Invention Grant
US08192151B2 Turbine engine having cooling gland 有权
涡轮发动机具有冷却压盖

Turbine engine having cooling gland
Abstract:
In one embodiment, a turbine may include a bearing housing for a rotor with a passage along an axis of rotation of the rotor shaft. A cooling gland configured to transfer cooling fluid to the passage may be mounted to the bearing housing with a mounting structure configured to mount the cooling gland substantially in-line with the passage of the rotor.
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