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公开(公告)号:EP2478424A1
公开(公告)日:2012-07-25
申请号:EP10754780.4
申请日:2010-08-25
IPC分类号: G05D7/01
CPC分类号: G05D7/0133 , G05D7/03 , Y10T137/7784 , Y10T137/7808 , Y10T137/85986 , Y10T137/8671
摘要: The present invention relates generally to flow regulation in aircraft systems. More particularly, the present invention relates to a flow regulator 100 and a high-lift system 200 for an aircraft incorporating such a flow regulator 100. The flow regulator 100 comprises a fluid input port 102 for receiving a pressurized fluid, a fluid output port 104 for providing fluid having a regulated flow rate, and a regulator valve 106 connected in fluid communication between the fluid input port 102 and the fluid output port 104. The regulator valve 106 is operable to provide regulated fluid at a substantially constant output flow rate to the fluid output port 104. The flow regulator 100 also includes a flow switching mechanism 108 for switching the substantially constant output flow of the flow regulated fluid provided by the regulator valve 106 between a first flow rate and a second flow rate, the first flow rate being less than the second flow rate.
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公开(公告)号:EP2126390B1
公开(公告)日:2012-03-28
申请号:EP08702070.7
申请日:2008-02-06
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公开(公告)号:EP3996996A1
公开(公告)日:2022-05-18
申请号:EP20736974.5
申请日:2020-07-02
发明人: THOMAS, Glynn
IPC分类号: B64D45/00
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公开(公告)号:EP2555979A2
公开(公告)日:2013-02-13
申请号:EP11713025.2
申请日:2011-03-23
发明人: THOMAS, Glynn
IPC分类号: B64D45/00
CPC分类号: B64D45/0005 , B64C13/28 , B64D2045/001
摘要: A control surface element skew and/or loss detection system (100) is provided which combines a cable (168, 178) system linked to movement transducers (120) via mechanical links (114, 116) connecting the fixed wing structure (102) to the control surface elements (106, 112).
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公开(公告)号:EP4377206A1
公开(公告)日:2024-06-05
申请号:EP22777244.9
申请日:2022-09-20
CPC分类号: B64D45/0005 , B64D2045/00120130101 , G01M13/023
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公开(公告)号:EP2478424B1
公开(公告)日:2018-06-13
申请号:EP10754780.4
申请日:2010-08-25
CPC分类号: G05D7/0133 , G05D7/03 , Y10T137/7784 , Y10T137/7808 , Y10T137/85986 , Y10T137/8671
摘要: The present invention relates generally to flow regulation in aircraft systems. More particularly, the present invention relates to a flow regulator 100 and a high-lift system 200 for an aircraft incorporating such a flow regulator 100. The flow regulator 100 comprises a fluid input port 102 for receiving a pressurized fluid, a fluid output port 104 for providing fluid having a regulated flow rate, and a regulator valve 106 connected in fluid communication between the fluid input port 102 and the fluid output port 104. The regulator valve 106 is operable to provide regulated fluid at a substantially constant output flow rate to the fluid output port 104. The flow regulator 100 also includes a flow switching mechanism 108 for switching the substantially constant output flow of the flow regulated fluid provided by the regulator valve 106 between a first flow rate and a second flow rate, the first flow rate being less than the second flow rate.
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