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    AIRFOIL HAVING INTERNAL LATTICE NETWORK
    1.
    发明申请
    AIRFOIL HAVING INTERNAL LATTICE NETWORK 审中-公开
    具有内部网络的航空

    公开(公告)号：WO2014011290A2

    公开(公告)日：2014-01-16

    申请号：PCT/US2013/036511

    申请日：2013-04-14

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： FISK, Benjamin T. ,  PROPHETER-HINCKLEY, Tracy A. ,  TRACY, Anita L. ,  LOUREIRO, Sergio M. ,  KLUCHA, Agnes

    CPC classification number: F04D29/388 ,  F01D5/16 ,  F02C3/04 ,  F02K3/06 ,  F04D29/325 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2240/30

    Abstract: An airfoil includes an airfoil body that defines a longitudinal axis. The airfoil body includes a leading edge and a trailing edge and a first side wall and a second side wall that is spaced apart from the first side wall. The first side wall and the second side wall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A lattice network connects the first side and the second side. The lattice network includes at least one enlarged node spaced apart from the first side wall and the second side wall and ribs that extend from the at least one enlarged node. Each of the ribs connects to one of the first side wall and the second side wall.

    Abstract translation: 翼型件包括限定纵向轴线的翼型件。 机翼本体包括前缘和后缘以及与第一侧壁间隔开的第一侧壁和第二侧壁。 第一侧壁和第二侧壁连接前缘和后缘，并且在翼型体中至少部分地限定空腔。 网格网络连接第一侧和第二侧。 网格网络包括与第一侧壁和第二侧壁间隔开的至少一个扩大节点和从至少一个放大节点延伸的肋。 每个肋连接到第一侧壁和第二侧壁中的一个。

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