Invention Grant
US08408491B2 Nacelle assembly having inlet airfoil for a gas turbine engine
有权
具有用于燃气涡轮发动机的入口翼型的机舱组件
- Patent Title: Nacelle assembly having inlet airfoil for a gas turbine engine
- Patent Title (中): 具有用于燃气涡轮发动机的入口翼型的机舱组件
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Application No.: US11739216Application Date: 2007-04-24
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Publication No.: US08408491B2Publication Date: 2013-04-02
- Inventor: Ashok K. Jain , Michael Winter
- Applicant: Ashok K. Jain , Michael Winter
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds PC
- Main IPC: B64D33/02
- IPC: B64D33/02
Abstract:
A nacelle assembly includes an inlet lip section and an airfoil adjacent to the inlet lip section. The airfoil is selectively moveable between a first position and a second position to adjust the flow of oncoming airflow and to influence an effective boundary layer thickness of the nacelle assembly.
Public/Granted literature
- US20080267762A1 NACELLE ASSEMBLY HAVING INLET AIRFOIL FOR A GAS TURBINE ENGINE Public/Granted day:2008-10-30
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