发明名称 Method for microplasma spray coating a portion of a turbine vane in a gas turbine engine
摘要 <p>An apparatus for microplasma spray coating a portion of a turbine vane (72) without masking includes a microplasma gun (12) with an anode (16), cathode (18), and an arc generator for generating an electric arc between the anode (16) and cathode (18). An arc gas emitter injects gas through the electric arc. The electric arc is operable for ionizing the gas to create a plasma gas stream (21). A powder injector (22) injects powdered material into a plasma stream (21). A localized area of the turbine vane (72) is coated with the powdered material (34) without having to mask the turbine vane (72).</p>
申请公布号 EP1652951(B1) 申请公布日期 2009.10.28
申请号 EP20050256727 申请日期 2005.10.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ZAJCHOWSKI, PAUL H.;SHUBERT, GARY C.;BLANKENSHIP, DONN R.;MEMMEN, ROBERT L.
分类号 C23C4/12;B23P15/02;B23P15/04;F01D5/00;F01D5/28;H05H1/42 主分类号 C23C4/12
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