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Turbine Compressor Rotor Spacers
This inspection fixture checks gas turbine engine compressor rotor spacers for radial size and runout at five stages.
It represents a specific Starrett special gage capability – the designing and building of large, ultra-precise fixture gages mounted on Starrett precision granite surface plates which meet or exceed U.S. Federal Specification GGG-P-463C. |  |
Right: Rotor turned 360° on
its axis to determine runout
and radial deviation.
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