首页> 外国专利> Method and apparatus for assessing the impact of individual parts of a gas turbine component on the overall thermal performance of a gas turbine

Method and apparatus for assessing the impact of individual parts of a gas turbine component on the overall thermal performance of a gas turbine

机译:用于评估燃气轮机部件的各个部分对燃气轮机整体热性能的影响的方法和装置

摘要

A method of determining performance impact of a gas turbine component on overall thermal performance of a gas turbine. The method includes obtaining measured physical condition data for a select gas turbine component part. The measured physical condition data is compared with a predetermined reference value for the select gas turbine component part to determine a deviation of the measured physical condition data with respect to the predetermined reference value. The impact of the deviation on the overall thermal performance of the gas turbine is subsequently determined.
机译:一种确定燃气轮机部件的性能对燃气轮机的整体热性能的影响的方法。该方法包括获得用于选择的燃气轮机部件的测量的身体状况数据。将测得的身体状况数据与用于选择的燃气轮机部件的预定参考值进行比较,以确定测得的身体状况数据相对于预定参考值的偏差。随后确定偏差对燃气轮机整体热性能的影响。

著录项

  • 公开/公告号US2003125906A1

    专利类型

  • 公开/公告日2003-07-03

    原文格式PDF

  • 申请/专利权人 GUAGLARDI PAUL A.;

    申请/专利号US20010028936

  • 发明设计人 PAUL A. GUAGLARDI;

    申请日2001-12-28

  • 分类号G06F11/30;G06F15/00;G21C17/00;

  • 国家 US

  • 入库时间 2022-08-22 00:09:07

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