| 摘要 |
A method of using a gas turbine engine is provided. The method may include supporting a first portion of the gas turbine engine on one or more guide tracks extending in a first direction, the first direction being at an angle to a longitudinal axis of the gas turbine engine. The method may also include moving the first portion of the gas turbine engine in the first direction on the guide tracks independently of a second portion of the gas turbine engine.
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