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1.发明授权公开(公告)号：US08907595B2
公开(公告)日：2014-12-09
申请号：US13320360
申请日：2010-05-19
CPC分类号： F02K1/763 , B64D29/06 , B64D33/04 , B64F5/00 , H02P5/74 , H02P9/007 , H02P2101/30 , H02P2207/01 , Y02T50/672
摘要： A nacelle for receiving an aircraft engine, the nacelle having a tubular stationary cover and at least one movable portion connected to the stationary cover via movement means for moving the movable portion between a position close to the stationary cover and a position spaced apart therefrom. The movement means have asynchronous motors, each having a stator with windings connected in parallel to a power supply circuit and a rotor having windings, each connected to a resistive load in parallel with a winding of the rotor of each of the other motors.
摘要翻译： 一种用于接收飞机发动机的机舱，所述机舱具有管状固定盖和经由移动装置连接到所述固定盖的至少一个可移动部分，用于在靠近所述固定盖的位置和与所述固定盖间隔开的位置之间移动所述可动部。 移动装置具有异步电动机，每个异步电动机具有定子，其绕组与电源电路并联连接，绕组具有绕组，每个转子与每个其它电动机的转子的绕组并联连接到电阻负载。
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2.发明申请公开(公告)号：US20120107109A1
公开(公告)日：2012-05-03
申请号：US13320360
申请日：2010-05-19
IPC分类号： F01D25/24
CPC分类号： F02K1/763 , B64D29/06 , B64D33/04 , B64F5/00 , H02P5/74 , H02P9/007 , H02P2101/30 , H02P2207/01 , Y02T50/672
摘要： A nacelle for receiving an aircraft engine, the nacelle having a tubular stationary cover and at least one movable portion connected to the stationary cover via movement means for moving the movable portion between a position close to the stationary cover and a position spaced apart therefrom. The movement means have asynchronous motors, each having a stator with windings connected in parallel to a power supply circuit and a rotor having windings, each connected to a resistive load in parallel with a winding of the rotor of each of the other motors.
摘要翻译： 一种用于接收飞机发动机的机舱，所述机舱具有管状固定盖和经由移动装置连接到所述固定盖的至少一个可移动部分，用于在靠近所述固定盖的位置和与所述固定盖间隔开的位置之间移动所述可动部。 移动装置具有异步电动机，每个异步电动机具有定子，其绕组与电源电路并联连接，绕组具有绕组，每个转子与每个其它电动机的转子的绕组并联连接到电阻负载。
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公开(公告)号：US20120187874A1
公开(公告)日：2012-07-26
申请号：US13498878
申请日：2010-10-07
申请人： Tony Fourmont , Franck Delnaud , Jérôme Piaton , Roland Casimir
发明人： Tony Fourmont , Franck Delnaud , Jérôme Piaton , Roland Casimir
IPC分类号： H02P3/00
CPC分类号： H02P3/22 , H02P25/024
摘要： A damper circuit for damping a synchronous servo-motor having at least one winding, at least one main damper resistor, connection means for connecting the main damper resistor in series with the winding, and at least one additional damper cell including at least one additional damper resistor connected in parallel with the main damper resistor via a static switch connected to a control module for controlling the switch as a function of a voltage of the winding. The control module has a shunt in parallel with the main damper resistor. The shunt has an output connected to the control input of the switch and a divider bridge connected to the shunt to form a comparator between the voltage of the winding and a conduction voltage of the shunt.
摘要翻译： 一种用于阻尼具有至少一个绕组的同步伺服电动机的阻尼器电路，至少一个主阻尼电阻器，用于将主阻尼电阻器与绕组串联连接的连接装置，以及包括至少一个附加阻尼器 电阻器通过连接到控制模块的静态开关与主阻尼电阻器并联连接，用于根据绕组的电压来控制开关。 控制模块具有与主阻尼电阻并联的并联。 分路具有连接到开关的控制输入的输出端和连接到分流器的分压器桥，以在绕组的电压和分路的导通电压之间形成比较器。
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公开(公告)号：US09035511B2
公开(公告)日：2015-05-19
申请号：US13141159
申请日：2009-11-17
申请人： Jérôme Piaton
发明人： Jérôme Piaton
CPC分类号： F16H25/2252 , F16H2025/2078 , H02K7/06 , H02K7/106
摘要： The electric motor consists of a rotor fitted with permanent magnets and comprises a stator the armature of which is made up of two parts: a stack of laminations forming round teeth and a solid tube-shaped field frame made of a material of the stainless steel kind enveloping the said stack of laminations. This armature constitutes a non-disengageable braking system that produces a damping effect in the face of possible movements of its rotor which are brought about and/or imposed by the members with which it collaborates. This motor can be used for driving a roto-linear actuator device with satellite rollers which is used as an actuator for maneuvering the control surfaces of an aircraft, for example an aileron.
