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公开(公告)号：US20060085100A1
公开(公告)日：2006-04-20
申请号：US11045348
申请日：2005-01-31
IPC分类号： G06F17/00
CPC分类号： H02J1/14 , B64D11/0624 , Y10T307/25 , Y10T307/50
摘要： The installation (10) for controlling power in an aircraft comprises: a power distribution network (22); at least two subscribers (14A, 14B, 14C) connected to the network (22); a central power control unit (20) which is capable of allocating a total available power level to each subscriber; and means for determining the total power effectively consumed for each load of the subscribers. The central power control unit (20) comprises means (18B) for acquiring information which represents the total power effectively consumed by each subscriber and is capable of allocating the total available power to each subscriber in accordance with the total power levels effectively consumed by the subscribers.
摘要翻译： 用于控制飞机中的动力的装置（10）包括：配电网（22）; 连接到网络（22）的至少两个用户（14A，14B，14C）; 中央功率控制单元（20），其能够向每个用户分配总可用功率水平; 以及用于确定用户的每个负载有效消耗的总功率的装置。 中央功率控制单元（20）包括用于获取表示每个用户有效消耗的总功率的信息的装置（18B），并且能够根据由所述用户有效消耗的总功率电平向每个用户分配总可用功率 订阅者。
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公开(公告)号：US20050081973A1
公开(公告)日：2005-04-21
申请号：US10500578
申请日：2003-01-09
CPC分类号： B60C23/004
摘要： A wheel assembly for a vehicle, includes a wheel rim (16) and a tire (18) defining a closed space (30) therebetween which is filled with a pressurized gas. The inventive wheel assembly also includes a pressurized-gas reservoir (40) and elements (50) for selectively connecting the pressurized-gas reservoir (40) to the closed space (30) defined between the wheel rim (16) and the tire (18). The pressurized-gas reservoir (40) is rotationally fixed to the wheel rim (16).
摘要翻译： 一种用于车辆的车轮组件，包括轮辋（16）和轮胎（18），其在其间限定有填充有加压气体的封闭空间（30）。 本发明的轮组件还包括加压气体储存器（40）和用于选择性地将加压气体储存器（40）连接到限定在轮缘（16）和轮胎（18）之间的封闭空间（30）的元件（50） ）。 加压气体储存器（40）旋转地固定到轮缘（16）。
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公开(公告)号：US06441576B1
公开(公告)日：2002-08-27
申请号：US09722501
申请日：2000-11-28
IPC分类号： B25J916
CPC分类号： B64D11/06395 , B60N2/0232 , B60N2/0244 , B60N2/0292 , B60N2/34 , B60N2/995 , B64D11/064 , B64D11/0641 , B64D11/0643
摘要： A device for actuating a seat element includes an actuator fitted with a transducer delivering a state information representative of the current position of the actuator and a unit for controlling the actuator which includes a device for registering and for storing several reference state informations each representative of a position of the actuator for an identified position of the element and a device for driving the actuator so as to move the seat element towards several target positions. The control unit is adapted so as, when a movement towards a predetermined target position is commanded, to activate the actuator until the current reference state information delivered by the transducer is equal to the reference state information stored for the position of the commanded element.
摘要翻译： 用于致动座椅元件的装置包括具有换能器的致动器，其传递表示致动器的当前位置的状态信息，以及用于控制致动器的单元，其包括用于登记和存储多个参考状态信息的装置，每个参考状态信息代表 用于所述元件的识别位置的致动器的位置和用于驱动致动器的装置，以便将座椅元件移动到多个目标位置。 控制单元适于在朝向预定目标位置的运动被命令时激活致动器，直到由换能器传送的当前参考状态信息等于为命令元件的位置存储的参考状态信息。
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4.发明申请Aircraft cabin equipped with means for controlling the power consumed by seat actuators 有权飞机机舱配备有用于控制座椅执行器消耗的功率的装置公开(公告)号：US20050231038A1
公开(公告)日：2005-10-20
申请号：US11094106
申请日：2005-03-31
CPC分类号： B64D11/06395 , A47C31/126 , B64D11/064 , B64D11/0643 , H02J1/14
摘要： The aircraft cabin comprises: at least two seats (14A, 14B, 14C) which each comprise at least two elements which can be moved relative to each other and at least one actuator (24, 26) for the relative displacement of these movable elements, at least one central power control unit (20) in the cabin in order to allocate a total available power level to each seat. Each seat (14A, 14B, 14C) comprises means (30, 32, 34) for reading at least one item of morphological information of the passenger sitting in the seat, and means (18B) for transmitting information to the central power control unit (20) in accordance with the or each item of morphological information. The central power control unit (20) is capable of allocating to each seat (14A, 14B, 14C) a total available power level in accordance with the or each item of morphological information.
