发明名称 |
GAS TURBINE GAP ASSESSMENT DEVICE AND GAS TURBINE SYSTEM |
摘要 |
<p>Disclosed is a gas turbine gap assessment device which can assess the clearance of a rotary body and a stationary body precisely, and which does not have a clearance sensor embedded therein, or even if a clearance sensor is embedded therein the installation is minimal. A gap assessment device (15) for assessing a gap between a rotary component and a non-rotary component in accordance with a sensor signal produced by a sensor disposed in a gas turbine (1) comprising the rotary component and the non-rotary component, and in accordance with operation information of the gas turbine, wherein the gap assessment device (15) is provided with: a boundary condition calculation means (15b) for converting the sensor signal and the operation information to a boundary condition for a numerical analysis model; and a numerical analysis means comprising a finite element method numerical analysis model (15c1) for calculating a physical quantity of the gas turbine by using the boundary condition calculated by the boundary condition calculation means, and comprising a gap numerical analysis model (15c2) for calculating a value for the gap between the rotary component and the non-rotary component on the basis of the physical quantity calculated by the finite element method numerical analysis model.</p> |
申请公布号 |
WO2012001726(A1) |
申请公布日期 |
2012.01.05 |
申请号 |
WO2010JP04250 |
申请日期 |
2010.06.28 |
申请人 |
HITACHI, LTD.;HAYASAKA, YASUSHI;SEKIHARA, MASARU;KUROKI, HIDETOSHI |
发明人 |
HAYASAKA, YASUSHI;SEKIHARA, MASARU;KUROKI, HIDETOSHI |
分类号 |
F01D25/00;F01D11/08 |
主分类号 |
F01D25/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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