首页> 外国专利> TEST RIG FOR TESTING THERMAL DURABILITY OF HIGH-TEMPERATURE PART AND TEST SYSTEM AND METHOD USING SAME

TEST RIG FOR TESTING THERMAL DURABILITY OF HIGH-TEMPERATURE PART AND TEST SYSTEM AND METHOD USING SAME

机译:用于测试高温零件热耐久性的试验台和试验系统以及使用该方法的方法

摘要

The present invention provides a test rig for testing the thermal durability of a high-temperature part and a test system and method using the same. The high-temperature part thermal durability test rig comprises a housing having an inlet connected to a combustor for combustion gas inflow and an outlet for combustion gas discharge, a flow path being provided in an accommodating space in the housing and the flow path being a passage for combustion gas circulation, a test body mounting portion provided in the housing, in which a test body including a vane and a blade installed in a gas turbine is mounted to be disposed on the flow path, and an air injection unit for pattern adjustment connected to an air compressor compressing air to imitate a gas turbine operation condition by adjusting the combustion gas temperature distribution in the housing, coupled with the inlet side of the housing, and injecting, into the flow path, cooling air, which is compressed and unheated air supplied from the air compressor.;COPYRIGHT KIPO 2018
机译:本发明提供了一种用于测试高温部件的热耐久性的测试台以及使用该测试台的测试系统和方法。高温部件热耐久性试验台包括壳体,该壳体具有连接至用于燃烧气体流入的燃烧器的入口和用于排出燃烧气体的出口,在壳体的容纳空间中设置有流路,该流路为通道。为了使燃烧气体循环,在壳体上设置有测试体安装部,在该测试体安装部上安装有将叶片和叶片安装在燃气轮机上的测试体,该测试体安装在流路上,并连接有用于图案调整的空气注入单元。通过调节壳体中的燃烧气体温度分布并与壳体的入口侧相连并将压缩空气和未加热空气冷却的空气注入流动路径,该空气压缩机压缩空气以模仿燃气轮机的运行条件由空气压缩机提供。; COPYRIGHT KIPO 2018

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