摘要翻译： 电动机包括一个装有永久磁铁的转子，它包括一个定子，其电枢由两部分组成：一叠形成圆形的叠片和一个由不锈钢材料制成的实心管状场框架 包围所述堆叠的叠片。 该电枢构成不能脱离的制动系统，其面向其转子的可能的运动产生阻尼作用，这是由与其协作的构件带来和/或施加的。 该电动机可以用于驱动具有卫星辊的旋转线性致动器装置，其用作用于操纵飞机（例如副翼）的控制表面的致动器。
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5.发明授权Angular position sensor and assembly comprising a rotary system and such a sensor 有权角位置传感器和组件包括旋转系统和这种传感器公开(公告)号：US08937473B2
公开(公告)日：2015-01-20
申请号：US13504124
申请日：2010-11-05
申请人： Jérôme Piaton
发明人： Jérôme Piaton
CPC分类号： G01D5/145 , G01D5/2451
摘要： Sensor for continuously measuring the angular position of a shaft rotatably mounted relative to a housing. The sensor includes a stator, a rotor attachable to the shaft, and permanent magnets having alternating polarities located on a stator or a rotor capable of creating magnetic induction during the rotation of the rotor. A magnetic circuit channels the magnetic induction such that it is proportional to a sinusoidal function of the angle of the rotor. At least two electric transducers having linear output, each angularly offset one from the other relative to the stator, are located in the gaps arranged in the circuit. The magnetic circuit is toothed and includes at least one measuring unit having three teeth per pair of magnets, each tooth including a gap with a transducer.
摘要翻译： 用于连续测量相对于壳体可旋转地安装的轴的角位置的传感器。 传感器包括定子，可连接到轴的转子和具有位于定子或转子上的交替极性的永磁体，能够在转子旋转期间产生磁感应。 磁路使磁感应通路，使其与转子角度的正弦函数成比例。 具有线性输出的至少两个电传感器位于布置在电路中的间隙中，每个具有线性输出的电子换能器彼此相对于定子成角度地偏置。 磁路是齿形的，并且包括至少一个具有每对磁体三个齿的测量单元，每个齿包括与换能器的间隙。
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公开(公告)号：US20110234057A1
公开(公告)日：2011-09-29
申请号：US13132496
申请日：2009-12-18
申请人： Jérôme Piaton
发明人： Jérôme Piaton
IPC分类号： H02K11/00
CPC分类号： H02K29/08 , G01D5/2291
摘要： The actuator is of the roto-linear type and comprises a sleeve, a clevis and an operating rod which transmits the load. An electromagnetic sensor that measures and controls the load is placed inside the actuator, at the shoulder of the clevis. This sensor is associated with measurement means for processing the signals from the said winding, which winding are torus-shaped and arranged inside a field frame which is magnetically closed by an armature.
摘要翻译： 致动器是旋转线性的，并且包括套筒，U形夹和传送负载的操作杆。 测量和控制负载的电磁传感器位于执行机构的U形夹的肩部。 该传感器与用于处理来自所述绕组的信号的测量装置相关联，所述绕组是圆环形的，并且布置在由电枢磁闭合的场框内。
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公开(公告)号：US08729764B2
公开(公告)日：2014-05-20
申请号：US13498878
申请日：2010-10-07
申请人： Tony Fourmont , Franck Delnaud , Jérôme Piaton , Roland Casimir
发明人： Tony Fourmont , Franck Delnaud , Jérôme Piaton , Roland Casimir
IPC分类号： H02K23/22
CPC分类号： H02P3/22 , H02P25/024
摘要： A damper circuit for damping a synchronous servo-motor having at least one winding, at least one main damper resistor, connection means for connecting the main damper resistor in series with the winding, and at least one additional damper cell including at least one additional damper resistor connected in parallel with the main damper resistor via a static switch connected to a control module for controlling the switch as a function of a voltage of the winding. The control module has a shunt in parallel with the main damper resistor. The shunt has an output connected to the control input of the switch and a divider bridge connected to the shunt to form a comparator between the voltage of the winding and a conduction voltage of the shunt.
