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Thrust chamber body outer wall structure of liquid propellant rocket engine

A technology of liquid rockets and thrust chambers, applied in rocket engine devices, machines/engines, mechanical equipment, etc., can solve the problems of small pressure loss, good flow uniformity, unsuitable welding process, etc., and achieve small flow resistance loss and flow uniformity Strong ability, good strength and rigidity

Pending Publication Date: 2018-11-16
BEIJING AEROSPACE PROPULSION INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In addition, for the liquid collecting ring on the combustion chamber side of the cylindrical section of the body of the diffusion welded thrust chamber, because it needs to bear a large pressure in the combustion chamber and the axial thrust of the engine, the liquid collecting ring is faced with strength, stiffness, flow equalization Good performance, small pressure loss and many other difficulties; and in order to avoid the thermal influence on the inner wall and outer wall of the thrust chamber, the vicinity of the diffusion welding seam is not suitable for the subsequent welding process again, which is the diffusion welding thrust chamber body. The design and manufacture of the department adds another difficulty

Method used

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  • Thrust chamber body outer wall structure of liquid propellant rocket engine
  • Thrust chamber body outer wall structure of liquid propellant rocket engine

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Embodiment

[0034] An outer wall structure of a thrust chamber of a liquid rocket engine, comprising an outer wall 2 of an expansion section, an outer wall 3 of a throat section, an outer wall 4 of a cylinder section, and an upper cover 5 of a liquid collecting ring. Wherein the outer wall 4 of the cylindrical section has the function of the lower cover of the liquid collecting ring.

[0035] One end of the outer wall 3 of the throat section is connected to the outer wall 2 of the expansion section; the other end of the outer wall 3 of the throat section is connected to the outer wall 4 of the cylindrical section, that is, the outer wall 2 of the expansion section, the outer wall 3 of the throat section, and the outer wall 4 of the cylindrical section are sequentially connected to the outer inner wall 1 After assembly, the outer wall 2 of the expansion section, the outer wall 3 of the throat section, and the outer wall 4 of the cylindrical section are connected by diffusion welding; the ou...

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Abstract

The invention discloses a thrust chamber body outer wall structure of a liquid propellant rocket engine. The structure comprises an expansion section outer wall (2), a throat section outer wall (3), acylindrical section outer wall (4) and a liquid collecting ring upper cover (5); one end of the throat section outer wall (3) is connected with the expansion section outer wall (2), and the other endof the throat section outer wall (3) is connected with the cylindrical section outer wall (4); the cylindrical section outer wall (4) is provided with a radial hole (7) and a liquid collecting tank (6); the liquid collecting ring upper cover (5) is connected with the cylindrical section outer wall (4) to form a liquid collecting cavity (8); and the liquid collecting cavity (8) communicates with an external inner wall groove through the radial hole (7) and the liquid collecting tank (6) in sequence. The outer wall structure has the advantages of good assembly property, improvement of the dispersion welding line quality and the like; and meanwhile, the outer wall structure also achieves the function of a liquid collecting ring, is excellent in flowing uniformity and low in pressure loss, reduces the part number, and improves the reliability of a thrust chamber body part.

Description

technical field [0001] The invention relates to an outer wall structure of a thrust chamber body of a liquid rocket engine, belonging to the field of liquid rocket engines. Background technique [0002] The connection methods of the inner and outer walls of the thrust chamber of modern advanced liquid rocket engines mainly include electroforming and diffusion welding. Compared with the electroforming method, the advantages of diffusion welding are: (1) the outer wall is a layer of high-strength alloy or special steel such as S-06, which has high strength and light weight, which can greatly reduce the weight of the body; (2) the inner and outer walls It can be produced in parallel. During the process of slotting the inner wall with the milling cutter, the outer wall can process the body and the inlet and outlet holes. After that, the welding of the inner wall and the outer wall can be completed in a few days, so the entire production cycle is relatively electroforming. The p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/62
CPCF02K9/62
Inventor 姬威信赵世红丁兆波牛旭东王娟聂嵩孙纪国许晓勇郑孟伟王天泰刘潇
Owner BEIJING AEROSPACE PROPULSION INST
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