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Solid rocket ramjet fuel gas flow regulation device driven by linear motor

A gas flow regulation and ramjet technology, which is applied in rocket engine devices, machines/engines, jet propulsion devices, etc., can solve the problems of gas leakage, slow response speed, large volume, etc., and achieves simple structure, light weight, high precision effect

Inactive Publication Date: 2013-12-04
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although it is beneficial to increase the feedback, it needs to increase the gas source equipment, the structure is complex, the response speed is slow, and because the gas is prone to leakage, it is not easy to achieve precise control in the process of adjusting the gas flow
Wang Yilin of Northwestern Polytechnical University proposed a non-coaxial needle valve type gas flow regulation system, which is driven by a hydraulic system and also has a large volume

Method used

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  • Solid rocket ramjet fuel gas flow regulation device driven by linear motor

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Embodiment

[0022] The present invention is a solid rocket ramjet gas flow regulating device driven by a linear motor. The gas generator 6 is provided with an inner shell structure, the inner shell is hollow, and is equipped with a thermal insulation bushing 3, which is a cylindrical structure. The diameter of the protruding structures at both ends is matched with the inner shell of the gas generator 6. The heat insulating bushing 3 and the inner shell of the gas generator 6 form a cavity. Fixed fit, the other end is a circular hole, the tubular linear motor mover 2 is provided with a coil and a position feedback sensor, the tubular linear motor stator 1 is made of rare earth magnetic steel, and is fixedly connected to one end of the valve stem 4, the valve stem 4 The other end of the valve stem 4 is fixedly connected with the conical valve head 7, the conical valve head 7 extends into the nozzle of the solid fuel gas generator 6, the end of the valve stem 4 close to the conical valve head...

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PUM

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Abstract

The invention discloses a solid rocket ramjet fuel gas flow regulation device driven by a linear motor. The nozzle throat area of a fuel gas generator is changed through the linear motor driving a cone-shaped valve head, and thus the fuel gas flow of the fuel gas generator is regulated; an inner shell structure is formed in the fuel gas generator, a thermal insulation bushing is mounted in an inner shell, the tubular linear motor is arranged in the thermal insulation bushing, a rotor of the linear motor is fixed in the thermal insulation bushing, a stator of the linear motor is fixedly connected with one end of a valve rod, the other end of the valve rod is fixedly connected with the cone-shaped valve head which stretches into a spray pipe of the solid fuel gas generator, one end, close to the cone-shaped valve head, of the valve rod is matched with an inner hole of the thermal insulation bushing, an annular groove is arranged, a movable sealing piece is arranged in the annular groove, and a pressure sensor is mounted at a rear seal head of the fuel gas generator. According to the solid rocket ramjet fuel gas flow regulation device driven by the linear motor, fuel gas flow can be accurately and randomly regulated, the precision is high, the structure is simple and compact, the size is small, the weight is light, and the sealing effect is reliable.

Description

technical field [0001] The invention belongs to the field of solid rocket ramjet, in particular to a solid rocket ramjet gas flow regulating device driven by a linear motor. Background technique [0002] Solid rocket ramjet has the advantages of both ramjet and rocket motor, and has the advantages of specific impulse, small size, light weight, compact structure, reliable operation and low cost. In order to ensure that the engine has the best working performance and good thrust adjustment capability, the solid rocket ramjet should be adjusted for gas flow. At present, there are four main schemes for gas flow regulation: fixed flow type, blocking type, non-blocking type and vortex valve type. The configuration of flow regulating valve usually adopts plunger spool valve, rotary cam valve, rotary disc valve, poppet valve and so on. The existence of the needle valve cone improves the uniformity of the gas velocity, helps the diffusion of the gas, improves the combustion effect ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/08
Inventor 赵泽敏陈雄周俊
Owner NANJING UNIV OF SCI & TECH
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