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1. 发明授权

US07874168B2 Modular refrigeration unit and process for assembling a modular refrigeration unit to a cabinet of a refrigeration appliance 有权
标题翻译：模块化制冷单元和用于将模块化制冷单元组装到制冷设备的机柜的过程
公开(公告)号：US07874168B2
公开(公告)日：2011-01-25
申请号：US11813570
申请日：2005-12-27
申请人： Ilan Cohen , Per Wennerström , Xavier Hue , Per Fonser
发明人： Ilan Cohen , Per Wennerström , Xavier Hue , Per Fonser
IPC分类号： F25B45/00
CPC分类号： F25D19/00 , F25D2317/067
摘要： The present invention relates to a modular refrigeration unit for a refrigeration appliance, and to a process for assembling the modular refrigeration unit to a cabinet of a refrigeration appliance. A modular refrigeration unit (3) includes a base plate (6) supporting a condensing assembly (7), which comprises condensing means (8) and a compressor (9), and an evaporating assembly (10) comprising an evaporator (11); the condensing assembly and the evaporating assembly are operatively interconnected. The evaporating assembly (10) is arranged, in use, vertically spaced apart and above the compressor (9); the evaporating assembly (10) is supported by support means (24) vertically extending from the base plate (6); insulating means (16) separate the evaporating assembly (10) from the condensing assembly (7, 107).
摘要翻译：本发明涉及一种用于制冷设备的模块化制冷单元，以及用于将模块化制冷单元组装到制冷设备的机柜的过程。模块化制冷单元（3）包括支撑冷凝组件（7）的底板（6），其包括冷凝装置（8）和压缩机（9），以及包括蒸发器（11）的蒸发组件（10）。冷凝组件和蒸发组件可操作地互连。蒸发组件（10）在使用中被布置成垂直间隔开并在压缩机（9）上方; 蒸发组件（10）由从基板（6）垂直延伸的支撑装置（24）支撑; 绝缘装置（16）将蒸发组件（10）与冷凝组件（7,107）分开。

2. 发明申请

US20090000316A1 Modular Refrigeration Unit and Process for Assembling a Modular Refrigeration Unit to a Cabinet of a Refrigeration Appliance 有权
标题翻译：模块化制冷单元和将模块化制冷单元组装到制冷设备的机柜中的过程
公开(公告)号：US20090000316A1
公开(公告)日：2009-01-01
申请号：US11813570
申请日：2005-12-27
申请人： Ilan Cohen , Per Wennerstrom , Xavier Hue , Per Fonser
发明人： Ilan Cohen , Per Wennerstrom , Xavier Hue , Per Fonser
IPC分类号： F25B45/00 , F25B1/00 , F25D21/14 , A47B96/00 , F25D19/00
CPC分类号： F25D19/00 , F25D2317/067
摘要： The present invention relates to a modular refrigeration unit for a refrigeration appliance, and to a process for assembling the modular refrigeration unit to a cabinet of a refrigeration appliance. A modular refrigeration unit (3) includes a base plate (6) supporting a condensing assembly (7), which comprises condensing means (8) and a compressor (9), and an evaporating assembly (10) comprising an evaporator (11); the condensing assembly and the evaporating assembly are operatively interconnected. The evaporating assembly (10) is arranged, in use, vertically spaced apart and above the compressor (9); the evaporating assembly (10) is supported by support means (24) vertically extending from the base plate (6); insulating means (16) separate the evaporating assembly (10) from the condensing assembly (7, 107).
摘要翻译：本发明涉及一种用于制冷设备的模块化制冷单元，以及用于将模块化制冷单元组装到制冷设备的机柜的过程。模块化制冷单元（3）包括支撑冷凝组件（7）的底板（6），其包括冷凝装置（8）和压缩机（9），以及包括蒸发器（11）的蒸发组件（10）。冷凝组件和蒸发组件可操作地互连。蒸发组件（10）在使用中被布置成垂直间隔开并在压缩机（9）上方; 蒸发组件（10）由从基板（6）垂直延伸的支撑装置（24）支撑; 绝缘装置（16）将蒸发组件（10）与冷凝组件（7,107）分开。

