The embodiments of the invention provide a lifting device of a carrier rocket and a lifting method of the lifting device. According to the lifting device of the carrier rocket, the carrier rocket is fixed by an embracing arm mechanism in the lifting process of the carrier rocket, and the lifting appliance body can carry the carrier rocket to turn over to the vertical state by controlling the height difference between a first lifting point structure assembly and a second lifting point structure assembly. Compared with the lifting device in the prior art, according to the lifting device of the carrier rocket, a connecting mechanism used for being matched with a lifting appliance can be prevented from being arranged on the carrier rocket, the self weight of the carrier rocket can be reduced, so that the carrying capacity of the carrier rocket can be improved, and the launching cost of the carrier rocket can be reduced. A tray supports the carrier rocket in the axial direction parallel to the carrier rocket, and the reliability of connection between the carrier rocket and the lifting device can be guaranteed. The tray is rotatably connected with the lifting appliance body, so that the lifting appliance body can be prevented from colliding with the carrier rocket when the tray is withdrawn from the lifting appliance body.
本申请实施例提供了一种运载火箭的起吊装置及其起吊方法。在本申请实施例提供的运载火箭的起吊装置中,在运载火箭的起吊过程中抱臂机构固定运载火箭,通过控制第一吊点结构组件与第二吊点结构组件的高度差,能够使得吊具本体携带运载火箭翻转至竖直状态。相较于现有技术中的起吊装置,本申请实施例所提供的运载火箭的起吊装置,能够避免在运载火箭上设置用于配合吊具的连接机构,能够降低运载火箭自身重量,从而能够提高运载火箭的运载能力,降低运载火箭的发射成本。托盘在平行于运载火箭的轴向上承托运载火箭,能够保障运载火箭与起吊装置连接的可靠性。且托盘与吊具本体可转动连接,在撤离吊具本体时,能够避免吊具本体与运载火箭发生磕碰。
Lifting device of carrier rocket and lifting method of lifting device
运载火箭的起吊装置及其起吊方法
2021-09-03
Patent
Electronic Resource
Chinese
IPC: | B66C Krane , CRANES |