发明名称 Spaltform bei einem Leitschaufelsegment
摘要 <p>A vane cluster for a turbine engine compressor or turbine includes a shroud 12 with a nonlinear slot 26 extending therethrough to divide the shroud into thermally independent shroud segments 24 . The slot is bordered by matching nonlinear surfaces 28 that are easy and inexpensive to produce with conventional wire EDM equipment. The nonlinear profile of the slots effectively resists fluid leakage.</p>
申请公布号 DE60313716(D1) 申请公布日期 2007.06.21
申请号 DE2003613716 申请日期 2003.10.02
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 JOSLIN, FREDERICK R.
分类号 B23H7/02;F01D9/04;B23H9/10;F01D5/22;F01D9/02;F01D11/00;F02C7/00 主分类号 B23H7/02
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