发明申请
- 专利标题： Icephobic Flowpath for a Nose Cone and Method Therefor
- 专利标题（中）： 一种鼻锥的疏水流路及其方法
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申请号： US14615543申请日： 2015-02-06
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公开(公告)号： US20160229543A1公开(公告)日： 2016-08-11
- 发明人: James J. McPhail , Isaac Jon Hogate , Victor G. Filipenco
- 申请人： United Technologies Corporation
- 主分类号： B64D15/00
- IPC分类号： B64D15/00 ; F01D25/02 ; F01D5/02
摘要：
A gas turbine engine is provided having a nose cone, wherein the nose cone is symmetrically disposed about an axis. The nose cone includes a leading edge and a base. A forward section is disposed between the leading edge and the base and has a radius at any axial location defined by a first equation. A transition section is disposed between the forward section and the base and has a radius at any axial location defined by a second equation. The first equation is different than the second equation.
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