Invention Application
US20120048995A1 Method For Enhancing The Aerodynamic Efficiency Of The Vertical Tail Of An Aircraft 有权
提高飞机垂直尾翼空气动力效率的方法

  • Patent Title: Method For Enhancing The Aerodynamic Efficiency Of The Vertical Tail Of An Aircraft
  • Patent Title (中): 提高飞机垂直尾翼空气动力效率的方法
  • Application No.: US13319381
    Application Date: 2010-05-17
  • Publication No.: US20120048995A1
    Publication Date: 2012-03-01
  • Inventor: Alain Tanguy
  • Applicant: Alain Tanguy
  • Applicant Address: FR Toulouse Cedex
  • Assignee: AIRBUS OPERATIONS (S.A.S.)
  • Current Assignee: AIRBUS OPERATIONS (S.A.S.)
  • Current Assignee Address: FR Toulouse Cedex
  • Priority: FR0902466 20090520
  • International Application: PCT/FR10/50943 WO 20100517
  • Main IPC: B64C9/00
  • IPC: B64C9/00 B64C5/06 B64F5/00
Method For Enhancing The Aerodynamic Efficiency Of The Vertical Tail Of An Aircraft
Abstract:
The invention comprises varying the ratio between the control surface local chord (I) and the vertical stabilizer local chord (L) along the height of the vertical tail (2) in order to adapt the local value of the coefficient of the side lift applied to the vertical tail (2) to a maximum acceptable value of the side lift coefficient.
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