发明名称 OUTER DIAMETER PLATFORM COOLING HOLE SYSTEM AND ASSEMBLY
摘要 An airfoil component is described herein. The airfoil component may include an OD platform comprising a gaspath face and a non-gaspath face coupled together via a plurality of cooling holes. The airfoil component may include an airfoil extending in from the outer diameter platform. The plurality of cooling holes comprises a plurality of groups of cooling holes disposed in the outer diameter platform proximate a suction side of the airfoil and a pressure side of the airfoil.
申请公布号 US2016245093(A1) 申请公布日期 2016.08.25
申请号 US201514627915 申请日期 2015.02.20
申请人 United Technologies Corporation 发明人 Deibel Russell;Gleiner Matthew S.
分类号 F01D5/18;F02C7/18;F02C3/04 主分类号 F01D5/18
代理机构 代理人
主权项 1. An airfoil component comprising: an OD platform comprising: a non-gaspath face; anda gaspath face coupled to the non-gaspath face via a plurality of cooling holes; and an airfoil extending from the outer diameter platform, wherein the plurality of cooling holes comprise a plurality of groups of cooling holes disposed in the outer diameter platform proximate a suction side of the airfoil and a pressure side of the airfoil, wherein a plenum is formed adjacent to the non-gaspath face, wherein the plurality of cooling holes are coupled to the plenum.
地址 Hartford CT US