公开(公告)号：US07987709B2

公开(公告)日：2011-08-02

申请号：US12525071

申请日：2008-01-31

申请人： Cyril Barre ,  Michel Dos-Reis ,  Hervé Magnin

发明人： Cyril Barre ,  Michel Dos-Reis ,  Hervé Magnin

IPC分类号： G01F1/68

CPC分类号： G01P5/10 ,  G01P5/12 ,  G01P13/006 ,  G01P13/04

摘要： A device for measuring the flow speed of a fluid as well as its direction and its orientation, based on a thermal-sensor measurement principle, that comprises at least three flow measurement probes each having a sensitive member and an obstacle masking a predetermined measurement area of the sensor, characterized in that the flow measurement probes are attached on carrier posts, the carrier posts defining the obstacles that form masking members for an angular sector of the flow measurement probes facing the sensitive member of the probes.

摘要翻译： 一种用于测量流体的流速以及其方向及其取向的装置，其基于热传感器测量原理，其包括至少三个流量测量探针，每个流量测量探针具有敏感部件和障碍物遮蔽预定的测量区域 所述传感器的特征在于，所述流量测量探针附接在载体柱上，所述载体柱限定形成用于面向所述探针的敏感构件的所述流量测量探针的角部分的掩蔽构件的障碍物。

公开(公告)号：US07959107B2

公开(公告)日：2011-06-14

申请号：US11765065

申请日：2007-06-19

申请人： Jacques Beaufort

发明人： Jacques Beaufort

IPC分类号： B64C1/14

CPC分类号： B64D29/06 ,  E05D3/022 ,  E05Y2900/502 ,  Y10T16/522

摘要： A hinge device of a nacelle cowling of an aircraft engine on a supporting structure is disclosed. The hinge device includes two fittings and a link rod connected thereto and mounted on the fitting by an end connection. The link rod is further mounted on the fitting by an intermediate connection including a pivot pin slidably housed in a hole, and the end connection includes a guide pin slidably housed in a guide ramp. The connections are designed so as to create, upon rotation of the link rod about the pin, a relative movement of the axis in the ramp, simultaneously causing a relative movement of the pin in the hole.

摘要翻译： 公开了一种在支撑结构上的飞机发动机的机舱罩的铰链装置。 铰链装置包括两个配件和连接到其上的连杆，并通过端部连接安装在配件上。 连杆通过包括可滑动地容纳在孔中的枢轴销的中间连接件进一步安装在配件上，并且端连接件包括可滑动地容纳在引导斜坡中的引导销。 连接件被设计成在链条围绕销旋转时产生轴在斜面中的相对运动，同时引起销在孔中的相对移动。

公开(公告)号：US07952492B2

公开(公告)日：2011-05-31

申请号：US12304451

申请日：2007-06-07

申请人： Florian Constans

发明人： Florian Constans

IPC分类号： G01C23/00 ,  G05D1/12

CPC分类号： G05D1/0676

摘要： A landing assistance device and method for an aircraft according to the invention, based on the landing procedure rules attached to the runway, a lower threshold and an upper threshold of total energy acceptable for the aircraft are determined and the current total energy of the latter is compared with the thresholds.

摘要翻译： 根据本发明的飞机的着陆辅助装置和方法，基于附接到跑道的着陆程序规则，确定飞行器可接受的总能量的下阈值和上限阈值，并且后者的当前总能量 与门槛相比。

公开(公告)号：US07942580B2

公开(公告)日：2011-05-17

申请号：US11608971

申请日：2006-12-11

申请人： Virginie Audart-Noel ,  Stephane Levert

发明人： Virginie Audart-Noel ,  Stephane Levert

IPC分类号： F16C27/00

CPC分类号： F16C11/0614 ,  B64D27/26 ,  B64D2027/266 ,  F16C27/02 ,  F16C2326/43 ,  Y02T50/44

摘要： A rear suspension (10) for an aircraft engine assembly comprises a structure comprising two three-point shackles (12, 12′) and one two-point shackle (14). One of the hinge pins in waiting on the two-point shackle (14), preferably the hinge pin (26) fixed to the engine yoke joint, is mounted with clearance and with a damping ring acting as a spring to prevent vibrations of the engines as long as the hinge pin (26) is not engaged. Each of the suspension connecting pins (10) is a ball joint connection, the beam (16) of the suspension (10) being provided with five aligned orifices (24, 24a, 28, 24′, 24a′).

