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1. 发明授权

US08100362B2 Cockpit and aircraft including such cockpit 有权
标题翻译：驾驶舱和飞机包括这样的驾驶舱
公开(公告)号：US08100362B2
公开(公告)日：2012-01-24
申请号：US12162379
申请日：2007-01-29
申请人： Bernard Guering
发明人： Bernard Guering
IPC分类号： B64C1/00 , B64C13/00 , B64C13/04 , B64C39/02 , B64D25/12
CPC分类号： B64C1/068 , B64C1/22
摘要： A cockpit and an aircraft including such cockpit. The cockpit includes a front section of an aircraft. Such cockpit includes a pressure bulkhead sealing the section and a pressurization system for pressurizing such section.
摘要翻译：驾驶舱和包括这种驾驶舱的飞机。驾驶舱包括飞机的前部。这种驾驶舱包括密封该部分的压力隔板和用于对该区段加压的加压系统。

2. 发明授权

US08083182B2 Monolithic self-stiffened panels 有权
标题翻译：单片自加强板
公开(公告)号：US08083182B2
公开(公告)日：2011-12-27
申请号：US11996302
申请日：2006-07-12
申请人： Bruno Cacciaguerra
发明人： Bruno Cacciaguerra
IPC分类号： B64C1/14
CPC分类号： B64C25/16 , B64C1/12 , B64C2001/0072 , B64C2001/0081 , Y02T50/43
摘要： A composite panel having a first skin forming the outer wall of the panel, known as the lower face (1), and a second skin forming part of the inner wall of the panel. The second skin is formed hollow such as to produce an inner reinforcing frame (2) in the form of a half-box structure (3) which, together with the first skin, forms box parts. The aforementioned frame is equipped with a rim (4a, 4b) for fixing to the first skin, a face known as the upper face (5) and connecting side walls (6, 6a, 6b, 6c, 6d, 6e, 7) between the rim (4a, 4b) and the upper face (5) the first and second skins forming a monolithic self-stiffened panel. The half-box frame (2) has perforated sections (8) which are defined by hollow beam sections forming the half-box frame (2).
摘要翻译：一种复合面板，其具有形成面板外壁的第一皮肤，称为下表面（1），以及形成面板内壁部分的第二皮肤。第二皮肤形成为中空的，以产生半框结构（3）形式的内部加强框架（2），其与第一皮肤一起形成箱体部件。上述框架配备有用于固定到第一皮肤的边缘（4a，4b），称为上表面（5）的表面和连接侧壁（6,6a，6b，6c，6d，6e，7）之间的边缘边缘（4a，4b）和上表面（5），第一和第二表皮形成一体的自加强板。半框框架（2）具有由形成半框框架（2）的中空梁部分限定的穿孔部分（8）。

3. 发明授权

US08066221B2 Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing 有权
标题翻译：飞机腹侧整流罩分隔壁和飞机配有腹侧整流罩
公开(公告)号：US08066221B2
公开(公告)日：2011-11-29
申请号：US12096459
申请日：2006-11-23
申请人： Francois Rouyre
发明人： Francois Rouyre
IPC分类号： B64C1/10 , B64C1/38
CPC分类号： B64C7/00 , B64C1/26
摘要： The invention concerns a wall (10) of vertical partitioning for a ventral cowling of an aircraft including a plurality of vertical panels (11, 12, 12′, 13, 13′), each panel being linked to an adjacent panel by a vertical post (14, 15, 16). At least one exterior panel (13, 13′) is mounted in a fixed manner on at least one associated vertical post (14, 16). The upper end of said vertical post is fitted with a means of fastening in transverse rotation intended to be fixed to the structure (8) of an aircraft, the means of fastening in transverse rotation being capable of allowing the displacement (Dy) of the structure of the aircraft with respect to the fixed partitioning wall. It is also possible for at least one intermediary panel (12, 12′) to be mounted floating on at least one associated vertical post (15, 16), in such a way as to have a deflection parallel and perpendicular to the adjacent panels.
摘要翻译：本发明涉及一种包括多个垂直面板（11,12,12'，13,13'）的飞行器的腹部整流罩的垂直分隔壁（10），每个面板通过垂直柱连接到相邻的面板（14,15,16）。至少一个外部面板（13,13'）以固定的方式安装在至少一个相关联的垂直柱（14,16）上。所述立柱的上端装有横向旋转固定在飞行器结构（8）上的装置，横向旋转的紧固装置能够允许结构的位移（Dy）相对于固定分隔壁的飞机。至少一个中间面板（12,12'）也可以浮动地安装在至少一个相关联的垂直柱（15,16）上，以便具有平行且垂直于相邻面板的偏转。

