Interlayer structure for reducing interlayer strain of double-pulse solid engine

A solid engine, double-pulse technology, applied in the direction of machines/engines, rocket engine devices, mechanical equipment, etc., can solve the problems of large hoop strain, easy damage, weak internal ballistic adjustment ability, etc., to reduce hoop strain, Effect of reducing probability and improving regulation performance

Inactive Publication Date: 2019-12-20
XIAN AEROSPACE PROPULSION TECH INST
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

The radial compartment of the conventional compartment type double-pulse solid motor is as follows figure 1 As shown, the radial compartment A and the axial compartment B are designed with a vertical structure, the structure of the I / II pulse grain is simple, and the adjustment ability of the internal ballistic is weak; under the same quality requirements of the I / II pulse grain, the radial Longer interlayer lengths, resulting in greater hoop strain under pressure and greater susceptibility to failure

Method used

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  • Interlayer structure for reducing interlayer strain of double-pulse solid engine
  • Interlayer structure for reducing interlayer strain of double-pulse solid engine
  • Interlayer structure for reducing interlayer strain of double-pulse solid engine

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Embodiment Construction

[0017] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0018] Such as figure 2 As shown, the interlayer double-pulse solid motor structure includes I pulse igniter 1, II pulse igniter 2, I pulse grain 6, interlayer structure, II pulse grain 3, nozzle 7 and adiabatic shell 8, and the insulation The grain structure separates the grains I pulse grain 6 and grain II pulse grain 3 .

[0019] A kind of interlayer structure that reduces the interlayer strain of double-pulse solid motor provided by this embodiment, such as image 3 As shown, it includes a radial partition 4 and an axial partition 5. The radial partition 4 is wrapped on the inner circumference of the II pulse grain 3, and the radial partition 4 is bonded to the shaft at the axis of the solid motor. To the inner side of the head of the partition layer 5, the overall sealing structure of the partition layer is formed, and the radius length of the bond...

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Abstract

The invention discloses an interlayer structure for reducing interlayer strain of a double-pulse solid engine. The interlayer structure separates a grain into I pulse grains and II pulse grains, the interlayer structure comprises an axial interlayer and a radial interlayer, the radial interlayer is wrapped on the inner circumferential surface of the II pulse grain, the tail part of the radial interlayer is overlapped on the inner side of the head part of the axial interlayer, the axial interlayer is transited from the head part arc to the tail part, and the axial interlayer is wrapped on the opposite end surfaces of the II pulse grain and the I pulse grain. According to the interlayer structure, the hoop strain of the radial interlayer can be reduced, so that the strain of the interlayer of the double-pulse solid engine is reduced.

Description

technical field [0001] The invention relates to the technical field of solid motors, in particular to an interlayer structure for reducing the strain of an interlayer of a double-pulse solid motor. Background technique [0002] In order to meet the power requirements of the new generation of tactical missiles, a dual-pulse solid motor with energy management advantages came into being. By designing the I / II pulse working time and pulse interval time, the energy during the whole working process of the engine can be effectively distributed without increasing the missile In the case of the maximum speed, the average speed of the missile can be effectively increased, which can better meet the energy controllable demand of the missile power plant and improve the combat effectiveness of the missile. [0003] The compartment isolation method is one of the advanced solutions to realize the double pulse technology of solid motor, which has the advantages of light negative mass and hig...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/32F02K9/12
CPCF02K9/12F02K9/32
Inventor 张翔宇利凤祥甘晓松郭运强郜伟伟李青频黄薇薇张兵李泽卫
Owner XIAN AEROSPACE PROPULSION TECH INST
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