发明名称 Structural stator airfoil
摘要 An airfoil comprises a leading edge, a trailing edge, and pressure and suction surfaces defined therebetween. An inner platform is coupled to a root section of the airfoil, with a curvilinear gusset extending along a lower surface of the inner platform, opposite the root section. An outer platform is coupled to a tip section of the airfoil, with a multi-lobed gusset extending along an upper surface of the inner platform, opposite the tip section.
申请公布号 US8998575(B2) 申请公布日期 2015.04.07
申请号 US201113295724 申请日期 2011.11.14
申请人 United Technologies Corporation 发明人 Lucashu John P.;Reinhardt Gregory E.;Ditomasso John C.
分类号 F03D11/00;F01D9/04 主分类号 F03D11/00
代理机构 Kinney & Lange, P.A. 代理人 Kinney & Lange, P.A.
主权项 1. An airfoil comprising: a leading edge, a trailing edge, and pressure and suction surfaces defined therebetween; an inner platform coupled to a root section of the airfoil, the inner platform comprising a curvilinear gusset extending along a lower surface of the inner platform, opposite the root section, wherein the curvilinear gusset extends along a camber line of the airfoil defined in the root section of the airfoil opposite the curvilinear gusset; an outer platform coupled to a tip section of the airfoil, the outer platform comprising a multi-lobed gusset extending along an upper surface of the outer platform, opposite the tip section; wherein the multi-lobed gusset comprises four legs meeting at a nexus, wherein two of the four legs extend axially forward from the nexus and two of the four legs extend axially aft from the nexus.
地址 Hartford CT US