An aircraft launching and rapid turning method is characterized in that a boosting engine device (13) is connected to the tail of a guidance aircraft (1) in a sealed mode through an explosive screw, and the method comprises the following steps that firstly, a turning attitude control device (14) is installed at the front end of the guidance aircraft (1), the end of the guidance aircraft (1) is inserted into the inner space of the turning attitude control device (14), and the turning attitude control device (14) is connected with the guidance aircraft (1); the annular lower end part of the turning attitude control device (14) and the outer wall of the upper part of the guidance aircraft (1) are hermetically mounted together through explosion screws; the method is suitable for various guidance aircrafts, the guidance aircrafts can be launched in various vertical or inclined modes of different carriers such as most modern roadbeds, surface ships and underwater submarines, and rapid turning of the guidance aircrafts is achieved.
一种飞行器发射及快速转弯方法,在制导飞行器(1)的尾部用爆炸螺钉密封连接有助推发动机装置(13),其特征在于,包括下列步骤,步骤一、在制导飞行器(1)前端安装一个转弯姿控装置(14),其中制导飞行器(1)的端头插入转弯姿控装置(14)的内部空间,使转弯姿控装置(14)的环形下端部与制导飞行器(1)的上部外壁用爆炸螺钉密封安装在一起;本发明适用于多种制导飞行器,能够满足大部分现代化路基、水面舰艇、水下潜艇等不同载具垂直或倾斜多种方式下发射制导飞行器,并实现制导飞行器的快速转弯。
Aircraft launching and rapid turning method
一种飞行器发射及快速转弯方法
2023-05-02
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft launching system, launching method and aircraft
European Patent Office | 2021
|Launching aircraft electrically
Engineering Index Backfile | 1946
|