Patent ID: 9388709
Filing Date: 2016-07-12
CPC Classification: F01D,F05D

Claim Text:
1. A gas turbine rotor and exhaust assembly maintenance system, said system comprising: a maintenance skid configured to support the gas turbine rotor and exhaust assembly after it has been removed from a gas turbine, said maintenance skid including an exhaust portion configured to support an exhaust of the gas turbine rotor and exhaust assembly and a rotor portion configured to support a rotor of the gas turbine rotor and exhaust assembly, said exhaust portion including opposing tracks and said rotor portion including a rotor portion platform; a pair of exhaust stands where each exhaust stand is slidably mounted to one of the tracks so as to allow the exhaust to be slidably removed from the rotor and reassembled thereto; and at least two rotor stands secured to the rotor portion platform and being configured to support the rotor, said rotor stands including rollers that are configured to allow the rotor that is seated on the rotor portion to be turned.