Invention Application
- Patent Title: FILTERS FOR AIRCRAFT ENGINE INLETS
- Patent Title (中): 飞机引擎入口滤清器
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Application No.: US14292248Application Date: 2014-05-30
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Publication No.: US20150344141A1Publication Date: 2015-12-03
- Inventor: Albert G. Brand
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: US TX Fort Worth
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: US TX Fort Worth
- Main IPC: B64D33/02
- IPC: B64D33/02 ; F02C7/055

Abstract:
Some examples of an aircraft engine barrier filtration system include an engine barrier filter layer positioned near an aircraft engine intake. The filter layer filters aircraft engine intake air. The system includes a check valve assembly positioned adjacent to the engine barrier filter layer. The check valve assembly permits the engine intake air to flow into the engine through the filter layer during a first aircraft operation mode and to prevent air flow away from the engine through the filter layer during a second aircraft operation mode that is different from the first aircraft operation mode.
Public/Granted literature
- US09517842B2 Filters for aircraft engine inlets Public/Granted day:2016-12-13
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