发明名称 Gas turbine nozzle construction
摘要 A planar top plate (32) has film cooling slots (34) therein. A rigid honeycomb structure (38) sealingly joins this top plate with bottom plate (36). Cooling air distributed by openings (50) impinges on the top plate and passes through metering openings (48) to the slots. A flat wall surface with reduced aerodynamic losses is maintained and the uniform support of the top plate avoids local distortion which would crack any heat resistant coating applied thereto.
申请公布号 US5388765(A) 申请公布日期 1995.02.14
申请号 US19900510758 申请日期 1990.04.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HILL, JAMES D.;STOGNER, CLAUDE R.;ZIMMERMAN, ANTHONY M.
分类号 F02K1/12;F02K1/82;(IPC1-7):F02K1/38 主分类号 F02K1/12
代理机构 代理人
主权项
地址