantages that: only use three actuator alright whole three -axis control in order to realize the airborne vehicle. Airborne vehicle to the mixed wing body of the all -wing aircraft of vertical take -off and landing and low aspect ratio, the utility model discloses especially, has the value.
一种控制飞机俯仰、侧翻、偏航的系统,其升降舵(1)的前边铰接在机翼后缘中部的凹口内,在该升降舵(1)的前部或全部以及机翼后缘设有沿飞机中线的细长的缺口(2),在该缺口(2)内设有与机翼固定连接、位于飞机对称面内、并向飞机上方和下方延伸的垂直稳定器(3);在该垂直稳定器(3)后边的上部和下部分别铰接一个方向副翼(4),在两个方向副翼(4)之间留有升降舵(1)上下摆动的凹口。本实用新型的优点是:仅使用三个致动器便可以实现航空器的全部三轴控制。对于垂直起飞和着陆的飞翼和低展弦比的混合翼身的航空器,本实用新型尤其具有利用价值。

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