Invention Application
- Patent Title: Compact Nacelle With Contoured Fan Nozzle
- Patent Title (中): 紧凑型机舱带轮廓风扇喷嘴
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Application No.: US14611887Application Date: 2015-02-02
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Publication No.: US20150330254A1Publication Date: 2015-11-19
- Inventor: Richard Alan Weiner , Wesley K. Lord
- Applicant: United Technologies Corporation
- Main IPC: F01D25/24
- IPC: F01D25/24 ; B64D33/04 ; F02C3/06 ; B64D29/02
Abstract:
A gas turbine engine including a fan, compressor, combustor and a turbine arranged in series and surrounded by a nacelle. An engine core cowl is disposed within the nacelle. Each of these elements shares a central longitudinal axis. The nacelle length may be non-uniform around the circumference of the nacelle.
Information query