摘要翻译： 飞机舱包括：至少两个座（14A，14B，14C），每个座包括至少两个可相对于彼此移动的元件和至少一个致动器（24,26），用于使这些元件相对移动 可移动元件，在舱室中的至少一个中央功率控制单元（20），以便为每个座椅分配总可用功率水平。 每个座椅（14A，14B，14C）包括用于读取坐在座椅中的乘客的至少一个形态信息的装置（30,32,34），以及用于将信息发送到中央的装置（18B） 功率控制单元（20）根据或每个项目的形态信息。 中央电源控制单元（20）能够根据形状信息或每个项目向每个座位（14A，14B，14C）分配总可用功率电平。
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5.发明申请NOISE REDUCTION DEVICE FOR TURBOJET NACELLE WITH MOBILE CHEVRONS, AND ASSOCIATED NACELLE 有权具有移动雨刷的涡轮增压器的噪声减少装置和相关的NACELLE公开(公告)号：US20110139540A1
公开(公告)日：2011-06-16
申请号：US13057935
申请日：2009-08-05
IPC分类号： F02K1/34
摘要： The invention relates to a turbojet nacelle (1) and to an aeroacoustic noise reduction device for said nacelle, the nacelle comprising a nozzle (10) on the downstream end thereof, said nozzle (10) comprising an inner wall inside which a first flow from the turbojet circulates and an outer wall (102) outside which a second flow corresponding to the surrounding outside air circulates. The invention also relates to an aeroacoustic noise reduction device (20) of the turbojet, comprising a plurality of chevrons (201) arranged on the circumference of the nozzle (10). The invention is characterised in that the aeroacoustic noise reduction device also comprises a slide (202) arranged on the circumference of the nozzle in such a way that it can rotate about the axis of the nozzle, each chevron (201) being connected to the slide (202) by means of a guiding element (204) that can move along the slide (202) during the rotation thereof in order to ensure the displacement of the chevron (201).
摘要翻译： 本发明涉及涡轮喷气发动机舱（1）和用于所述机舱的空气声学降噪装置，所述机舱在其下游端包括喷嘴（10），所述喷嘴（10）包括内壁，所述喷嘴 涡轮喷气发生器循环，外壁（102）在其外部对应于周围的外部空气的第二流动循环。 本发明还涉及一种涡轮喷气发动机的气声降噪装置（20），包括布置在喷嘴（10）的圆周上的多个人字（201）。 本发明的特征在于，所述气动噪音降低装置还包括布置在所述喷嘴的圆周上的滑动件（202），使得其能够围绕所述喷嘴的轴线旋转，每个人字形件（201）连接到所述滑块 （202），其能够在其旋转期间沿着所述滑动件（202）移动以便确保所述人字形件（201）的位移的引导元件（204）。
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公开(公告)号：US20100089191A1
公开(公告)日：2010-04-15
申请号：US12527584
申请日：2007-10-26
CPC分类号： B64C13/34 , F16H25/2454 , Y10T74/18704
摘要： The invention relates to a jack (1) that comprises, on the one hand, a rod (2) that can be driven in translation by a driving system (5, 6), and, on the other hand, a system for blocking the expansion of the rod that comprises at least one bolt (9) mounted so as to move between an engagement position, in which it defines an abutment means for the rod in the expansion direction thereof, and a release position, in which it is spaced away from the rod and allows the expansion thereof, wherein the bolt is associated with a barrel (14) having a first stable position in which it maintains the bolt (9) in the engagement position and a second stable position in which it maintains the bolt (9) in its release position, said barrel system (14) being designed so that it can be alternatively switched from the first stable position to the second stable position under the action of the rod (2) driven by a slight backward movement before expansion and at the end of the return stroke.
摘要翻译： 本发明涉及一种千斤顶（1），其一方面包括可由驱动系统（5,6）平移驱动的杆（2），另一方面，包括用于阻挡 所述杆的膨胀包括至少一个螺栓（9），所述至少一个螺栓（9）安装成在接合位置之间移动，所述接合位置在所述接合位置之间移动，所述接合位置在所述接合位置中限定所述杆沿其膨胀方向的抵接装置和释放位置， 并且允许其膨胀，其中所述螺栓与具有第一稳定位置的筒体（14）相关联，在所述第一稳定位置中，所述螺栓将所述螺栓（9）保持在所述接合位置，在所述第二稳定位置中，所述螺栓（9）保持在所述螺栓 9）在其释放位置中，所述枪管系统（14）被设计成使得它可以在膨胀之前由轻微向后运动驱动的杆（2）的作用下从第一稳定位置切换到第二稳定位置，并且 在回程结束时。
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公开(公告)号：US07286910B2
公开(公告)日：2007-10-23
申请号：US11045348
申请日：2005-01-31
CPC分类号： H02J1/14 , B64D11/0624 , Y10T307/25 , Y10T307/50
摘要： The installation (10) for controlling power in an aircraft comprises a power distribution network (22); at least two subscribers (14A, 14B, 14C) connected to the network (22); a central power control unit (20) which is capable of allocating a total available power level to each subscriber; and a device for determining the total power effectively consumed for each load of the subscribers. The central power control unit (20) acquires information which represents the total power effectively consumed by each subscriber and is capable of allocating the total available power to each subscriber in accordance with the total power levels effectively consumed by the subscribers.
