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公开(公告)号:EP3658290B1
公开(公告)日:2023-06-07
申请号:EP18750113.5
申请日:2018-07-20
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公开(公告)号:EP3507002B1
公开(公告)日:2021-05-12
申请号:EP17847665.1
申请日:2017-09-01
发明人: HALE, Brian, R. , VOGEL, Jeremy
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公开(公告)号:EP3698886A1
公开(公告)日:2020-08-26
申请号:EP20159003.1
申请日:2020-02-24
申请人: Stratec SE
发明人: Hinderer, Fabian , Polushkin, Igor
摘要: The present invention relates to a method for monitoring a dispensed fluid jet. The invention provides an oscillation nozzle, comprising a main channel and at least one secondary channel surrounding the main channel, wherein the nozzle has an inlet and an outlet for an air flow defining a flow axis running centrally through the main channel, characterized in that the secondary channel comprises a drill hole.
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公开(公告)号:EP3628591A1
公开(公告)日:2020-04-01
申请号:EP19198594.4
申请日:2019-09-20
发明人: Stefes, Bruno , Bauer, Matthias , Lohse, Jakob
摘要: Disclosed is a flow guide body (19) for an aircraft (1), comprising a main body (29) having an outer aerodynamic surface (33) provided with a plurality of outlet openings (21), and a plurality of flow control devices (31), each flow control device (31) comprising an inlet (35), an interaction chamber (37), a first outlet (39) and a second outlet (41), wherein a first control inlet (53) is connected to the interaction chamber (37) at the first side (49) of the chamber axis (47), wherein the first and second outlets (39, 41) are each connected to outlet openings (21) in the aerodynamic surface (33), wherein the first outlet (39) is provided with a first control outlet (55) and the second outlet (41) is provided with a second control outlet (57), wherein at least one second flow control device (31b) is arranged such that the first or second outlet (39, 41) is connected with the inlet (35) of the first flow control device (31a), wherein one of the first and second control outlets (55, 57) of the first flow control device (31a) is connected to the first control inlet (53) of the first flow control device (31a), and wherein the other of the first and second control outlets (55, 57) of the first flow control device (31a) is connected to the first control inlet (53, 59) of the second flow control device (31b).
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公开(公告)号:EP2722275B1
公开(公告)日:2019-07-24
申请号:EP13188983.4
申请日:2013-10-16
申请人: The Boeing Company
发明人: Raghu, Surya
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公开(公告)号:EP2708426B1
公开(公告)日:2019-06-26
申请号:EP12800401.7
申请日:2012-05-23
申请人: Mitsuba Corporation
发明人: NISHIO, Kentarou
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公开(公告)号:EP2240399B1
公开(公告)日:2019-05-29
申请号:EP09709574.9
申请日:2009-02-11
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