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Automatic overturning and docking device for rocket engine

A rocket engine, automatic flip technology, used in metal processing, metal processing equipment, manufacturing tools and other directions, can solve the problems of large overall size, poor stress state, poor structural stability, etc., to achieve good stress state and increase bearing capacity Ability and resistance to deformation, high reliability effect

Active Publication Date: 2021-01-05
太仓臻溢科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The existing overturning docking device has disadvantages such as poor structural stability, large overall size, and poor stress state. Therefore, an overturning docking device with a simple structure, good stress state, high reliability, and stability during the overturning process of large components is urgently needed. Appear

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  • Automatic overturning and docking device for rocket engine
  • Automatic overturning and docking device for rocket engine
  • Automatic overturning and docking device for rocket engine

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Embodiment Construction

[0032] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0033] A rocket engine automatic flip docking device, its structure is as follows figure 1 , figure 2 and image 3 As shown, it includes: a movable base mechanism, a single-degree-of-freedom multi-link mechanism, a frame-type moving platform 8 for placing the target object 10, and a motor screw drive mechanism, a single-degree-of-freedom multi-link mechanism and a motor screw drive The mechanisms are respectively installed on the movable bas...

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Abstract

The invention relates to an automatic overturning and docking device for a rocket engine. The device comprises a movable base mechanism, a single-degree-of-freedom multi-connecting-rod mechanism, a frame type movable platform used for containing a target object and a motor lead screw driving mechanism. The single-degree-of-freedom multi-connecting-rod mechanism and the motor lead screw driving mechanism are installed on the movable base mechanism. The frame type movable platform is installed on the single-degree-of-freedom multi-connecting-rod mechanism and connected with the movable base mechanism through the single-degree-of-freedom multi-connecting-rod mechanism, the motor lead screw driving mechanism drives the single-degree-of-freedom multi-connecting-rod mechanism, 90-degree overturning of the frame type movable platform is achieved, and the target object is overturned to a horizontal state from a vertical state. When the frame type movable platform is in a horizontal state, themulti-connecting-rod mechanism is located at the dead point position. Compared with the prior art, the device has the advantages of being high in reliability and good in stress state, reducing the working space, improving the space utilization rate and the like.

Description

technical field [0001] The invention relates to the technical field of rocket engine docking devices, in particular to a rocket engine automatic flip docking device. Background technique [0002] The use of flipping devices is very extensive. The installation and transfer of large equipment components require the equipment to be flipped 90°, from horizontal to vertical, or from vertical to horizontal. However, due to the large size of the related equipment, during the flipping process It requires stable overturning and strong bearing capacity, which makes it very necessary to design and invent a high-reliability overturning device. For example, for a rocket engine in aerospace, during the assembly process, the engine needs to be placed in a horizontal attitude and assembled with the horizontally placed bazooka segment. Stable and reliable, the flip device needs the feature of high load capacity. [0003] The existing flip-and-butt devices have shortcomings such as poor str...

Claims

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Application Information

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IPC IPC(8): B23P19/00B23P19/10
CPCB23P19/00B23P19/10
Inventor 岳义韦宝琛李研彪
Owner 太仓臻溢科技有限公司
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