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1.发明公开OPTIMIZED NACELLE PROFILE AND PLENUM SHAPE FOR BOUNDARY LAYER INGESTION ACTIVE LAMINAR FLOW CONTROL 审中-公开优胜者GONDELPROFIL UND OPTIMIERTE KAMMERFORMFÜRGRENZSCHICHTAUFNAHMEAKTIVE LAMINARESTRÖMUNGSSTEUERUNG
公开(公告)号：EP3090941A1
公开(公告)日：2016-11-09
申请号：EP16166460.2
申请日：2016-04-21
申请人： Rohr, Inc.
发明人： KHIDEKEL, Ann E.
CPC分类号： B64C7/02 , B64C21/06 , B64C2230/06 , B64C2230/08 , B64C2230/20 , B64C2230/22 , B64D27/16 , B64D29/02 , B64D2033/0226 , Y02T50/166
摘要： Aspects of the disclosure are directed to a nacelle of an aircraft, comprising a surface that is profiled such that during cruise flight operation lines of constant static pressure of a boundary layer around the nacelle (322; 422; 522) in a given region are substantially contained within a plane that is normal to an engine axis.
摘要翻译： 本公开的方面涉及飞机的机舱，其包括被轮廓化的表面，使得在巡航飞行操作期间，给定区域中的机舱（322; 422; 522）周围的边界层的恒定静态压力线基本上是 包含在与发动机轴线垂直的平面内。
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2.发明公开
公开(公告)号：EP3552958A1
公开(公告)日：2019-10-16
申请号：EP19177540.2
申请日：2016-04-21
申请人： Rohr, Inc.
发明人： KHIDEKEL, Ann E.
摘要： Aspects of the disclosure are directed to a nacelle of an aircraft, comprising a surface that is profiled such that during cruise flight operation lines of constant static pressure of a boundary layer around the nacelle (422; 522) in a given region are substantially contained within a plane that is normal to an engine axis.
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3.发明授权
公开(公告)号：EP3090941B1
公开(公告)日：2019-07-17
申请号：EP16166460.2
申请日：2016-04-21
申请人： Rohr, Inc.
发明人： KHIDEKEL, Ann E.
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