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Method for processing large-cambered-surface volute liquid collector for liquid rocket engine thrust chamber

A volute liquid collector and liquid rocket technology, which is applied in the direction of rocket engine devices, machines/engines, mechanical equipment, etc., can solve the problems of oxide skin shedding, affecting processing progress, and reducing the qualified rate of parts, so as to achieve good parts quality, High processing efficiency and good stability

Active Publication Date: 2016-12-21
湖北三江航天江北机械工程有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] 1) Different positions of the steel pipe are subjected to different forms of force during cold deformation bending. The inner side of the liquid collector is subjected to extrusion force, which causes the side wall thickness to become thicker, and the outer side is subjected to tensile force to cause the side to become thinner. The wall of the liquid collector uneven thickness
In addition, the cold deformation bending process will cause deformation of the section of the liquid collector, which cannot guarantee the roundness of the section of the liquid collector, and the diameter and roundness of the ring of the liquid collector cannot be guaranteed;
[0006] 2) When argon arc welding is used to butt weld the elbow, due to local heating, local deformation will occur at the welding place. In addition, oxide scales may be formed on the inner surface of the welding place, and the risk of excess material will be generated when the oxide scales fall off;
[0007] 3) It is difficult to ensure the consistency of the liquid collector gap by the cutting process, which may lead to problems such as local lamination when welding with other components;
[0008] 4) There are certain defects in the various processes used in the traditional processing method of the liquid collector, which greatly reduces the pass rate of parts production, and the process flow is too cumbersome to affect the processing progress, which is not conducive to the stable production of products

Method used

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  • Method for processing large-cambered-surface volute liquid collector for liquid rocket engine thrust chamber
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  • Method for processing large-cambered-surface volute liquid collector for liquid rocket engine thrust chamber

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Embodiment Construction

[0042] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments, so as to facilitate a clearer understanding of the present invention, but they do not limit the present invention.

[0043] In the following embodiments, the middle circular arc segment cutter, the outer circular arc segment cutter and the inner circular arc segment cutter are all specific cutters, and the special tool seat is also a specific tool seat. like figure 2As shown, the middle circular arc section tool 3 includes a first knife handle and a first truncated circular blade 3.3, the first knife handle includes a first knife handle body 3.1 and a first vertical rod 3.2 vertically connected to the first knife handle body 3.1, The first frusto-conical blade 3.3 is mounted on the end of the first vertical bar 3.2. In order to reduce the cutting resistance, the rounded corner of the first conical blade 3.3 should not be too large, an...

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Abstract

The invention discloses a method for processing a large-cambered-surface volute liquid collector for a liquid rocket engine thrust chamber. Inner cavity arc surfaces are processed by three special cutters and a special cutter base step by step, wherein the middle arc segment cutter performs cutter feeding processing on the inner side of a middle arc segment by a vertical mode; the middle arc segment cutter performs cutter feeding processing on the outer side of the middle arc segment by an inclined mode; the outside arc segment cutter performs cutter feeding processing on an outside arc segment by an inclined mode; and the inside arc segment cutter performs cutter feeding processing on an inside arc segment by a vertical mode. By the step-by-step process, the stability is high and the processing qualified rate of parts can reach more than 98%; and the method is simple in process, high in processing efficiency and suitable for batch production. Compared with the traditional process method, the method for processing the large-cambered-surface volute liquid collector for the liquid rocket engine thrust chamber, provided by the invention, has the advantages that the quality of the parts is higher and the reliability is higher.

Description

technical field [0001] The invention relates to the technical field of processing liquid collectors for thrust chambers of liquid rocket engines, in particular to a method for processing large-arc volute liquid collectors for thrust chambers of liquid rocket engines. Background technique [0002] The liquid rocket engine is the power device of the aerospace vehicle, and the engine thrust chamber is its important component. The thrust chamber is mainly composed of the thrust chamber head, the thrust chamber body and the nozzle extension. The liquid collector is one of the important parts of the thrust chamber. It is a collection device for liquid propellant. Its main function is to collect the propellant before the propellant enters the main structure of the head or body, so as to ensure the uniformity of the propellant entering the main cavity. sex. [0003] The liquid collector in the thrust chamber of liquid rocket engine is mostly made of stainless steel. According to di...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P15/00F02K9/62
CPCB23P15/00F02K9/62
Inventor 吴钦初敬生徐明亮杨勇赵攀
Owner 湖北三江航天江北机械工程有限公司