3. 发明授权

US08925871B2 Wing of an aircraft 有权
标题翻译：机翼
公开(公告)号：US08925871B2
公开(公告)日：2015-01-06
申请号：US13464960
申请日：2012-05-05
申请人： Xavier Hue , Bernhard Schlipf
发明人： Xavier Hue , Bernhard Schlipf
IPC分类号： B64C9/26 , B64C9/22
CPC分类号： B64C9/22
摘要： A wing of an aircraft provided with a main wing and an arrangement of leading edge lifting bodies, which as seen with reference to the incident flow direction are arranged on the leading edge, which are adjustably arranged on the main wing one behind another as seen in the spanwise direction of the main wing by means of respectively two positioning devices spaced apart from one another in the spanwise direction of the main wing. The wing has a connecting device, which is coupled to each of two adjacent leading edge lifting bodies, wherein the connecting device is configured such that in the event of a fracture of a positioning device of a positioning body external forces acting on the latter are transferred via the respective connecting device to the leading edge lifting bodies coupled up via the latter.
摘要翻译：具有主翼的飞机翼和前缘提升体的布置，其如参照入射流动方向所看到的那样布置在前缘上，前缘被可调节地布置在主翼上，如前所述通过分别在主翼的翼展方向上彼此间隔开的两个定位装置，主翼的翼展方向。机翼具有连接装置，其连接到两个相邻的前缘提升体中的每一个，其中连接装置被构造成使得在定位体的定位装置的断裂的情况下，作用在定位体上的外力被转移通过相应的连接装置连接到通过其连接的前缘提升体。

4. 发明授权

US08311494B2 Test unit for testing the frequency characteristic of a transmitter 有权
标题翻译：用于测试变送器频率特性的测试单元
公开(公告)号：US08311494B2
公开(公告)日：2012-11-13
申请号：US12518852
申请日：2006-12-15
申请人： Francois Dupis , Xavier Hue , Lionel Mongin , Jacques Trichet
发明人： Francois Dupis , Xavier Hue , Lionel Mongin , Jacques Trichet
IPC分类号： H03C1/62 , H04B17/00
CPC分类号： H04B17/15 , H04B17/101
摘要： A test unit for testing the frequency characteristics of one or more components of a transmitter of modulated signals. The test unit includes a data source for generating a test pattern of data. A test unit output is connected to the data source and connectable to an input of one or more of the components, for inputting the test pattern of data to the one or more components. The test unit includes a memory in which a first predetermined data sequence and a second predetermined data sequence are stored. The data source is connected with an data input to the memory, and the data source is arranged to generating the test pattern of data including the predetermined data sequences. When a modulated signal is generated in accordance with the test pattern of data will include a first signal part with a first frequency spectrum caused by the first predetermined data sequence and a second signal part after the first signal part, which second signal part has a second frequency spectrum caused by the second predetermined data sequence.
摘要翻译：用于测试调制信号发射机的一个或多个组件的频率特性的测试单元。测试单元包括用于产生数据测试模式的数据源。测试单元输出连接到数据源并且可连接到一个或多个组件的输入端，用于将数据的测试模式输入到一个或多个组件。测试单元包括其中存储有第一预定数据序列和第二预定数据序列的存储器。数据源与输入到存储器的数据连接，并且数据源被布置成产生包括预定数据序列的数据的测试模式。当根据数据的测试模式生成调制信号时，将包括由第一预定数据序列引起的具有第一频谱的第一信号部分和第一信号部分之后的第二信号部分，该第二信号部分具有第二信号部分由第二预定数据序列引起的频谱。

5. 发明授权

US07963484B2 Lift-augmenting flap, in particular for a leading edge flap, for an aerodynamically effective wing 有权
标题翻译：用于空气动力学有效的翼的提升增强翼，特别是用于前缘翼片
公开(公告)号：US07963484B2
公开(公告)日：2011-06-21
申请号：US11922068
申请日：2006-06-14
申请人： Morten Raudszus , Bernhard Schlipf , Luc Andreani , Xavier Hue , Mark Heintjes
发明人： Morten Raudszus , Bernhard Schlipf , Luc Andreani , Xavier Hue , Mark Heintjes
IPC分类号： B64C3/50
CPC分类号： B64C3/50 , Y02T50/14
摘要： A lift-augmenting leading edge flap for a carrying wing of an aircraft, wherein the flap comprises an essentially rigid main body which makes a transition from the first side to the second side of the wing the flap being adjustable by a retention- and actuation mechanism coupled between the flap and wing box, between a first, retracted, position and a second, extended, position, wherein the first transition region of the flap is slidable to rest in each position essentially free of any gap, against the first skin of the wing box or against the wing end cover, in relation to the wing end cover.
摘要翻译：一种用于飞行器的携带翼的提升增加的前缘翼片，其中所述翼片包括基本上刚性的主体，其从翼的第一侧向第二侧过渡，所述翼可通过保持和致动机构联接在所述翼片和翼盒之间，在第一缩回位置和第二延伸位置之间，其中所述翼片的第一过渡区域可滑动以在基本上没有任何间隙的每个位置中抵靠所述翼片的第一皮肤相对于机翼端盖，机翼盒或机翼端盖。

