发明授权
US07708520B2 Gas turbine engine with concave pocket with knife edge seal 有权
带凹口的燃气轮机,带刀口密封

Gas turbine engine with concave pocket with 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 concave pocket defined between a radially inner surface and a spaced radially outer surface. The concave pockets and their associated knife edge seals create a pair of vortices which prevent leakage into radially inner portions of the turbine section.
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