초록 ▼

The method serves to determine the vibrational state of turbine blades, arranged on a rotor shaft, mounted such as to rotate in a housing and/or of guide vanes. At least one electromagnetic wave is transmitted into a flow channel in the vicinity of the blades, using means for the generation of at le

The method serves to determine the vibrational state of turbine blades, arranged on a rotor shaft, mounted such as to rotate in a housing and/or of guide vanes. At least one electromagnetic wave is transmitted into a flow channel in the vicinity of the blades, using means for the generation of at least one electromagnetic wave. The electromagnetic waves are at least partly reflected from at least one blade. The reflected part of the at least one electromagnetic wave is received by means for receiving and the vibrational state of the corresponding blade is determined from a signal corresponding to the at least one received electromagnetic wave.

대표청구항 ▼

The invention claimed is: 1. A method for determining stress of at least one turbine blade or vane of a plurality of turbine blades or vanes that are arranged in rows of a turbine machine, comprising: providing at least one electromagnetic wave emitter for emitting at least one electromagnetic emis

The invention claimed is: 1. A method for determining stress of at least one turbine blade or vane of a plurality of turbine blades or vanes that are arranged in rows of a turbine machine, comprising: providing at least one electromagnetic wave emitter for emitting at least one electromagnetic emission wave; providing at least one electromagnetic wave receiver for receiving at least one electromagnetic receive wave; converting the electromagnetic emission wave into the electromagnetic receive wave by at least partially reflecting the electromagnetic emission wave by providing the at least one turbine blade or vane with a reflection surface arranged on a contoured airfoil surface of the blade or vane; arranging the electromagnetic wave emitter and the electromagnetic wave receiver at least one location between the blade or vane rows and operatively connected to the reflection surface of the blade or vane; matching the electromagnetic emission wave to a surface form of the blade or vane; emitting the electromagnetic emission wave by the electromagnetic wave emitter; converting the electromagnetic emission wave into the electromagnetic receive wave by the reflection surface of the blade or vane; receiving the electromagnetic receive wave by the electromagnetic wave receiver; and determining the stress of the blade or vane by frequency analysis to assist in determining component integrity by analyzing the received electromagnetic receive wave to effect an evaluation of the reflection surface by the at least one analyzer. 2. The method according to claim 1, wherein the method is executed to determine the stress of both a turbine blade and a guide vane. 3. The method according to claim 1, wherein analyzing the received electromagnetic wave comprises an evaluation of a surface quality of the reflection surface used for determining the stress. 4. The method according to claim 3, wherein the matched electromagnetic emission wave comprises a wavelength based on a shape of the reflection surface. 5. The method according to claim 3, wherein the evaluation of the surface quality comprises detecting an intensity of the electromagnetic receive wave. 6. The method according to claim 1, wherein analyzing the received electromagnetic wave comprises an evaluation of a vibration status of the reflection surface used for determining the stress. 7. The method according to claim 6, wherein emitting the electromagnetic emission wave comprises at least one electromagnetic emission wave having a wavelength based on a surface shape of the reflection surface. 8. The Method according to claim 6, wherein the evaluation of the vibration status comprises comparing a frequency of the electromagnetic emission wave and to a frequency of the electromagnetic receive wave. 9. The method according to claim 1, wherein analyzing the received electromagnetic wave comprising an evaluation of a surface quality of the reflection surface and an evaluation of a vibration status of the reflection surface, wherein the surface quality and the vibrational status are used for determining the stress. 10. The method according to claim 9, wherein the evaluation of the surface quality and the evaluation of the vibrational status are executed simultaneously. 11. The method according to claim 1, wherein determining the stress of the turbine component is executed while an operation of the turbine machine. 12. The method according to claim 1, wherein the electromagnetic emission wave is a radar wave. 13. A turbine machine, having a device for determining a stress of at least one turbine blade or vane of a plurality of turbine blades or vanes that are arranged in rows of the turbine machine, comprising: at least one electromagnetic wave emitter for emitting at least one electromagnetic emission wave that is matched to a surface form of the blade or vane; at least one electromagnetic wave receiver for receiving at least one electromagnetic receive wave; and at least one analyzer for analyzing the electromagnetic receive wave that evaluates the reflection surface used for determining the stress via frequency analysis, the turbine blade or vane comprising a reflection surface for converting the electromagnetic emission wave into the electromagnetic receive wave by at least partially reflecting the electromagnetic emission wave where the reflection surface is arranged on a contoured airfoil surface of the blade or vane, and the electromagnetic wave emitter and the electromagnetic wave receiver arranged at at least one location between the turbine blade or vane rows and operatively connected to the reflection surface of the turbine blade or vane. 14. The turbine machine according to claim 13, wherein the electromagnetic wave emitter and the electromagnetic wave receiver are operatively connected to the reflection surface such that by emitting the electromagnetic emission wave converting the electromagnetic emission wave into the electromagnetic receive wave and receiving the electromagnetic receive wave occur. 15. The turbine machine according to claim 13, further comprising a housing with a turbine channel in which the component rows are arranged. 16. The turbine machine according to claim 13, wherein the electromagnetic wave emitter comprises an electric vibration generator for generating an electric vibration and a transformer for transforming the electric vibration into the electromagnetic emission wave. 17. The turbine machine according to claim 13, wherein the electromagnetic wave emitter and the electromagnetic wave receiver form one integrated unit. 18. The turbine machine according to claim 13, further comprising a radar antenna included in the electronic wave emitter or in the electronic wave receiver. 19. The turbine machine according to claim 13, wherein the turbine machine is a gas turbine. 20. A device for determining stress of at least one turbine blade or vane of a plurality of turbine blades or vanes that are arranged in rows of the turbine machine, comprising: at least one electromagnetic wave emitter for emitting at least one electromagnetic emission wave that is matched to a surface form of the blade or vane; at least one electromagnetic wave receiver for receiving at least one electromagnetic receive wave; and at least one analyzer for analyzing the electromagnetic receive wave that evaluates the reflection surface used for determining the stress via frequency analysis, the turbine blade or vane comprising a reflection surface for converting the electromagnetic emission wave into the electromagnetic receive wave by at least partially reflecting the electromagnetic emission wave where the reflection surface is arranged on a contoured airfoil surface of the blade or vane, and the electromagnetic wave emitter and the electromagnetic wave receiver sized and configured to be arranged at at least one location between the turbine blade or vane rows and operatively connectable to the reflection surface of the turbine blade or vane.