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公开(公告)号：EP2584323B1
公开(公告)日：2013-12-04
申请号：EP11400048.2
申请日：2011-10-20
CPC分类号： G01F23/18 , B64C27/006 , B64C27/32 , B64C27/82 , G01F23/14
摘要： The invention relates to a monitoring device (1, 30) for lubricant quantities, particularly a monitoring device (1, 30) for lubricant quantities in a rotor head (2) of a helicopter (50) and more particularly a monitoring device (1, 30) for lubricant quantities in a rotor head (2) of a tail rotor (3) of a helicopter (50), comprising a casing (5) to preserve the lubricant quantities for monitoring, a shaft (6) mounted inside said casing to rotationally drive the casing (5), at least one bearing (11-14), said at least one bearing (11-14) being mounted from outside to the casing (5) and/or shaft (6) and said at least one bearing (11-14) being connected to the casing (5) for supply of lubricant, sensor means (19-22, 31-34) to detect the lubricant quantities inside said casing (5), and, interface means for communication of data from said sensor means (19-22, 31-34) to at least one display (54).
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2.发明公开Device and method for monitoring of particles in a lubricating circuit or a hydraulic system 审中-公开在润滑电路或液压系统的方法和用于监测粒子设备
公开(公告)号：EP2574905A1
公开(公告)日：2013-04-03
申请号：EP11400045.8
申请日：2011-09-29
发明人： Lees, Thilo , Vogel, Dominik , Regenfelder, Florian , Schida, Silvio , Fuchs, Christian , Gerstenhoefer, Manfred
CPC分类号： G01N15/0625 , G01N15/0205 , G01N15/0656 , G01N21/67 , G01N33/2888
摘要： The invention is related to a device and a method for monitoring particles contaminating a lubricating circuit or a hydraulic system, particularly a lubricating circuit or a hydraulic system of an aircraft, such as a helicopter. Measuring means (12, 14, 15, 16) for sizes and quantities of particle (2) in a liquid medium of the lubricating circuit or of the hydraulic system comprise a luminous source (12) directing light into the liquid medium through optical windows (7, 8), at least one photo cell (15, 16) and at least one retaining means (9) for said particles (2).
摘要翻译： 本发明涉及一种装置和用于监控污染的润滑电路或液压系统，特别是润滑回路或飞机的液压系统的粒子，作为搜索直升机的方法。 测量对尺寸和颗粒的量（2）在润滑回路的或液压系统的液体介质包括一个发光源（12）将光引导到通过光学窗口的液体介质的装置（12，14，15，16）（ 7，8），至少一个光电池（15,16）和至少一个保持装置（9）用于所述颗粒（2）。
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公开(公告)号：EP2584323A1
公开(公告)日：2013-04-24
申请号：EP11400048.2
申请日：2011-10-20
CPC分类号： G01F23/18 , B64C27/006 , B64C27/32 , B64C27/82 , G01F23/14
摘要： The invention relates to a monitoring device (1, 30) for lubricant quantities, particularly a monitoring device (1, 30) for lubricant quantities in a rotor head (2) of a helicopter (50) and more particularly a monitoring device (1, 30) for lubricant quantities in a rotor head (2) of a tail rotor (3) of a helicopter (50), comprising a casing (5) to preserve the lubricant quantities for monitoring, a shaft (6) mounted inside said casing to rotationally drive the casing (5), at least one bearing (11-14), said at least one bearing (11-14) being mounted from outside to the casing (5) and/or shaft (6) and said at least one bearing (11-14) being connected to the casing (5) for supply of lubricant, sensor means (19-22, 31-34) to detect the lubricant quantities inside said casing (5), and, interface means for communication of data from said sensor means (19-22, 31-34) to at least one display (54).
摘要翻译： 本发明涉及用于润滑剂量的监测装置（1,30），特别是用于直升机（50）的转子头（2）中的润滑剂量的监测装置（1,30），并且更具体地涉及监测装置（1,30） 30），用于直升机（50）的尾旋翼（3）的转子头（2）中的润滑剂量，所述直升机（50）包括用于保存润滑剂量以用于监测的壳体（5），安装在所述壳体内的轴（6） （5）旋转地驱动所述壳体（5），至少一个轴承（11-14），所述至少一个轴承（11-14）从外部安装到所述壳体（5）和/或轴（6），并且所述至少一个 轴承（11-14）连接到用于供应润滑剂的壳体（5），用于检测所述壳体（5）内的润滑剂量的传感器装置（19-22,31-34）以及用于数据通信的接口装置 从所述传感器装置（19-22,31-34）传送到至少一个显示器（54）。
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公开(公告)号：EP2572982A1
公开(公告)日：2013-03-27
申请号：EP11400044.1
申请日：2011-09-20
IPC分类号： B64C27/00
CPC分类号： B64C27/006 , B63B1/248 , B63H1/28 , B63H2001/286 , B64C3/141 , B64D2045/0085
摘要： The invention is related to a profile (1,10,20), particularly to a profile for an airfoil of an aircraft and more particularly to a profile for a rotor blade of a helicopter, with a circulation control system (13) having at least one passageway (4,15) for a pressure responsive medium inside said profile, wherein said circulation control system includes means (5) sensing medium pressure in said at least one medium passageway inside each profile, means (6) comparing the sensed medium pressure and signal means in response to the comparing means. The inventive profile allows monitoring of damages to the profile.
摘要翻译： 本发明涉及一种轮廓（1,10,20），特别涉及一种用于飞行器的翼型的轮廓，更具体地涉及用于直升机的转子叶片的轮廓，其中循环控制系统（13）至少具有 用于所述轮廓内的压力响应介质的一个通道（4,15），其中所述循环控制系统包括用于感测每个轮廓内的所述至少一个介质通道中的介质压力的装置（5），将所感测的介质压力和 信号装置响应于比较装置。 本发明的简档允许监视轮廓的损坏。
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