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Invention Application
US20160003072A1 GAS TURBINE ENGINE THIN WALL COMPOSITE VANE AIRFOIL 审中-公开
气体涡轮发动机薄壁复合材料VANE AIRFOIL

  • Patent Title: GAS TURBINE ENGINE THIN WALL COMPOSITE VANE AIRFOIL
  • Patent Title (中): 气体涡轮发动机薄壁复合材料VANE AIRFOIL
  • Application No.: US14767512
    Application Date: 2014-02-05
  • Publication No.: US20160003072A1
    Publication Date: 2016-01-07
  • Inventor: Hoyt Y. Chang , Shelton O. Duelm
  • Applicant: UNITED TECHNOLOGIES CORPORATION
  • International Application: PCT/US14/14908 WO 20140205
  • Main IPC: F01D9/04
  • IPC: F01D9/04
GAS TURBINE ENGINE THIN WALL COMPOSITE VANE AIRFOIL
Abstract:
An airfoil for a gas turbine engine has a first layer forming a cavity having transitioning from a first thickness to a second thickness through a ply drop region. A second layer is secured to the first layer.
Abstract(Chinese):

用于燃气涡轮发动机的翼型件具有形成通过层压降区域从第一厚度过渡到第二厚度的空腔的第一层。 第二层被固定到第一层。

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