A gas turbine engine maintenance stand (200) for a gas turbine engine (100) that comprises modules including an engine core module (140) that houses a high pressure compressor (108) and a turbine module (150) that houses a low pressure turbine (116). The gas turbine engine maintenance stand has a pair of base beams (205), each base beam having a first end (210), a midsection (215) and a second end (220). The stand has an engine core module support (225) that straddles the pair of base beams at their midsection, the engine core module support having engine core module support arms (230) that are configured to engage opposing sides of the engine core module (140) of the gas turbine engine. The stand also has a turbine module support (240) that straddles the pair of beams adjacent their second ends, the turbine module support having turbine module support arms (245) that are configured to engage opposing sides of the turbine module (150) of the gas turbine engine. The gas turbine engine maintenance stand (200) is useful for disassembling and reassembling modules of a gas turbine engine (100) in order to maintain the gas turbine engine for safety and performance purposes.
GAS TURBINE ENGINE MAINTENANCE STAND AND CORRESPONDING METHOD OF MAINTAINING A GAS TURBINE ENGINE
GASTURBINENMOTORWARTUNGSSTAND UND ZUGEHÖRIGES VERFAHREN ZUM WARTEN EINES GASTURBINENMOTORS
SUPPORT DE MAINTENANCE D'UN MOTEUR À TURBINE À GAZ ET PROCÉDÉ DE MAINTENANCE ACSSOCIÉ D'UN MOTEUR À TURBINE À GAZ
2022-05-04
Patent
Electronic Resource
English
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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