Invention Grant
- Patent Title: Engine inlet configuration
- Patent Title (中): 发动机进气口配置
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Application No.: US14252236Application Date: 2014-04-14
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Publication No.: US09586692B2Publication Date: 2017-03-07
- Inventor: Steven Bofill , Scott A. Chasen , Joseph Lawrence Simonetti , Donald William Lamb, Jr.
- Applicant: Sikorsky Aircraft Corporation
- Applicant Address: US CT Stratford
- Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee Address: US CT Stratford
- Agency: Cantor Colburn LLP
- Main IPC: B64D33/02
- IPC: B64D33/02
Abstract:
An engine inlet assembly includes an inlet duct having a first inlet duct leg and a second inlet duct leg, the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet located at an engine inlet. The first inlet duct leg and the second inlet duct leg are fixedly secured to an airframe of an aircraft at an air inlet. The duct outlet has a floating interface with the engine inlet.
Public/Granted literature
- US20150291288A1 ENGINE INLET CONFIGURATION Public/Granted day:2015-10-15
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