发明申请
US20090067997A1 Gas turbine engine with canted pocket and canted knife edge seal 有权
燃气涡轮发动机带斜口袋和斜口刀边缘密封

Gas turbine engine with canted pocket and canted knife edge seal
摘要:
A gas turbine engine is provided with turbine sealing structures including knife edge seals which extend at an angle relative to an axial center line of the engine. Each knife edge seal is associated with a control pocket defined between a radially inner surface and a spaced radially outer surface. The control pockets and their associated knife edge seals create a difficult flow path to prevent leakage into radially inner portions of the turbine section.
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