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1. 发明申请

US20100001131A1 Method of and Apparatus for Producing Aerodynamic Resistance on an Aircraft 审中-公开
标题翻译：在飞机上产生气动阻力的方法和装置
公开(公告)号：US20100001131A1
公开(公告)日：2010-01-07
申请号：US12301751
申请日：2007-05-09
申请人： Anil B. Mertol , Volker Cleemann , Carsten Weber , Markus Fischer
发明人： Anil B. Mertol , Volker Cleemann , Carsten Weber , Markus Fischer
IPC分类号： B64C9/32 , B64C9/36
CPC分类号： B64C9/32 , B64C9/326 , B64C9/36
摘要： The invention concerns an apparatus for and a method of producing aerodynamic resistance on an aircraft, comprising at least one braking flap, wherein the at least one braking flap can be extended into the airflow around the aircraft. In accordance with the invention at least one braking flap is arranged on the fuselage of the aircraft in a region over the wings of the aircraft.
摘要翻译：本发明涉及一种用于在飞行器上产生空气阻力的装置和方法，其包括至少一个制动挡板，其中所述至少一个制动挡板可以延伸到飞行器周围的气流中。根据本发明，至少一个制动挡板布置在飞行器的机身的机身上方在飞行器的机翼上的区域中。

2. 发明授权

US09315255B2 Aircraft comprising a device for influencing the directional stability of the aircraft, and a method for influencing the directional stability of the aircraft 有权
标题翻译：包括用于影响飞行器的方向稳定性的装置的飞行器以及影响飞行器的方向稳定性的方法
公开(公告)号：US09315255B2
公开(公告)日：2016-04-19
申请号：US13255246
申请日：2010-03-17
申请人： Carsten Weber , Markus Fischer , Arnaud Namer
发明人： Carsten Weber , Markus Fischer , Arnaud Namer
IPC分类号： B64C5/06 , B64C9/32
CPC分类号： B64C5/06 , B64C9/32 , Y02T50/32
摘要： An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.
摘要翻译：提供了包括用于影响飞行器的方向稳定性的装置的飞机。该装置包括控制输入装置; 飞行控制装置; 用于获取飞行器的转速的传感器装置，包括偏航率; 以及与副翼，扰流器，电梯和方向舵耦合的至少一个致动器。飞行控制装置包括控制功能，该控制功能根据控制命令产生用于控制飞行器的致动器的调节命令。飞机包括两个尾部安装的翼片，每个翼片包括与飞行控制装置连接的致动器，其彼此对称并且在机身的相对侧上对准，并且可在缩回位置和伸出位置之间移动。控制功能被设计成使得基于所获取的旋转速度而基于控制命令生成的调节命令包括调整到尾部安装的翼片的致动器的命令。

3. 发明申请

US20120205490A1 AIRCRAFT HORIZONTAL STABILISER FITTED WITH LEADING-EDGE STRAKE 审中-公开
标题翻译：飞机水平稳定器配有前沿边缘
公开(公告)号：US20120205490A1
公开(公告)日：2012-08-16
申请号：US13502175
申请日：2010-10-18
申请人： Ian Roy Whitehouse , Carsten Weber , Markus Fischer , Alain Tanguy
发明人： Ian Roy Whitehouse , Carsten Weber , Markus Fischer , Alain Tanguy
IPC分类号： B64C5/02 , B64C5/06
CPC分类号： B64C5/02 , B64C23/06 , Y02T50/162
摘要： An adjustable, or all-moving, horizontal stabiliser for an aircraft, the stabiliser having a leading edge, a trailing edge, a root and a tip, and a strake fixed with respect to the stabiliser and attached to, or integrally formed with, the stabiliser leading edge adjacent the root.
摘要翻译：一种用于飞行器的可调节或全移动的水平稳定器，所述稳定器具有前缘，后缘，根部和尖端以及相对于所述稳定器固定或与所述稳定器一体形成的支架稳定器前缘毗邻根部。

4. 发明授权

US10543899B2 Aircraft horizontal stabiliser fitted with leading-edge strake 有权
公开(公告)号：US10543899B2
公开(公告)日：2020-01-28
申请号：US13502175
申请日：2010-10-18
申请人： Ian Roy Whitehouse , Carsten Weber , Markus Fischer , Alain Tanguy
发明人： Ian Roy Whitehouse , Carsten Weber , Markus Fischer , Alain Tanguy
IPC分类号： B64C5/02
摘要： An adjustable, or all-moving, horizontal stabiliser for an aircraft, the stabiliser having a leading edge, a trailing edge, a root and a tip, and a strake fixed with respect to the stabiliser and attached to, or integrally formed with, the stabiliser leading edge adjacent the root.

