Systems and methods for mitigating curved rotors in gas turbine engines

A system and method for mitigating a curved rotor in a gas turbine engine is provided. A turbomachine for a vehicle is provided. The turbine includes a first rotatable member; a first power source operably coupled with the first rotatable member; a second power source selectively coupled with the first rotatable member; and a controller having one or more processors and one or more storage devices, the one or more storage devices storing instructions that, when executed by the one or more processors, cause the one or more processors to perform operations and, when performing the operations, cause the one or more processors to perform operations. The one or more processors are configured to: receive an input indicative of an engine shutdown of the turbine; and responsive to engine shutdown, causing a second power source to power and rotate the first rotatable component. 提供了一种用于减轻燃气涡轮发动机中弯曲转子的系统和方法。具体地，提供了一种用于运载工具的涡轮机。涡轮机包括第一可旋转部件；第一功率源，该第一功率源与第一可旋转部件可操作地联接；第二功率源，该第二功率源选择性地与第一可旋转部件联接；以及控制器，该控制器具有一个或多个处理器和一个或多个存