Invention Grant
US08127531B2 Radially translating fan nozzle nacelle 有权
径向翻译风扇喷嘴机舱

  • Patent Title: Radially translating fan nozzle nacelle
  • Patent Title (中): 径向翻译风扇喷嘴机舱
  • Application No.: US12268902
    Application Date: 2008-11-11
  • Publication No.: US08127531B2
    Publication Date: 2012-03-06
  • Inventor: Dean L. Parham
  • Applicant: Dean L. Parham
  • Applicant Address: US IL Chicago
  • Assignee: The Boeing Company
  • Current Assignee: The Boeing Company
  • Current Assignee Address: US IL Chicago
  • Main IPC: F02K3/02
  • IPC: F02K3/02
Radially translating fan nozzle nacelle
Abstract:
A variable area nozzle system for a turbofan gas turbine engine comprises a fan duct inner wall, a fan duct outer wall and a fan nozzle. The fan duct outer wall is disposed in radially-spaced relation to the fan duct inner wall. The fan nozzle defines at least a portion of the fan duct outer wall and has a nozzle aft edge defining a fan duct throat area relative to the fan duct inner wall. The fan nozzle is configured to move outwardly relative to the longitudinal axis during axial aft translation thereof in order to vary the fan duct throat area.
Public/Granted literature
Information query
Patent Agency Ranking
0/0