Slow descent anti-crash aircraft and slow descent method thereof
Slow descent anti-crash aircraft and slow descent method thereof
- Neue Suche nach: LIU SHAOBAO
- Neue Suche nach: LIN YITING
- Neue Suche nach: SUN YUHAN
- Neue Suche nach: WANG ZITONG
- Neue Suche nach: TIAN LANQI
- Neue Suche nach: LIU SHAOBAO
- Neue Suche nach: LIN YITING
- Neue Suche nach: SUN YUHAN
- Neue Suche nach: WANG ZITONG
- Neue Suche nach: TIAN LANQI
The invention provides a slow descent anti-crash aircraft and a slow descent method thereof.The aircraft comprises a fuselage and wings, the fuselage and the wings are connected through tilting assemblies, and the mass ratio of the wings to the fuselage is 10%-40%; a built-in sleeve is fixed in the fuselage, a plurality of gyro directional rotors are mounted in the built-in sleeve, and an engine of the aircraft is connected with the gyro directional rotors and controls the gyro directional rotors to rotate; when the aircraft descends abnormally, the included angle between the wings and the horizontal plane of the fuselage is 60-90 degrees, the front edges of the left and right wings face opposite directions, and the gyroscope orientates the rotor to rotate When the airplane stalls, the falling speed of the airplane can be reduced, the torque generated by rotation of the airplane is balanced, the airplane is prevented from crashing, and casualties of passengers are reduced to the maximum extent.
本发明提供了一种缓降防坠毁飞机及其缓降方法，飞机包括机身和机翼，所述机身和机翼通过倾转组件连接，机翼与机身的质量比为10%至40%；所述机身内固定有内置套筒，内置套筒内安装有若干陀螺定向转子，飞机的发动机与陀螺定向转子连接并控制其旋转；飞机非正常下降时，机翼与机身水平面夹角为60°~90°，左右机翼前缘朝向相反，陀螺定向转子旋转。本发明能够在飞机失速时减缓飞机坠落的速度，平衡飞机旋转产生的扭矩，防止飞机发生坠毁，最大程度减小乘员伤亡。
Dokumentinformationen
Slow descent anti-crash aircraft and slow descent method thereof
缓降防坠毁飞机及其缓降方法
2022-12-30
Patent
Elektronische Ressource
Chinesisch
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