发明名称 SPLIT COATING MASK SYSTEM FOR GAS TURBINE ENGINE COMPONENT
摘要 A mask assembly for a gas turbine engine component includes a second mask that at least partially overlaps a first mask to fit a platform of a gas turbine engine component.
申请公布号 US2014242278(A1) 申请公布日期 2014.08.28
申请号 US201414188089 申请日期 2014.02.24
申请人 United Technologies Corporation 发明人 Hlavaty Kirk D.;Palmieri Bartolomeo;Toppen Harvey R.
分类号 B05C21/00;B05D1/32 主分类号 B05C21/00
代理机构 代理人
主权项 1. A mask assembly for a gas turbine engine component comprising: a first mask; and a second mask that at least partially overlaps said first mask to fit a platform of a gas turbine engine component.
地址 Hartford CT US