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An apparatus and method for a more time efficient measurement of backlash in one or more variable guide vanes of a gas turbine system are provided. A mounting structure, with an indicator attached thereto, may be provided. Further, a guide structure may be provided to allow the mounting structure to

An apparatus and method for a more time efficient measurement of backlash in one or more variable guide vanes of a gas turbine system are provided. A mounting structure, with an indicator attached thereto, may be provided. Further, a guide structure may be provided to allow the mounting structure to be moved adjacent to two or more variable guide vanes without moving the guide structure.

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1. An apparatus for measuring the change in position of a variable guide vane in a turbine system, comprising: an electronic indicator comprising a body and a shaft extending from the body, wherein the electronic indicator measures displacement of the shaft relative to the body and generates an elec

1. An apparatus for measuring the change in position of a variable guide vane in a turbine system, comprising: an electronic indicator comprising a body and a shaft extending from the body, wherein the electronic indicator measures displacement of the shaft relative to the body and generates an electronic signal indicative of the displacement; anda mounting structure configured to be mounted within a casing of the turbine system adjacent to an end of the variable guide vane along an axial direction of the turbine system, wherein the electronic indicator is attached to the mounting structure and the mounting structure is configured to be moved relative to the variable guide vane. 2. An apparatus as in claim 1, wherein the mounting structure comprises: a mounting block; andan indicator block, wherein the indicator block is moveable relative to the mounting block, and wherein the indicator is attached to the indicator block. 3. An apparatus as in claim 1, wherein the mounting structure is configured to be mounted within an inlet duct of the turbine system. 4. An apparatus as in claim 1, further comprising a pivot bar pivotally attached to the mounting structure, wherein a first end of the pivot bar is configured to contact the shaft of the indicator and a second end of the pivot bar is configured to contact the variable guide vane. 5. A system for measuring the change in position of one or more variable guide vanes in a turbine system, comprising: a mounting structure;an indicator attached to the mounting structure, wherein the indicator is configured to measure variable guide vane displacements; anda guide structure configured to be mounted to a surface within a casing of the turbine system adjacent to an end of two or more variable guide vanes along an axial direction of the turbine system, wherein the mounting structure is configured to be moved relative to the guide structure such that the mounting structure is moveable between the two or more variable guide vanes without moving the guide structure. 6. A system. as in claim 5, wherein the mounting structure comprises: a mounting block; andan indicator block, wherein the indicator block is moveable relative to the mounting block, and wherein the indicator is attached to the indicator block. 7. A system as in claim 6, wherein the indicator block, is slidably connected to the mounting block such that the indicator block is capable of moving closer to or further away from the two or more variable guide vanes. 8. A system as in claim 5, further comprising a pivot bar pivotally attached to the mounting structure, wherein a first end of the pivot bar is configured to contact the indicator and a second end of the pivot bar is configured to contact the variable guide vane. 9. A system as in claim 5, wherein the indicator is an electronic indicator configured to generate an electronic signal indicative of the two variable guide vane displacement measurements. 10. A system as in claim 5, wherein the surface within the casing of the turbine system is an inner surface of an inlet duct of the turbine system. 11. A system as in claim 5, wherein the guide structure comprises a first end, a second end, and a first guide rail extending between the first and second ends, wherein the first guide rail has a shape that is complementary to a portion of an inlet duct of the turbine system, and wherein the variable guide vane comprises an inlet guide vane. 12. A system as in claim 11, wherein the first end and the second end each comprise a magnetic mount configured for mounting the guide structure to a casing of the inlet duct. 13. A system as in claim 11, wherein the first end and the second end each comprise an alignment structure configured for aligning the guide structure in an axial direction of the turbine system. 14. A system as in claim 11, wherein the mounting structure is configured to be attached to the first guide rail using a bolt-type fastener. 15. A system as in claim 11, wherein the guide structure further comprises a second guide rail extending parallel to the first guide rail between the first end and second end of the guide structure, and wherein the mounting structure comprises mounting plates positioned on opposing sides of the guide rails, the mounting plates being connected together with a bolt. 16. A method for measuring the change in position of two or more variable guide vanes in a turbine system, comprising: determining a change in position of a first variable guide vane using an electronic indicator, the electronic, indicator being moveable along a guide structure mounted within a casing of the turbine system adjacent to an end of a variable guide vane along an axial direction of the turbine system; andmoving the electronic indicator along the guide structure. 17. A method as in claim 16, wherein the electronic indicator is attached to a mounting structure comprising a mounting block and an indicator block, the electronic indicator being attached to the indicator block and the indicator block being moveable relative to the mounting block, the method further comprising: moving the indicator block relative to the mounting block towards the first variable guide vane to allow the electronic indicator to be used to determine the change in position of the first variable guide vane; andmoving the indicator block relative to the mounting block away from the first variable guide vane after the change in position of the first variable guide vane has been determined. 18. A method as in claim 16, wherein moving the electronic indicator along the guide structure comprises: moving the electronic indicator along the guide structure from a location adjacent to the first variable guide vane to a location adjacent to a second variable guide vane. 19. A method as in claim 18, further comprising: determining a change in position of the second variable guide vane using the electronic indicator. 20. A method as in claim 18, wherein the guide structure comprises a first end, a second end, and a guide rail extending between the first and second ends, the electronic indicator being configured to slide along the guide rail between the location adjacent to the first variable guide vane and the location adjacent to the second variable guide vane.