发明名称 Fastback turbulator structure and turbine nozzle incorporating same
摘要 <p>Heat transfer apparatus comprises a wall 66 exposed to a fluid flow F and a plurality of turbulators 100 disposed on the wall, each turbulator having an upright front face 102 which generally faces the direction of flow, and a back face 104 which defines a ramp which tapers from the front face to the wall. The heat transfer apparatus may comprise part of a turbine nozzle which also comprises a hollow vane and an arcuate band disposed at an end of the vane and having a flow path face adjacent the vane and an opposed back face. The back face includes at least one open pocket defined in part by the wall which is recessed from the back face, opposed ends of the wall merging with the back face, and wherein the pocket is exposed to a fluid flow.</p>
申请公布号 GB2473949(B) 申请公布日期 2016.01.20
申请号 GB20100015936 申请日期 2010.09.23
申请人 GENERAL ELECTRIC COMPANY 发明人 ROBERT DAVID BRIGGS;SHAWN MICHAEL PEARSON;JOHN CREIGHTON SCHILLING
分类号 F01D9/04;F01D25/12 主分类号 F01D9/04
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