6. 发明申请

US20090272853A1 Lift-Augmenting Flap, in Particular for Leading Edge Flap, for an Aerodynamically Effective Wing 有权
标题翻译：升降翼，特别是前缘翼片，用于空气动力学有效的翼
公开(公告)号：US20090272853A1
公开(公告)日：2009-11-05
申请号：US11922068
申请日：2006-06-14
申请人： Morten Raudszus , Bernhard Schlipf , Luc Andreani , Xavier Hue , Mark Heintjes
发明人： Morten Raudszus , Bernhard Schlipf , Luc Andreani , Xavier Hue , Mark Heintjes
IPC分类号： B64C3/50 , B64C9/22
CPC分类号： B64C3/50 , Y02T50/14
摘要： A lift-augmenting leading edge flap for a carrying wing of an aircraft, wherein the flap comprises an essentially rigid main body which makes a transition from the first side to the second side of the wing the flap being adjustable by a retention- and actuation mechanism coupled between the flap and wing box, between a first, retracted, position and a second, extended, position, wherein the first transition region of the flap is slidable to rest in each position essentially free of any gap, against the first skin of the wing box or against the wing end cover, in relation to the wing end cover.
摘要翻译：一种用于飞行器的携带翼的提升增加的前缘翼片，其中所述翼片包括基本上刚性的主体，其从翼的第一侧向第二侧过渡，所述翼可通过保持和致动机构联接在所述翼片和翼盒之间，在第一缩回位置和第二延伸位置之间，其中所述翼片的第一过渡区域可滑动以在基本上没有任何间隙的每个位置中抵靠所述翼片的第一皮肤相对于机翼端盖，机翼盒或机翼端盖。

7. 发明申请

US20080282705A1 Chilled Beverage Storage Device 审中-公开
标题翻译：冷冻饮料储存装置
公开(公告)号：US20080282705A1
公开(公告)日：2008-11-20
申请号：US11885139
申请日：2006-02-13
申请人： Xavier Hue , Magnus Jonzon
发明人： Xavier Hue , Magnus Jonzon
IPC分类号： F25B21/02 , F25D3/08 , F28D15/00
CPC分类号： F25D31/007 , F25B21/02 , F25B2321/0251 , F25D11/006 , F25D16/00 , F25D2303/082 , F25D2331/803 , F25D2331/805 , F25D2331/809
摘要： The present invention relates to a chilled beverage storage device constituted by a cold area and a hot area; the cold area comprises a first structure (2) arranged towards at least one cold generating module (4, 5) and provided with at least one holding arrangement (1) adapted to hold, in direct contact, one or more beverage containers to be kept chilled; one or more reservoirs (7) containing a phase change material in thermal exchange with the cold generating module (4, 5) are arranged around the holding arrangement (1).
摘要翻译：本发明涉及由冷区域和热区域构成的冷冻饮料储存装置; 冷区域包括朝向至少一个冷发生模块（4,5）布置的第一结构（2），并且设置有至少一个保持装置（1），该保持装置适于直接接触要保持的一个或多个饮料容器冷藏一个或多个储存器（7）围绕保持装置（1）设置，其中包含与冷产生模块（4,5）热交换的相变材料。

8. 发明授权

US09422050B2 Fore flap disposed on the wing of an aircraft 有权
标题翻译：飞机前翼设在飞机机翼上
公开(公告)号：US09422050B2
公开(公告)日：2016-08-23
申请号：US13122733
申请日：2009-10-06
申请人： Bernhard Schlipf , Xavier Hue
发明人： Bernhard Schlipf , Xavier Hue
IPC分类号： B64C3/48 , B64C3/50 , B64C9/24 , B64C9/14
CPC分类号： B64C9/24 , B64C3/50 , B64C2009/143
摘要： A leading edge slat arranged on the aerofoil of an aircraft. The leading edge slat is provided on the front of the main wing. The leading edge slat has a partially extended setting, with its trailing edge flat against the wing, and a further extended setting, with its trailing edge spaced apart from the nose of the wing to open a gap feeding high-energy air from the lower surface of the slat to the upper surface of the wing. The leading edge slat includes a body and a trailing edge facing the main wing, which can be bent around the spanwise direction of the slat relative to the body, and on which the trailing edge of the slat is provided, and which by means of a device generating a contact force is loaded for making contact between the trailing edge of the slat and the profile nose of the wing.
摘要翻译：一架安排在飞机机翼上的前沿板条。前缘板条设置在主翼的前部。前缘板条具有部分延伸的设置，其后缘平坦地抵靠机翼，并且进一步延伸设置，其后缘与机翼的鼻部间隔开以打开从下表面供给高能量空气的间隙的板条到机翼的上表面。前缘板条包括主体和面向主翼的后缘，其可相对于主体围绕板条的翼展方向弯曲，并且在其上设置板条的后缘，并且借助于加载产生接触力的装置用于使板条的后缘与机翼的轮廓鼻之间接触。

