发明名称 GAS TURBINE ENGINE AIRFOIL TRAILING EDGE PASSAGE AND CORE FOR MAKING SAME
摘要 An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.
申请公布号 US2015118064(A1) 申请公布日期 2015.04.30
申请号 US201314390496 申请日期 2013.03.12
申请人 United Technologies Corporation 发明人 Levine Jeffrey R.;Beattie Jeffrey S.;Staddon Malcolm C.
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
主权项 1. An airfoil comprising: a body including leading and trailing edges adjoining pressure and suction sides to provide an exterior airfoil surface, a cooling passage extending in a radial direction from a root to a tip, and a trailing edge cooling passage interconnecting the cooling passage to the trailing edge, the trailing edge cooling passage including first and second pedestals of different sizes and arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.
地址 Hartford CT US