The invention discloses an ejection seat landing through autorotation rotors and a working method of the ejection seat. The ejection seat comprises blades, a steering engine, a propeller hub, an automatic inclinator, a rotor shaft, a rotor shaft with threads, a seat, an empennage and a propeller tip ejector. The propeller blades are connected with the propeller hub and can be folded forwards; the blade tip ejector is arranged at the tip of the blade; the propeller hub is connected with the automatic inclinator through a connecting rod; the automatic inclinator is connected with the rotor shaft and is mounted on the seat; the empennage is mounted on the seat; the lower portion of the automatic inclinator is connected with a rotor shaft with threads through a bearing and connected with a steering engine through three connecting rods, and the steering engine is fixedly connected to a supporting plane on the rotor shaft; and the automatic inclinator tilts towards all directions. After a pilot catapults, the automatic inclinator and the vertical empennage can be operated to change the course in the flight process, so that the aircraft is far away from a combat area, a mountainous area and a sea surface to reach a safe area.
本发明公开了一种通过自转旋翼降落的弹射座椅及其工作方法,包括:桨叶、舵机、桨毂、自动倾斜器、旋翼轴、带螺纹的旋翼轴、座椅及尾翼、桨尖喷射器;所述桨叶与桨毂连接,桨叶可向前折叠;桨叶桨尖装有桨尖喷射器;桨毂与自动倾斜器通过连杆相连;自动倾斜器与旋翼轴相连并安装在座椅上;尾翼安装于座椅上;所述自动倾斜器的下方与带螺纹的旋翼轴通过轴承连接,并且通过三根连杆与舵机相连,所述舵机固连在旋翼轴上的支撑平面上;使自动倾斜器向各方向倾倒。本发明在飞行员弹射后可以操纵自动倾斜器以及垂直尾翼可以使其在飞行过程中改变航向,从而远离战斗区域、山区以及海面从而到达安全区域。
Ejection seat landing through autorotation rotors and working method of ejection seat
通过自转旋翼降落的弹射座椅及其工作方法
2021-07-09
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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|NTRS | 1986
|Engineering Index Backfile | 1952
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