4. 发明授权

US08065899B2 Advanced feed device for a superplastic press forming system 有权
标题翻译：用于超塑性压制成型系统的先进进料装置
公开(公告)号：US08065899B2
公开(公告)日：2011-11-29
申请号：US12419673
申请日：2009-04-07
申请人： Valerie Frustie
发明人： Valerie Frustie
IPC分类号： B21B45/02 , B21D37/16
CPC分类号： B21D37/14 , B21D26/055 , Y10S72/709
摘要： A feed device for a superplastic press-forming press has a slide that moves vertically and a base between which is held a tool having a cover and a bottom die enclosing a forming tool, which includes at least one heating shuttle to transport the bottom die, equipped with the forming tool and a cover, with the heating shuttle adapted to complete the press and constitute the base of the press during a hot-press forming operation.
摘要翻译：用于超塑性压制成型压力机的进料装置具有垂直移动的滑动件和保持具有盖的工具的底座和封闭成形工具的底模，该成型工具包括至少一个用于输送底模的加热梭，装有成形工具和盖子，加热梭适于在热压成形操作期间完成压机并构成压机的基座。

5. 发明授权

US08014912B2 Method and device for aiding the piloting of an airplane during an approach phase 有权
标题翻译：在接近阶段帮助驾驶飞机的方法和装置
公开(公告)号：US08014912B2
公开(公告)日：2011-09-06
申请号：US11934608
申请日：2007-11-02
申请人： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Bénédicte Michal , Adrien Ott , Frédéric Lemoult
发明人： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Bénédicte Michal , Adrien Ott , Frédéric Lemoult
IPC分类号： G06G7/00 , G08B21/00 , G05D1/04 , G06F17/00
CPC分类号： G08G5/025 , G08G5/0021
摘要： A method and device for aiding the piloting of an airplane includes: (1) determining current values of flight parameters of the airplane, (2) determining, with the aid of the current values, an approach distance that corresponds to a distance in a horizontal plane between the current position of the airplane and a position of contact with the ground, and (3) presenting the approach distance on a screen.
摘要翻译：一种用于辅助飞机驾驶的方法和装置包括：（1）确定飞机的飞行参数的当前值，（2）借助于当前值确定对应于水平距离的接近距离在飞机的当前位置和与地面接触的位置之间的平面，以及（3）在屏幕上呈现接近距离。

6. 发明授权

US08005583B2 Method and device for determining the air turbulence likely to be encountered by an aircraft 有权
标题翻译：用于确定飞机可能遇到的空气湍流的方法和装置
公开(公告)号：US08005583B2
公开(公告)日：2011-08-23
申请号：US11693191
申请日：2007-03-29
申请人： Isabelle Lacaze , Jacques Rosay , Jean-Pierre Daniel
发明人： Isabelle Lacaze , Jacques Rosay , Jean-Pierre Daniel
IPC分类号： G06F7/70 , G06F19/00 , G06G7/00 , G06G7/76
CPC分类号： G01C23/00 , G01W1/00 , G01W2001/003
摘要： A method and device for determining the air turbulence likely to be encountered by a first aircraft may use a turbulence indication from a second aircraft so as to make and use a prediction of the impact of the turbulence on the first aircraft if it is located in a particular position.
摘要翻译：用于确定可能由第一飞行器遇到的空气湍流的方法和装置可以使用来自第二飞行器的湍流指示，以便如果湍流位于特殊的位置。

7. 发明申请

US20110198918A1 DEVICE AND METHOD FOR STANDBY POWER SUPPLY ON BOARD AN AIRCRAFT 有权
标题翻译：飞机上的待机电源的装置和方法
公开(公告)号：US20110198918A1
公开(公告)日：2011-08-18
申请号：US12294435
申请日：2007-03-13
申请人： Olivier Langlois , Etienne Foch
发明人： Olivier Langlois , Etienne Foch
IPC分类号： B60L1/00 , H02K7/18
CPC分类号： B64D41/00 , B64D41/007 , B64D2041/002 , B64D2221/00 , F03D9/12 , F03D9/25 , F03D9/32 , F05B2220/50 , Y02E10/725 , Y02E60/16 , Y02T50/44 , Y02T50/54
摘要： A device and a method for emergency electricity supply on board an aircraft, able to supply a part of the aircraft's electrical power circuit. The device includes a synchronous machine with separate excitation, associated with a flywheel, and an auxiliary device to set the flywheel in rotation and to maintain rotation of the flywheel.
摘要翻译：一种用于飞机上的紧急电力供应的装置和方法，能够提供飞机电力电路的一部分。该装置包括具有与飞轮相关联的单独激励的同步机，以及用于将飞轮旋转并保持飞轮旋转的辅助装置。