摘要翻译： 一种用于阻尼具有至少一个绕组的同步伺服电动机的阻尼器电路，至少一个主阻尼电阻器，用于将主阻尼电阻器与绕组串联连接的连接装置，以及包括至少一个附加阻尼器 电阻器通过连接到控制模块的静态开关与主阻尼电阻器并联连接，用于根据绕组的电压来控制开关。 控制模块具有与主阻尼电阻并联的并联。 分路具有连接到开关的控制输入的输出端和连接到分流器的分压器桥，以在绕组的电压和分路的导通电压之间形成比较器。
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8.发明申请ANGULAR POSITION SENSOR AND ASSEMBLY COMPRISING A ROTARY SYSTEM AND SUCH A SENSOR 有权角位置传感器和包括旋转系统和其他传感器的组件公开(公告)号：US20120217957A1
公开(公告)日：2012-08-30
申请号：US13504124
申请日：2010-11-05
申请人： Jérôme Piaton
发明人： Jérôme Piaton
IPC分类号： G01B7/30
CPC分类号： G01D5/145 , G01D5/2451
摘要： The invention relates to a sensor (1000) for continuously measuring the angular position (θa) of a shaft (1) rotatably mounted relative to a housing (2). Said sensor comprises: a stator (20); a rotor (10) attachable to the shaft (1); permanent magnets (3) having alternating polarities (N, S), located on the stator (20) or the rotor (10), and capable of creating magnetic induction (B) during the rotation of the rotor (10); a magnetic circuit (21) for channeling said magnetic induction (B) such that it is proportional to a sinusoidal function of the angle (?r) of the rotor (10); and at least two electric transducers (4) having linear output, each angularly offset (φ) one from the other relative to the stator (20) and located in the gaps (210) arranged in said circuit (21). The magnetic circuit (21) is toothed and comprises at least one measuring unit (5) comprising three teeth (211) per pair of (30) magnets (3), each tooth comprising a gap (210) taking a transducer (4).
摘要翻译： 本发明涉及一种用于连续地测量相对于壳体（2）可旋转地安装的轴（1）的角位置（＆A; a）的传感器（1000）。 所述传感器包括：定子（20）; 可连接到所述轴（1）的转子（10）; 具有位于定子（20）或转子（10）上的交替极性（N，S）的永磁体（3），并且能够在转子（10）旋转期间产生磁感应（B）; 用于引导所述磁感应（B）使得其与转子（10）的角度（θr）的正弦函数成比例的磁路（21）; 和至少两个具有线性输出的电子换能器（4），每个电子换能器（4）相对于定子（20）彼此成角度地偏移（＆phgr），并且位于布置在所述电路（21）中的间隙（210）中。 磁路（21）是齿形的并且包括至少一个测量单元（5），每个测量单元（5）包括每对（30）磁体（3）的三个齿（211），每个齿包括取换换器（4）的间隙（210）。
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公开(公告)号：US20110254394A1
公开(公告)日：2011-10-20
申请号：US13141159
申请日：2009-11-17
申请人： Jérôme Piaton
发明人： Jérôme Piaton
IPC分类号： H02K7/102
CPC分类号： F16H25/2252 , F16H2025/2078 , H02K7/06 , H02K7/106
摘要： The electric motor consists of a rotor fitted with permanent magnets and comprises a stator the armature of which is made up of two parts: a stack of laminations forming round teeth and a solid tube-shaped field frame made of a material of the stainless steel kind enveloping the said stack of laminations. This armature constitutes a non-disengageable braking system that produces a damping effect in the face of possible movements of its rotor which are brought about and/or imposed by the members with which it collaborates. This motor can be used for driving a roto-linear actuator device with satellite rollers which is used as an actuator for manoeuvring the control surfaces of an aircraft, for example an aileron.
摘要翻译： 电动机包括一个装有永久磁铁的转子，它包括一个定子，其电枢由两部分组成：一叠形成圆形的叠片和一个由不锈钢材料制成的实心管状场框架 包围所述堆叠的叠片。 该电枢构成不能脱离的制动系统，其面向其转子的可能的运动产生阻尼作用，这是由与其协作的构件带来和/或施加的。 该电动机可以用于驱动具有卫星辊的旋转线性致动器装置，其用作用于操纵飞机（例如副翼）的控制表面的致动器。
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10.发明授权Aircraft flight control system comprising a connecting rod provided with a sensor 有权飞行器飞行控制系统包括设置有传感器的连杆公开(公告)号：US08950706B2
公开(公告)日：2015-02-10
申请号：US13260596
申请日：2010-03-30
申请人： Arnaud Duyck , Bruno Tilly , François Guillot , Jérôme Piaton
发明人： Arnaud Duyck , Bruno Tilly , François Guillot , Jérôme Piaton
摘要： A control system, in particular an aircraft flight control system, having a linkage with a force-transmission link (3), the link having a body (5) having at least one end housing (8) slidably receiving a coupling rod (9) for coupling the link to an adjacent element of the linkage, the housing being closed by an elastically-deformable test member (10) through which the rod passes and that has an inner periphery fastened to the rod and an outer periphery fastened to a wall defining the end housing, and the end housing receiving at least one sensor (11) for sensing relative movement between the rod and the body.
摘要翻译： 具有与力传递连杆（3）连接的控制系统，特别是飞机飞行控制系统，所述连杆具有主体（5），该主体具有可滑动地接收联接杆（9）的至少一个端部壳体（8） 用于将连杆联接到联动装置的相邻元件，壳体由可弹性变形的测试构件（10）封闭，杆可穿过该构件（10），并且具有固定到杆的内周边，以及限定 所述端部壳体和所述端部壳体接收至少一个用于感测所述杆和所述主体之间的相对运动的传感器（11）。
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