초록 ▼

A degradation state of the gas turbine is repeatedly estimated with the aid of a set of measured values, at least one of the measured values not being taken into account in each case during the estimation. A deviating estimate which deviates substantially from the remaining estimates or from an esti

A degradation state of the gas turbine is repeatedly estimated with the aid of a set of measured values, at least one of the measured values not being taken into account in each case during the estimation. A deviating estimate which deviates substantially from the remaining estimates or from an estimate which takes account of all the measured values implies that a measured value which has not been taken into account for this deviating estimate is defective. This renders it possible to distinguish in a simple way between changes in state and measuring errors. In the case of a method for determining a degradation of a gas turbine which is being implemented in any case, the determination of defective sensors according to the invention is possible with a low programming outlay and without assumptions concerning a response of individual sensors.

대표청구항 ▼

1. A method for determining a degradation of a gas turbine, in which a set of measured values y is detected at a measuring instant and a state vector x characterizing the degradation of the gas turbine is calculated from this set of measured values, the method comprising: forming subsets of the s

1. A method for determining a degradation of a gas turbine, in which a set of measured values y is detected at a measuring instant and a state vector x characterizing the degradation of the gas turbine is calculated from this set of measured values, the method comprising: forming subsets of the set of measured values y, and calculating a corresponding state vector x for each subset; assigning each of the subsets and the corresponding state vector x to at least one of the measured values y when the subset does not include the at least one measured value y; and diagnosing as defective a measured value whose assigned state vector or assigned state vectors substantially deviates/deviate from state vectors not assigned to the measured value. 2. The method as claimed in claim 1, wherein in a nominal state of the gas turbine a nominal state vector x0results from nominal measured values y0,and the method comprises: calculating the state vector x for each subset of measured values by determining deviations dy of the measured values y from the nominal measured values y0,and determining a deviation dx of the state vector x from the nominal state x0based on the deviations dy of the measured values y. 3. The method as claimed in claim 2, comprising: calculating the measured values y from the state vector x using a function y=f(x), wherein the function y=f(x) is linearized in a nominal state x0 and a Jacobi matrix J is formed, and determining the deviation dx of the state vector x by multiplying an inverse J-1of the Jacobi matrix J by the deviations dy of the measured values y. 4. The method as claimed in claim 1, comprising: determining the measured values y from the state vector x using a function y=f(x), and determining the state vector x from the measured values y iteratively using a numerical method with the aid of the function y=f(x). 5. The method as claimed in claim 2, comprising: calculating the measured values y from the state vector x using a function y=f(x), and determining the deviation dx of the state vector x from the deviations dy of the measured values y iteratively using a numerical method with the aid of the function y=f(x). 6. The method as claimed in claim 1, wherein a measure Qkof the quality of a kth measured value is essentially determined in accordance with m being a number of states or of elements of a vector dx=(dx,12,dx2,. . . dxm) of deviations of an estimated state x from a nominal state x0,the vector dx being determined taking account of the kth measured value, and the vector dx(k) being determined without taking account of the kth measured value. 7. The method as claimed in claim 1, wherein the set of measured values has measured values of an outlet pressure (PC) and an outlet temperature (TC) of a compressor, an exhaust pressure (PG) and an exhaust temperature (TG) of a turbine and at least one measured value of a mechanical power, a mechanical torque or a fuel mass flow of the gas turbine. 8. The method as claimed in claim 1, comprising: forming the subsets of the measured values from the set of measured values y by cyclically omitting exactly one measured value. 9. A computer readable medium comprising a computer program for causing a computer to execute the method as claimed in claim 1.