发明名称 RETROFITTABLE INTERSTAGE ANGLED SEAL
摘要 PROBLEM TO BE SOLVED: To accommodate the differential axial and radial movement of a rotor/bucket assembly and adjacent stationary stator components.SOLUTION: A rotary turbomachine includes a rotor mounting at least one disk having an outer surface and at least one bucket extending radially from the outer surface. A stationary stator component is located adjacent to the disk, and a seal plate extends from a portion of the stationary stator component. An angel wing seal extends from the bucket, thereby defining a clearance between the seal plate and the angel wing seal. An abradable seal element is disposed on the seal plate, and the abradable seal element and the seal plate are angled at an acute angle relative to a center axis of the rotor extending radially outwardly in a direction toward the angel wing seal.
申请公布号 JP2013151936(A) 申请公布日期 2013.08.08
申请号 JP20130008855 申请日期 2013.01.22
申请人 GENERAL ELECTRIC CO <GE> 发明人 ADAICKALASAMY JAMES
分类号 F01D11/02;F02C7/28;F16J15/44;F16J15/447;F16J15/453 主分类号 F01D11/02
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