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1.发明公开FLOW INLET FOR SUPERSONIC AIRCRAFT WITH ELLIPTICAL COMPRESSION RAMP 审中-公开STRÖMUNGSEINLASSFÜRÜBERSCHALLFLUGZEUGMIT ELLIPTISCHER KOMPRESSIONSRAMPE
公开(公告)号：EP3059169A1
公开(公告)日：2016-08-24
申请号：EP16154793.0
申请日：2016-02-09
Applicant: The Boeing Company
Inventor： ADAMSON, Eric E , FUGAL, Spencer Robert
CPC classification number: B64D33/02 , B64D2033/026 , F02C7/04 , F05D2220/80 , F05D2250/14 , Y02T50/672
Abstract: An apparatus is formed of a cowl and a flow inlet formed on an interior surface of the cowl. The flow inlet has a supersonic compression section attached to a subsonic diffusion section at a throat. The supersonic compression section includes an at least partially elliptical compression ramp which extends along an approximately 180 degree arc along the interior surface. The flow inlet may form part of an aircraft. A method of air flow using the flow inlet is also disclosed.
Abstract translation: 装置由整流罩和形成在整流罩的内表面上的流动入口形成。 流入口具有连接到喉部处的亚音速扩散部分的超音速压缩部分。 超音速压缩部分包括至少部分椭圆形的压缩斜坡，其沿着内表面沿大约180度的弧延伸。 流入口可以形成飞机的一部分。 还公开了使用流入口的空气流动的方法。
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公开(公告)号：EP3059169B1
公开(公告)日：2018-11-21
申请号：EP16154793.0
申请日：2016-02-09
Applicant: The Boeing Company
Inventor： ADAMSON, Eric E , FUGAL, Spencer Robert
CPC classification number: B64D33/02 , B64D2033/026 , F02C7/04 , F05D2220/80 , F05D2250/14 , Y02T50/672
Abstract: An apparatus is formed of a cowl and a flow inlet formed on an interior surface of the cowl. The flow inlet has a supersonic compression section attached to a subsonic diffusion section at a throat. The supersonic compression section includes an at least partially elliptical compression ramp which extends along an approximately 180 degree arc along the interior surface. The flow inlet may form part of an aircraft. A method of air flow using the flow inlet is also disclosed.
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