发明名称 High fidelity integrated heat transfer and clearance in component-level dynamic turbine system control
摘要 A system comprises a rotary apparatus, a control law and a processor. The rotary apparatus comprises a rotor and a housing forming a gas path therebetween, and the control law controls flow along the gas path. The processor comprises an output module, a plurality of temperature modules, a thermodynamic module, a comparator and an estimator. The output module generates an output signal as a function of a plurality of rotor and housing temperatures defined along the gas path, and the temperature modules determine time derivatives of the rotor and housing temperatures. The thermodynamic module models boundary conditions for the gas path, and the comparator determines errors in the boundary conditions. The estimator estimates the rotor and housing temperatures based on the time derivatives, such that the errors are minimized and the flow is controlled.
申请公布号 US8315741(B2) 申请公布日期 2012.11.20
申请号 US20090552656 申请日期 2009.09.02
申请人 KARPMAN BORIS;MEISNER RICHARD P.;SHADE JOHN L.;UNITED TECHNOLOGIES CORPORATION 发明人 KARPMAN BORIS;MEISNER RICHARD P.;SHADE JOHN L.
分类号 G05D7/00;G05D11/00;G06G7/70 主分类号 G05D7/00
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