发明名称 FAST ACTING AIRCRAFT ENGINE BLEED AIR CHECK VALVE
摘要 An engine air supply system includes an air source, which is a gas turbine engine in one example. A component, such as an environmental control system component, is interconnected to the air source by a conduit that includes a supply flow direction. A check valve is arranged in the conduit. The check valve includes a valve portion moveable in the supply flow direction from a closed position to an open position. The closed position is arranged at an acute angle relative to the supply flow direction. The check valve includes first and second valve portions that are hemi-elliptical in shape. The first and second valve portions are non-planar and arranged approximately 90 degrees apart when in the closed position. The first and second valve portions move toward one another from the closed position to the open position. Each of the first and second valve portions moves approximately 30-40 degrees from the open position to the closed position in response to a stall condition, which significantly reduces the response time and forces generated by the first and second valve portions when closing.
申请公布号 US2009320495(A1) 申请公布日期 2009.12.31
申请号 US20070741001 申请日期 2007.04.27
申请人 ELDER JAMES;ADAMS JOSHUA 发明人 ELDER JAMES;ADAMS JOSHUA
分类号 F02C6/04;F16K15/00 主分类号 F02C6/04
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