摘要翻译： 用于飞机发动机组件的后悬架（10）包括包括两个三点钩环（12,12'）和一个两点卸扣（14）的结构。 等待两点卸扣（14）的铰链销之一，优选地固定在发动机轭架接头上的铰链销（26）安装有间隙，并具有用作弹簧的阻尼环，以防止发动机振动 只要铰链销（26）不接合即可。 悬挂连接销（10）中的每一个是球接头连接，悬架（10）的梁（16）设置有五个对准的孔（24,24a，28,24'，24a'）。

公开(公告)号：US07940195B2

公开(公告)日：2011-05-10

申请号：US12105688

申请日：2008-04-18

申请人： Nicolas Fabas ,  Fabien Cases ,  Laurent Signol ,  Serge Blind

发明人： Nicolas Fabas ,  Fabien Cases ,  Laurent Signol ,  Serge Blind

IPC分类号： G08B21/00

CPC分类号： G05B23/0272

摘要： A method for updating a content of a given warning message emitted in an aircraft by a monitoring system in case of detection of a particular state of at least one monitored system of the aircraft, the method including a step of delivery of a plurality of modification information items to a selection tool, each modification information item defining a modification of a content of a warning message capable of being emitted by the monitoring system, the selection tool being capable of selecting at least one information item among the plurality of modification information items in such a way as to permit modification of the content of the given warning message.

摘要翻译： 一种用于在检测到飞行器的至少一个被监视系统的特定状态的情况下更新由监视系统在飞行器中发射的给定警告消息的内容的方法，所述方法包括传送多个修改信息的步骤 项目到选择工具，每个修改信息项定义能够被监视系统发出的警告消息的内容的修改，所述选择工具能够选择所述多个修改信息项中的至少一个信息项 允许修改给定警告消息的内容的方式。

公开(公告)号：US07939962B2

公开(公告)日：2011-05-10

申请号：US11689821

申请日：2007-03-22

申请人： Etienne Foch ,  Gaetan Bisson ,  Pascal Maussion ,  Maria Pietrzak-David ,  Maurice Fadel

发明人： Etienne Foch ,  Gaetan Bisson ,  Pascal Maussion ,  Maria Pietrzak-David ,  Maurice Fadel

IPC分类号： B60L1/00 ,  H02J3/06

CPC分类号： H02J1/10 ,  B64D2221/00 ,  H02J4/00 ,  Y02T50/54 ,  Y10T307/313 ,  Y10T307/391

摘要： The invention relates to a power supply system for several user systems onboard an aircraft. This system comprises at least two power supply electronics (10, 11) and means of connecting these at least two power supply electronics to at least two user systems (12, 13, 14, 15), characterised in that these connecting means comprise a network of connecting contactors (16, 17; 32, 33) from each power supply electronics with at least two user systems not performing similar functions but technologically compatible such that these power supply electronics supply these user systems at different times.

摘要翻译： 本发明涉及一种用于飞机上的多个用户系统的电源系统。 该系统包括至少两个电源电子设备（10,11）以及将这些至少两个电源电路连接到至少两个用户系统（12,13,14,15）的装置，其特征在于，这些连接装置包括网络 将来自每个电源电子设备的接触器（16,17; 32,33）与不具有相似功能但技术上相容的至少两个用户系统连接，使得这些电源电子设备在不同时间提供这些用户系统。

公开(公告)号：US07933714B2

公开(公告)日：2011-04-26

申请号：US11995024

申请日：2006-07-13

申请人： Fabien Fetzmann ,  Pierre Coldefy ,  Thierry Malaval ,  Stéphane Collins

发明人： Fabien Fetzmann ,  Pierre Coldefy ,  Thierry Malaval ,  Stéphane Collins

IPC分类号： G01S19/21 ,  G01C21/00 ,  G06F19/00

CPC分类号： G01C23/00

摘要： A device includes a current position unit for determining a current position of a aircraft, a mapping database, a navigation system, a current heading unit for determining the current heading of the aircraft, and a display system for displaying on a viewing screen, at least a partial map of the airport and, thereon, an aircraft symbol which is positioned at the current position and which is oriented in accordance with the current heading.

