Invention Grant
- Patent Title: Variable geometry nacelle assembly for a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机的可变几何机舱组件
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Application No.: US11749260Application Date: 2007-05-16
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Publication No.: US08205430B2Publication Date: 2012-06-26
- Inventor: Ashok K. Jain
- Applicant: Ashok K. Jain
- 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: F02K3/02
- IPC: F02K3/02
Abstract:
A nacelle assembly includes an inlet lip section and a cowl section positioned downstream of the inlet lip section. At least a portion of the cowl section is moveable to influence an effective boundary layer thickness of the nacelle assembly.
Public/Granted literature
- US20080286094A1 VARIABLE GEOMETRY NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE Public/Granted day:2008-11-20
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