8. 发明授权

US07996121B2 Device and method for assisting in the management of an engine failure on an aircraft 有权
标题翻译：用于协助在飞机上管理发动机故障的装置和方法
公开(公告)号：US07996121B2
公开(公告)日：2011-08-09
申请号：US12027229
申请日：2008-02-06
申请人： Daniel Ferro , Amelie David
发明人： Daniel Ferro , Amelie David
IPC分类号： G05D1/00 , G06F7/00
CPC分类号： G08G5/025 , G01C23/00 , G05D1/0072 , G08G5/0056
摘要： A device and method for assisting in the management of an engine failure on an aircraft: (1) determine, when an engine failure occurs, flight profiles allowing the closest airports to be reached according to flight strategies and (2) present, on a screen, the airports associated with the determined flight profiles and corresponding predictions.
摘要翻译：一种用于协助管理飞机上的发动机故障的装置和方法：（1）确定发动机故障发生时，根据飞行策略允许最接近机场的航班概况，以及（2）在屏幕上显示，与确定的航班概况相关联的机场和相应的预测。

9. 发明授权

US07959453B2 Electrical cabinet with electrical connection to its door 有权
标题翻译：电气柜与电气连接到其门
公开(公告)号：US07959453B2
公开(公告)日：2011-06-14
申请号：US11718899
申请日：2005-11-18
申请人： Bernard Guering
发明人： Bernard Guering
IPC分类号： H01R35/00
CPC分类号： E05D11/0081 , E05Y2900/208 , H02B1/38 , H02G11/00
摘要： The invention concerns an electrical cabinet (1) including a housing (2), a door (3) and a hinge (4). The housing and the door support electric wires which are each routed from an electrical component located inside an electrical equipment compartment (11) formed by the housing towards the outside of the compartment to be connected to a corresponding electrical connector (17). Therefor, according to the invention the electric wires are routed through the hinge which is itself connected to the electrical connector. The hinge forms at least one passage orifice (18, 19) guiding, the electric wires from inside the compartment towards the outside of the compartment while directing them towards the electrical connector.
摘要翻译：本发明涉及一种包括壳体（2），门（3）和铰链（4）的电气柜（1）。所述外壳和所述门支撑电线各自从位于由所述壳体形成的电气设备隔间（11）内部的电气部件路由到所述隔间的外部，以连接到相应的电连接器（17）。因此，根据本发明，电线通过自身连接到电连接器的铰链。所述铰链形成至少一个通道孔（18,19），其将所述电线从所述隔室内部朝向所述隔室的外部引导，同时将它们引向所述电连接器。

10. 发明授权

US07934425B2 Non-destructive ultrasound inspection method and measurement probe for implementing the method 有权
标题翻译：非破坏性超声检查方法和测量探头实现方法
公开(公告)号：US07934425B2
公开(公告)日：2011-05-03
申请号：US11930276
申请日：2007-10-31
申请人： Pierre Barbeau , Guillaume Ithurralde
发明人： Pierre Barbeau , Guillaume Ithurralde
IPC分类号： G01N29/06
CPC分类号： G01N29/2462 , G01N29/221 , G01N2291/044 , G01N2291/104 , G01N2291/106 , G01N2291/2694
摘要： A method for inspecting a part by a non-destructive ultrasound inspection, the part is immersed in an acoustic wave conducting medium and an incident ultrasound wave having a wide beam of section Σ is emitted into the ultrasound-conducting medium towards the part. The characteristics of the waves reflected by faces of the part to be inspected are measured on at least a small section σ, the characteristic dimensions of which are substantially less than those of the section Σ. The location of the section or sections σ is determined such that, despite the possible variations of the position of the part and the relative slopes of its faces, the section σ is always located in the volumes passed through by the reflected waves, for example substantially in an area close to the axis of the incident beam when the incident beam is controlled to be oriented substantially in a direction perpendicular to a face of the part.
摘要翻译：一种通过非破坏性超声波检查检查部件的方法，该部件浸没在声波导电介质和具有宽横截面积Sgr的入射超声波中; 朝向该部分发射到超导传导介质中。测量被检测部件表面反射的波的特性至少在小截面尺寸上测量，其特征尺寸基本上小于部分＆Sgr; 该部分或部分的位置＆sgr; 确定为尽管部件的位置和其面部的相对斜率可能的变化，总是位于反射波通过的体积中，例如当入射光束被控制为基本上在垂直于该部分的面的方向上时，基本上在接近入射光束的轴线的区域中。

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