The invention discloses a rocket locking mechanism with a guiding function. The mechanism comprises a base. A rotating arm is hinged to the base; a first locking device and a second locking device which are oppositely arranged are fixedly arranged on the rotating arm; a guide block is arranged on the rotating arm; the rotating arm has a guide position and a locking position relative to the base; and when the rotating arm is located at the guiding position, a rocket is guided through the guiding block, the rotating arm and the base are fixed through a third locking device, and when the rotatingarm is located at the locking position, the rocket is locked through the first locking device and the second locking device, and the rotating arm and the base are fixed through a fourth locking device. According to the rocket locking mechanism with the guiding function, guiding and positioning can be provided for the rocket in a rocket hoisting process, and the rocket can be locked in a rocket transportation process.
本发明公开了一种具有导向功能的锁箭机构,其包括底座,底座上铰接有转臂,转臂上固定设有相对布置的第一锁紧装置和第二锁紧装置,转臂上设有导向块,转臂相对于底座具有导向位置和锁紧位置,当转臂处于导向位置时通过导向块对火箭进行导向并且转臂与底座之间通过第三锁紧装置固定,当转臂处于锁紧位置时通过第一锁紧装置和第二锁紧装置对火箭进行锁紧并且转臂与底座之间通过第四锁紧装置固定。其目的是为了提供一种具有导向功能的锁箭机构,其既能在火箭吊装过程中为火箭提供导向定位,也能在火箭运输过程中将火箭锁紧。
Rocket locking mechanism with guiding function
一种具有导向功能的锁箭机构
2020-11-20
Patent
Electronic Resource
Chinese
IPC: | B60P Fahrzeuge zum Transport von Lasten oder zum Befördern, Tragen oder Aufnehmen besonderer Lasten oder Gegenstände , VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS |
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