Large size efficient regenerative cooling nozzle

A high-efficiency regeneration and large-scale technology, which is used in civil, combustion, and aerospace fields, can solve problems such as installation and disassembly difficulties, and achieve the effects of improving work reliability, strength, and feasibility

Active Publication Date: 2019-11-29
BEIJING AEROSPACE PROPULSION INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to overcome the above-mentioned deficiencies of the prior art, to provide a large-scale high-efficiency regenerative cooling nozzle, to improve the regenerative cooling capacity adapted to its area ratio, to improve the processability of the process, to solve the difficulty of process production, and the upstream structure Difficulty in installation and disassembly

Method used

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  • Large size efficient regenerative cooling nozzle
  • Large size efficient regenerative cooling nozzle
  • Large size efficient regenerative cooling nozzle

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Embodiment Construction

[0024] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0025] The invention provides a large-sized high-efficiency regenerative cooling nozzle, which improves the regenerative cooling capacity adapted to its area ratio, improves processability, and solves the problems of difficult process production and difficult installation and disassembly with upstream structures

[0026] Such as figure 1 Shown is a schematic diagram of the overall structure of the nozzle. It can be seen from the figure that the large-scale high-efficiency regenerative cooling nozzle includes the inlet collector 1, the upper part of the nozzle 2, the connecting ring 3, the lower part of the nozzle 4 and the outlet collector 5; among them, the nozzle The upper section 2 is a hollow arc-shaped conical structure; the inlet collector 1 is fixedly installed on the narrow mouth end of the upper section 2 of the nozzle; the lower sectio...

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Abstract

The invention discloses a large-size efficient regenerative cooling spray pipe and relates to the technical fields of aerospace, civil use and combustion. The large-size efficient regenerative coolingspray pipe comprises an inlet collector, a spray pipe upper segment, a connecting ring, a spray pipe lower segment and an outlet collector. The spray pipe upper segment is of a hollow arc-shaped conical structure. The inlet collector is fixedly mounted at the narrow-opening end of the spray pipe upper segment. The spray pipe lower segment is of a hollow arc-shaped conical structure. The narrow-opening end of the spray pipe lower segment is in butt joint with the wide-opening end of the spray pipe upper segment in the axial direction. The outlet collector is fixedly mounted at the wide-openingend of the spray pipe lower segment. The connecting ring is fixedly mounted between the spray pipe upper segment and the spray pipe lower segment. An external medium sequentially flows through a medium inlet, a first inner chamber, radial flow equalizing holes, a second inner chamber, secondary flow equalizing holes and a gap formed between a spray pipe upper segment outer wall and a spray pipe upper segment inner wall and finally flows out of the outlet collector. By means of the large-size efficient regenerative cooling spray pipe, the regenerative cooling capacity matched with the area ofthe spray pipe is increased; technological processability is improved; and the problems that the technological production difficult is high, and a pipe cannot be mounted onto or dismounted from an upstream structure easily are solved.

Description

technical field [0001] The invention relates to the fields of aerospace, civil and combustion technologies, in particular to a large-size high-efficiency regenerative cooling nozzle. Background technique [0002] Regenerative cooling nozzle devices are widely used in aerospace, civil and combustion technology fields. The existing regenerative cooling nozzle device has a relatively small area ratio and a low cooling working pressure, so the structure is relatively simple, and the inner wall and the outer wall are mostly integral structures, and the inner and outer walls are mostly made of the same metal. In addition, the nozzle extension section and the upstream device are mostly welded structures, and once welded to the upstream, they cannot be disassembled. For the nozzle extension section with a large area ratio, if the same connection method is used, it will make later inspection and related work more difficult. Contents of the invention [0003] The purpose of the pre...

Claims

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Application Information

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Patent Type & AuthorityPatents(China)
IPC IPC(8): F02K1/78F02K1/80
CPCF02K1/78F02K1/80F02K1/822F02K9/97F02K9/972
Inventor王仙丁兆波杨继东刘鑫鹏杨岩田原许晓勇孙纪国郑孟伟潘刚刘倩张晋博姬威信赵世红
OwnerBEIJING AEROSPACE PROPULSION INST