Scramjet engine fuel gas analysis high-enthalpy sampling probe

A technology of scramjet and engine, which is applied in the direction of engine testing, machine/structural component testing, measuring devices, etc. It can solve the problems of fast gas speed and difficult comprehensive performance determination, and achieve short processing cycle and satisfy structural strength and heat exchange requirements, the effect of high processing precision

Inactive Publication Date: 2018-06-29
AECC SICHUAN GAS TURBINE RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When evaluating the comprehensive performance of the scramjet combustion chamber, it is difficult to directly determine the comprehensive performance due to the high temperature in the combustion chamber, the fast gas velocity, the influence of the complex shock wave system in the combustion chamber, and mutual coupling

Method used

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  • Scramjet engine fuel gas analysis high-enthalpy sampling probe
  • Scramjet engine fuel gas analysis high-enthalpy sampling probe
  • Scramjet engine fuel gas analysis high-enthalpy sampling probe

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Embodiment Construction

[0030] The high enthalpy sampling probe for scramjet fuel gas analysis in the present invention is suitable for multi-flow gas sampling, and can expand the flow path functionality according to actual engineering requirements. This article mainly takes six-point sampling probes as an example. The engine fuel gas analysis high enthalpy sampling probe is described in detail. The following examples help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be pointed out that for those of ordinary skill in the art, a number of modifications and improvements can be made without departing from the concept of the present invention. These all belong to the protection scope of the present invention. The high enthalpy sampling probe for gas analysis of scramjet engine provided by the present invention is such as Figure 1-6 Shown.

[0031] The described high enthalpy sampling probe for scramjet fuel gas analysi...

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Abstract

The invention belongs to the technical field of aerospace testing, provides a scramjet engine fuel gas analysis high-enthalpy sampling probe, and particularly provides a blow-down scramjet engine combustion device and a fuel gas sampling probe for capturing high-enthalpy fuel gas in engine combustor tests.

Description

Technical field [0001] The invention belongs to the technical field of aerospace testing, and provides a high enthalpy sampling probe for gas analysis of scramjets, and in particular provides a method for capturing reality in the test of temporary impulse scramjet burners and engine combustion chambers. Gas sampling probe for high enthalpy gas. Background technique [0002] In the process of developing hypersonic propulsion, scramjet has always been a focus of attention. When evaluating the comprehensive performance of the scramjet combustion chamber, it is difficult to directly determine the comprehensive performance due to the high temperature in the combustion chamber, the fast gas velocity, and the influence of the complex shock wave system in the combustion chamber. At present, among the existing multiple combustion chamber performance evaluation methods, the sampling method has attracted attention because of its multi-point measurement, simple structure, easy-to-find mater...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/02
CPCG01M15/02
Inventor 张杰朱涛王军刘重阳蒙正猛
Owner AECC SICHUAN GAS TURBINE RES INST
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