发明名称 Integral aft seal for turbine applications
摘要 An integral aft seal for sealing the interface between a gas turbine transition piece and first stage nozzle exhibits sufficient variable thickness to adjust for relative component movement. The seal comprises a contiguous material having opposing planar faces and stiffeners attached at each of the faces. The contiguous material has corrugations to provide variable thickness. The stiffeners are attached to the planar faces of the contiguous material and generally have the same planar shape as the seal. Flexibility in the thickness dimension due to the corrugations biases the stiffeners away from one another and into contact with the turbine components. The aft seal is affixed to the transition piece by an attachment structure that eliminates relative movement between the seal and the transition piece to thereby eliminate wear.
申请公布号 US6450762(B1) 申请公布日期 2002.09.17
申请号 US20010774022 申请日期 2001.01.31
申请人 GENERAL ELECTRIC COMPANY 发明人 MUNSHI JONATHAN
分类号 F01D9/02;(IPC1-7):F01D5/02 主分类号 F01D9/02
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