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公开(公告)号：US20100015830A1
公开(公告)日：2010-01-21
申请号：US11721119
申请日：2005-11-30
IPC分类号： H01R4/00
CPC分类号： H01R13/642 , F16L25/01 , F16L2201/10 , H01R13/005 , H01R24/005
摘要： The invention relates to a device for connecting an item of equipment and two cables, one of which carries electrical data and the other of which carries pneumatic data. The device comprises an electrical socket and a pneumatic socket, both mounted on an item of equipment, an electrical plug secured to a cable, the electrical plug being intended to be connected to the electrical socket, and a pneumatic plug secured to a cable, the pneumatic plug being intended to be connected to the pneumatic socket. According to the invention, when the pneumatic plug is in a connected but unlocked position, the electrical plug cannot be plugged in.
摘要翻译： 本发明涉及一种用于连接设备和两条电缆的设备，其中一条电缆承载电气数据，另一条电缆承载气动数据。 该装置包括电气插座和气动插座，两者都安装在一件设备上，固定到电缆上的电插头，该电插头旨在连接到电插座，以及一个固定到电缆的气动插头， 气动插头旨在连接到气动插座。 根据本发明，当气动塞处于连接但解锁位置时，电插头不能插入。
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公开(公告)号：US07726993B2
公开(公告)日：2010-06-01
申请号：US11721119
申请日：2005-11-30
IPC分类号： H01R13/642
CPC分类号： H01R13/642 , F16L25/01 , F16L2201/10 , H01R13/005 , H01R24/005
摘要： The invention relates to a device for connecting an item of equipment and two cables, one of which carries electrical data and the other of which carries pneumatic data. The device comprises an electrical socket and a pneumatic socket, both mounted on an item of equipment, an electrical plug secured to a cable, the electrical plug being intended to be connected to the electrical socket, and a pneumatic plug secured to a cable, the pneumatic plug being intended to be connected to the pneumatic socket. According to the invention, when the pneumatic plug is in a connected but unlocked position, the electrical plug cannot be plugged in.
摘要翻译： 本发明涉及一种用于连接设备和两条电缆的设备，其中一条电缆承载电气数据，另一条电缆承载气动数据。 该装置包括电气插座和气动插座，两者都安装在一件设备上，固定到电缆上的电插头，该电插头旨在连接到电插座，以及一个固定到电缆的气动插头， 气动插头旨在连接到气动插座。 根据本发明，当气动塞处于连接但解锁位置时，电插头不能插入。
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公开(公告)号：US07114847B2
公开(公告)日：2006-10-03
申请号：US10517426
申请日：2003-06-13
申请人： Marc Simeon
发明人： Marc Simeon
CPC分类号： G01K13/028 , G01K1/20 , G01K13/02
摘要： The invention relates to a total temperature probe for an aircraft and to a method of determining temperature by means of such a probe. The total temperature measurement probe comprises a base, an external face of which is intended to be mounted so as to be substantially coplanar with a skin of the aircraft, and a mast that projects from the base and supports an active part of the probe. The probe furthermore includes several temperature sensors placed on, the external face of the base and distributed around the mast. The method consists in determining the total temperature of the air surrounding the probe on the basis of the temperature measurement carried out in the active part (4) of the probe and on the basis of the maximum difference that exists between the measurements made by the temperature sensors.
摘要翻译： 本发明涉及一种用于飞行器的总温度探测器以及通过这种探测器确定温度的方法。 总温度测量探头包括底座，其外表面旨在被安装成与飞行器的皮肤基本上共面，以及从基座突出并支撑探针的有效部分的桅杆。 探头还包括放置在基座的外表面上并分布在桅杆周围的几个温度传感器。 该方法在于基于在探针的有效部分（4）中进行的温度测量并基于温度测量之间存在的最大差异来确定探针周围的空气的总温度 传感器。
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公开(公告)号：US07124630B2
公开(公告)日：2006-10-24
申请号：US10493567
申请日：2002-12-10
申请人： Nicolas Hanson , Marc Simeon , Jean-Jacques Barbou
发明人： Nicolas Hanson , Marc Simeon , Jean-Jacques Barbou
IPC分类号： G01P13/00
CPC分类号： G01K13/028 , B64D15/12 , B64D43/02 , G01K13/02 , G01P5/165 , G01P13/025
摘要： The invention concerns a multifunction probe for aircraft. The probe measures the total pressure and measures the total temperature of an air flow surrounding the aircraft. The total pressure is measured by a first tube, the so-called Pitot tube oriented substantially along the axis of the air flow surrounding the aircraft, the total temperature is measured by a second tube open to the air flow and oriented substantially in the axis of the air flow. The first tube is situated inside the second tube. The invention also concerns a process for shaping a heating wire forming means of deicing of the multifunction probe. The process includes: winding the heating wire helically around a first mandrel, inserting the first mandrel into a second hollow mandrel, continuing the winding of the heating wire around the second mandrel, and placing the heating wire, thus formed, inside the two tubes and being fixed therein.
摘要翻译： 本发明涉及一种用于飞行器的多功能探头。 探头测量总压力并测量飞机周围空气流的总温度。 总压力通过第一管测量，所谓的皮托管基本上沿着围绕飞行器的空气流的轴线取向，总温度由对气流开放的第二管测量，并且基本上在 气流。 第一管位于第二管内。 本发明还涉及一种用于成形多功能探针除冰加热线形成装置的方法。 该过程包括：将加热丝线螺旋缠绕在第一心轴上，将第一心轴插入第二空心心轴中，将加热线的绕组连续围绕第二心轴，并将由此形成的加热线放置在两个管内， 被固定在其中。
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公开(公告)号：US20050190816A1
公开(公告)日：2005-09-01
申请号：US10517426
申请日：2003-06-13
申请人： Marc Simeon
发明人： Marc Simeon
CPC分类号： G01K13/028 , G01K1/20 , G01K13/02
摘要： The invention relates to a total temperature probe for an aircraft and to a method of determining temperature by means of such a probe. The total temperature measurement probe comprises a base, an external face of which is intended to be mounted so as to be substantially coplanar with a skin of the aircraft, and a mast that projects from the base and supports an active part of the probe. The probe furthermore includes several temperature sensors placed on, the external face of the base and distributed around the mast. The method consists in determining the total temperature of the air surrounding the probe on the basis of the temperature measurement carried out in the active part (4) of the probe and on the basis of the maximum difference that exists between the measurements made by the temperature sensors.
摘要翻译： 本发明涉及一种用于飞行器的总温度探测器以及通过这种探测器确定温度的方法。 总温度测量探头包括底座，其外表面旨在被安装成与飞行器的皮肤基本上共面，以及从基座突出并支撑探针的有效部分的桅杆。 探头还包括放置在基座的外表面上并分布在桅杆周围的几个温度传感器。 该方法在于基于在探针的有效部分（4）中进行的温度测量并基于温度测量之间存在的最大差异来确定探针周围的空气的总温度 传感器。
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