摘要翻译： 用于控制飞机中的动力的装置（10）包括配电网（22）; 连接到网络（22）的至少两个用户（14A，14B，14C）; 中央功率控制单元（20），其能够向每个用户分配总可用功率水平; 以及用于确定用户的每个负载有效消耗的总功率的设备。 中央功率控制单元（20）获取表示每个用户有效消耗的总功率的信息，并且能够根据用户有效消耗的总功率电平为每个用户分配总可用功率。
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8.发明授权Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle 有权具有移动人字纹的涡轮喷气发动机舱和相关机舱的降噪装置公开(公告)号：US08430203B2
公开(公告)日：2013-04-30
申请号：US13057935
申请日：2009-08-05
IPC分类号： F02K1/00
摘要： The invention relates to a turbojet nacelle (1) and to an aeroacoustic noise reduction device for said nacelle, the nacelle comprising a nozzle (10) on the downstream end thereof, said nozzle (10) comprising an inner wall inside which a first flow from the turbojet circulates and an outer wall (102) outside which a second flow corresponding to the surrounding outside air circulates. The invention also relates to an aeroacoustic noise reduction device (20) of the turbojet, comprising a plurality of chevrons (201) arranged on the circumference of the nozzle (10). The invention is characterized in that the aeroacoustic noise reduction device also comprises a slide (202) arranged on the circumference of the nozzle in such a way that it can rotate about the axis of the nozzle, each chevron (201) being connected to the slide (202) by means of a guiding element (204) that can move along the slide (202) during the rotation thereof in order to ensure the displacement of the chevron (201).
摘要翻译： 本发明涉及涡轮喷气发动机舱（1）和用于所述机舱的空气声学降噪装置，所述机舱在其下游端包括喷嘴（10），所述喷嘴（10）包括内壁，所述喷嘴 涡轮喷气发生器循环，外壁（102）在其外部对应于周围的外部空气的第二流动循环。 本发明还涉及一种涡轮喷气发动机的气声降噪装置（20），包括布置在喷嘴（10）的圆周上的多个人字（201）。 本发明的特征在于，所述气动噪音降低装置还包括布置在所述喷嘴的圆周上的滑动件（202），使得其能够围绕所述喷嘴的轴线旋转，每个人字形件（201）连接到所述滑块 （202），其能够在其旋转期间沿着所述滑动件（202）移动以便确保所述人字形件（201）的位移的引导元件（204）。
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公开(公告)号：US07954759B2
公开(公告)日：2011-06-07
申请号：US11919353
申请日：2006-06-12
IPC分类号： F02K1/54
CPC分类号： F02K1/76 , B64D29/08 , F05D2240/14 , F05D2270/52 , F05D2270/62 , Y02T50/671
摘要： The invention relates to an electrical control system for the nacelle of a turboreactor, comprising a plurality of electromechanical maneuvering elements for a plurality of actuating devices embodied as auxiliary parts of the turboreactor. The invention is characterized in that the control system comprises an electronic control box comprising a plurality of control inlets to be connected to control elements, and a plurality of outlets connected to electromechanical maneuvering of the auxiliary actuating devices. The control box can translate each instruction received into an operating sequence for at least one corresponding electromechanical maneuvering element. The invention also relates to a nacelle and an aircraft provided with one such control system.
摘要翻译： 本发明涉及一种用于涡轮反应器的机舱的电气控制系统，其包括用于多个作为涡轮反应器的辅助部件的致动装置的机电操纵元件。 本发明的特征在于，该控制系统包括一个电子控制箱，该电子控制箱包括多个要连接到控制元件的控制进口，以及连接到辅助致动装置的机电操纵的多个出口。 控制箱可以将接收的每条指令转换成至少一个对应的机电操纵元件的操作顺序。 本发明还涉及一种具有一个这样的控制系统的机舱和飞机。
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公开(公告)号：US20070240803A1
公开(公告)日：2007-10-18
申请号：US11764238
申请日：2007-06-18
IPC分类号： B60C23/00
CPC分类号： B60C23/004
摘要： A wheel assembly for a vehicle, includes a wheel rim (16) and a tire (18) defining a closed space (30) therebetween which is filled with a pressurized gas. The inventive wheel assembly also includes a pressurized-gas reservoir (40) and elements (50) for selectively connecting the pressurized-gas reservoir (40) to the closed space (30) defined between the wheel rim (16) and the tire (18). The pressurized-gas reservoir (40) is rotationally fixed to the wheel rim (16).
摘要翻译： 一种用于车辆的车轮组件，包括轮辋（16）和轮胎（18），其在其间限定有填充有加压气体的封闭空间（30）。 本发明的轮组件还包括加压气体储存器（40）和用于选择性地将加压气体储存器（40）连接到限定在轮缘（16）和轮胎（18）之间的封闭空间（30）的元件（50） ）。 加压气体储存器（40）旋转地固定到轮缘（16）。
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