The invention belongs to the field of aircraft auxiliary take-off equipment, and particularly relates to an aircraft launching system and an aircraft, and the aircraft launching system comprises a driving part I and a fixed release mechanism; the output end of the driving part I has a circumferential rotation stroke or a linear movement stroke; the fixed release mechanism comprises a support, a fixed release rod and two connecting rods, the support, the fixed release rod and the two connecting rods form a parallelogram mechanism, and the support and the fixed release rod are oppositely arranged; the support is connected with the output end of the driving part I. The fixed release rod is provided with a fixed release structure used for fixing and releasing the aircraft. According to the invention, the fixed release mechanism composed of a parallelogram mechanism is arranged, so that when the aircraft takes off, the fixed release rod descends to make a flight space; the aircraft is prevented from colliding with the fixed release mechanism during takeoff, and the use safety of the launching system is improved.
本发明属于飞行器辅助起飞设备领域,具体是涉及到一种飞行器发射系统及飞行器,其中,飞行器发射系统包括驱动件Ⅰ和固定释放机构;所述驱动件Ⅰ的输出端具有圆周转动行程或直线移动行程;所述固定释放机构包括支座、固定释放杆和两个连接杆,支座、固定释放杆和两个连接杆构成平行四边形机构,其中,支座与固定释放杆相对设置;所述支座与驱动件Ⅰ的输出端连接,所述固定释放杆上设置有用于固定和释放飞行器的固定释放结构,本发明通过设置由平行四边形机构构成的固定释放机构,可以实现在飞行器起飞时,固定释放杆下降,让出飞行空间,防止飞行器起飞时与固定释放机构发生碰撞,提高发射系统的使用安全性。
Aircraft launching system and aircraft
一种飞行器发射系统及飞行器
2023-08-25
Patent
Elektronische Ressource
Chinesisch
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 |
Aircraft launching system, launching method and aircraft
Europäisches Patentamt | 2021
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Engineering Index Backfile | 1946
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