摘要翻译： 一种装置包括用于确定飞行器当前位置的当前位置单元，映射数据库，导航系统，用于确定飞行器当前航向的当前航向单元，以及至少在观看屏幕上显示的显示系统 机场的部分地图，以及位于当前位置并根据当前航向定向的飞机符号。

公开(公告)号：US07926261B2

公开(公告)日：2011-04-19

申请号：US12067931

申请日：2006-09-13

申请人： Alain Porte

发明人： Alain Porte

IPC分类号： F02K3/02

CPC分类号： F01D9/065 ,  B64D13/06 ,  F02C6/08 ,  F02C7/14 ,  F02C7/18 ,  F02K3/06 ,  F28D7/1615 ,  F28D7/1669 ,  F28D7/1684 ,  F28D2021/0021 ,  Y02T50/675

摘要： The invention is a turbofan provided with a pre-cooler. In order to evacuate the heated cool air stream, at least one discharge pipe is arranged in a chamber and connects the pre-cooler to at least one discharge orifice provided in the inner fairing, in output of an exhaust nozzle and at least more or less opposite the wing.

摘要翻译： 本发明是一种具有预冷器的涡轮风扇。 为了排出加热的冷空气流，至少一个排放管布置在室中，并将预冷器连接到设置在内部整流装置中的至少一个排出孔，并且在排气喷嘴的输出中至少或多或少地 在机翼对面

公开(公告)号：US07911165B2

公开(公告)日：2011-03-22

申请号：US12017578

申请日：2008-01-22

申请人： Laurent Peyras ,  David Rousset

发明人： Laurent Peyras ,  David Rousset

IPC分类号： H02P21/00

CPC分类号： H02P21/06

摘要： A device for controlling an electromechanical actuator includes an electric motor and an actuator operated by the electric motor. It also includes a digital signal processor (DSP) providing data of reference voltages (Ud—ffw, Uq—ffw) on the basis of an decoupled electrical model of the motor. The processor has at least one Park transformation module receiving measurement data for the currents of at least two supply phases of the motor (i_mot—2, i_mot—3) and a datum for the estimated angle of the motor (θestimated) and transforming them into data regarding the component of current with stator current axis (id) and the component of current in quadrature with the stator current (iq).

摘要翻译： 用于控制机电致动器的装置包括电动机和由电动机操作的致动器。 它还包括基于电动机的去耦电模型提供参考电压（Ud-ffw，Uq-ffw）的数据的数字信号处理器（DSP）。 该处理器具有至少一个Park变换模块，用于接收电动机至少两个供电相位（i_mot-2，i_mot-3）的电流的测量数据和用于估计电动机角度（“估计”）和变换 它们成为具有定子电流轴（id）的电流分量和定子电流（iq）正交的电流分量的数据。

公开(公告)号：US07908043B2

公开(公告)日：2011-03-15

申请号：US11949233

申请日：2007-12-03

申请人： Fabrice Villaume ,  David Chabe ,  Stephane Delannoy

发明人： Fabrice Villaume ,  David Chabe ,  Stephane Delannoy

IPC分类号： G05D1/08

CPC分类号： G05D1/0083

摘要： A control device a determination device for determining a roll objective, and a calculation device for calculating, on the basis of the roll objective, a deflection order which is applied exclusively to ailerons of the aircraft.

摘要翻译： 一种控制装置，用于确定滚动目标的确定装置，以及用于根据滚动目标计算专门用于飞行器副翼的偏转顺序的计算装置。