9. 发明申请

US20140231592A1 LEADING EDGE RIB ASSEMBLY 有权
标题翻译：领先的边框总成
公开(公告)号：US20140231592A1
公开(公告)日：2014-08-21
申请号：US14232247
申请日：2012-07-06
申请人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
发明人： Simon Topping , Christopher Payne , Llifon Williams , Martin Mayneord , David Belfourd , Xavier Hue
IPC分类号： B64C13/34
CPC分类号： B64C13/34 , B64C9/02 , B64C9/22
摘要： An aircraft wing comprising a main wing element with a spar and a leading edge rib which is supported by the spar and extends forward of the spar; a high lift device which is movably mounted to the main wing element; and an actuation mechanism comprising a drive shaft and a gear train. The gear train comprising a drive cog which is carried by the drive shaft, an actuator cog which is coupled to the high lift device, and one or more intermediate cogs which are mounted to the rib and coupled in series with the drive cog and the actuator cog so as to transmit torque from the drive cog to the actuator cog which moves the high lift device between a retracted position and an extended position in which the high lift device increases the camber of the wing. The sizes of the cogs in the gear train are selected so that the drive shaft rotates at a higher rate than the high lift device.
摘要翻译：一种飞机机翼，包括具有翼梁的主翼元件和由翼梁支撑并延伸到翼梁前方的前缘肋骨; 可移动地安装到主翼元件的高升降装置; 以及包括驱动轴和齿轮系的致动机构。齿轮系包括由驱动轴承载的驱动齿轮，联接到高提升装置的致动器齿轮和一个或多个中间齿轮，其安装到肋并与驱动齿轮串联连接，并且致动器齿轮，以便将扭矩从驱动齿轮传递到致动器齿轮，致动器齿轮使高升程装置在缩回位置和伸出位置之间移动，在该位置，高升程装置增加机翼的弯度。选择齿轮系中的齿轮的尺寸，使得驱动轴以比高提升装置更高的速度旋转。

10. 发明申请

US20120061524A1 AEROFOIL COMPRISING A HIGH LIFT FLAP 有权
标题翻译： AEROFOIL包含一个高提升片
公开(公告)号：US20120061524A1
公开(公告)日：2012-03-15
申请号：US13255276
申请日：2010-03-29
申请人： Bernhard Schlipf , Xavier Hue
发明人： Bernhard Schlipf , Xavier Hue
IPC分类号： B64C3/50
CPC分类号： B64C9/22 , B64C9/02 , B64C9/16
摘要： A wing is provided, including a high-lift flap arranged on the wing such that it is movable by means of at least two adjustment mechanisms arranged side-by-side in the spanwise direction of the wing and adjustable by means of a drive device. Each adjustment mechanism includes a first adjustment lever, articulated on a main wing surface via a first pivotal articulation, with the formation of a first rotation axis; a second adjustment lever, articulated on the high-lift flap via a second pivotal articulation, with the formation of a second rotation axis; and a central articulation, linking together the first and the second adjustment levers, with the formation of a third rotation axis. An intermediate articulated part is arranged on at least one of the adjustment mechanisms for coupling the first adjustment lever and the main wing surface, or for coupling the second adjustment lever and the high-lift flap.
摘要翻译：设置有一个机翼，包括一个设置在机翼上的高升降挡板，使其能够通过在机翼的翼展方向上并排设置并通过驱动装置可调节的至少两个调节机构来移动。每个调节机构包括第一调节杆，通过第一枢转关节铰接在主翼表面上，形成第一旋转轴线; 第二调节杆，通过第二枢转关节铰接在高升降翼上，形成第二旋转轴; 以及将第一和第二调节杆连接在一起的中心关节，形成第三旋转轴线。在至少一个用于联接第一调节杆和主翼面的调节机构中，或用于联接第二调节杆和高升降挡板的中间铰接部件。

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