Material ignition point test assessment device and assessment method

A technology of ignition point and test piece, which is used in measurement devices, analytical materials, thermal analysis of materials, etc., can solve the problems of limited and inability to provide material temperature performance data, and achieve shortened product processing and turnover cycles, sufficient assessment, and good rigidity. Effect

Active Publication Date: 2020-12-15
XIAN AEROSPACE PROPULSION INST
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that the current material temperature performance data is limited, and the existing metal ignition test cannot provide high-temperature, high-pressure and oxygen-enriched conditions, making it difficult to verify the material ignition point, and provides a material ignition point test assessment device and assessment method

Method used

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  • Material ignition point test assessment device and assessment method
  • Material ignition point test assessment device and assessment method
  • Material ignition point test assessment device and assessment method

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Embodiment Construction

[0050] The following embodiments in conjunction with the accompanying drawings and specific embodiments of the present invention will be further described in detail:

[0051] like Figure 1 - Figure 13 , The ignition point of a material testing apparatus comprising a gas generator sequentially assessment communication 1, a water-cooled section 2, the test piece holding section 3, section 4 and the process monitoring lance 5; cooled section 2, the specimen holder section 3, process monitoring section 4 and the nozzle 5 are made of a high temperature alloy.

[0052] A gas generator for providing a temperature high-pressure evaluation test pieces 11 to be oxygen-enriched gas, to assess the performance of the material temperature limit erosion in high pressure gas environment, the temperature of the oxygen-enriched gas may be supplied to the gas generator 1 enriched gas temperature provided to 800K ~ 900K, a pressure of 12 ~ 16MPa, an oxygen content higher than 89%, a flow rate of 100 ...

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Abstract

The invention provides a material ignition point test assessment device and assessment method, and solves the problems that the existing material temperature performance data is limited, and the material ignition point is difficult to verify due to the fact that the existing metal ignition test cannot provide high-temperature and high-pressure oxygen enrichment conditions. The material ignition point test assessment device comprises a fuel gas generator, a water cooling section, a test piece clamping section, a monitoring section and a process spray pipe which are sequentially communicated, wherein the fuel gas generator is used for providing high-temperature and high-pressure oxygen-enriched fuel gas for the test piece to be assessed; the water cooling section is greater than or equal to600 mm and used for improving the uniformity of the fuel gas; temperature sensors and pressure sensors are arranged on the water cooling section and the monitoring section and are used for monitoringthe temperature, pressure and pressure fluctuation conditions of the front and rear parts of the to-be-assessed test piece; the process spray pipe is used for controlling the incoming flow pressure ofthe oxygen-enriched fuel gas; and the water cooling section, the test piece clamping section, the monitoring section and the process spray pipe are all made of a high-temperature alloy material.

Description

Technical field [0001] The present invention is in material properties evaluation test apparatus, particularly relates to an ignition point of a material testing apparatus and assessment evaluation method. Background technique [0002] Liquid propellant rocket engine, certain components (e.g., individual components of a gas path structure: gas pipe, a turbine stator and a rotor, etc.) in a high temperature working environment, with the increase (e.g., engine performance requirements: high performance liquid oxygen kerosene afterburner cycle engine), the working environment of the engine parts are becoming more stringent, the operating temperature is also facing new challenges. [0003] To accommodate more demanding work environment, improve engine performance should be established to acquire all components in a high temperature environment Researchers used on the basis of material properties, but temperature performance data material has been unable to provide powerful data for t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N25/50G01N31/12
CPCG01N25/50G01N31/12
Inventor 赵剑李娟张晟秦红强李鹏飞陈园飞杨永红
Owner XIAN AEROSPACE PROPULSION INST
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