5. 发明申请

US20120104184A1 AIRCRAFT COMPRISING A DEVICE FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT, AND A METHOD FOR INFLUENCING THE DIRECTIONAL STABILITY OF THE AIRCRAFT 有权
标题翻译：包含影响飞机方向稳定性的装置的飞机，以及影响飞机方向稳定性的方法
公开(公告)号：US20120104184A1
公开(公告)日：2012-05-03
申请号：US13255246
申请日：2010-03-17
申请人： Carsten Weber , Markus Fischer , Arnaud Namer
发明人： Carsten Weber , Markus Fischer , Arnaud Namer
IPC分类号： B64C13/16 , B64C9/02 , B64C9/08 , B64C9/00
CPC分类号： B64C5/06 , B64C9/32 , Y02T50/32
摘要： An aircraft including a device for influencing the directional stability of the aircraft is provided. The device includes a control-input device; a flight control device; a sensor device for acquiring the rotation rates, including the yaw rates, of the aircraft; and at least one actuator, which is coupled with ailerons, spoilers, an elevator and a rudder. The flight control device includes a control function generating adjusting commands for the actuators for controlling the aircraft according to control commands. The aircraft includes two tail-mounted flaps, each including an actuator connected with the flight control device, situated symmetrically to each other and on opposite sides of the fuselage, and movable between retracted and extended positions. The control function is designed such that the adjusting commands that are generated on the basis of the control commands depending on the acquired rotation rates include adjusting commands to the actuators of the tail-mounted flaps.
摘要翻译：提供了包括用于影响飞行器的方向稳定性的装置的飞机。该装置包括控制输入装置; 飞行控制装置; 用于获取飞行器的转速的传感器装置，包括偏航率; 以及与副翼，扰流器，电梯和方向舵耦合的至少一个致动器。飞行控制装置包括控制功能，该控制功能根据控制命令产生用于控制飞行器的致动器的调节命令。飞机包括两个尾部安装的翼片，每个翼片包括与飞行控制装置连接的致动器，其彼此对称并且在机身的相对侧上对准，并且可在缩回位置和伸出位置之间移动。控制功能被设计成使得基于所获取的旋转速度而基于控制命令生成的调节命令包括调整到尾部安装的翼片的致动器的命令。

6. 发明授权

US08893669B2 Hybrid cooling system of an internal combustion engine 有权
标题翻译：内燃机混合冷却系统
公开(公告)号：US08893669B2
公开(公告)日：2014-11-25
申请号：US13278941
申请日：2011-10-21
申请人： Jan Mehring , Bernd Steiner , Carsten Weber
发明人： Jan Mehring , Bernd Steiner , Carsten Weber
IPC分类号： F01P7/00 , F01P3/02 , F01M1/12 , F01P3/00
CPC分类号： F01P3/02 , F01M2001/123 , F01P2003/008 , F01P2003/021 , F01P2003/024 , F01P2037/02
摘要： A hybrid cooling system for an engine is provided. The system comprises a block oil cooling circuit, a head coolant cooling circuit, the head and block circuits having a common heat exchanger. The system also includes a flow device in the head cooling circuit for preventing coolant flow in the head cooling circuit at least during a first phase of a warm-up phase of the internal combustion engine, a delivery device in the block cooling circuit which delivers engine oil constantly under pressure through the block cooling circuit to bearing points in a cylinder block and to bearing points in a cylinder head, and a control element arranged in a control line to reduce the delivery capacity of the delivery device through the block cooling circuit at least during the first phase of the warm-up phase. In this way, heat transfer in the common heat exchanger may be substantially prevented.
摘要翻译：提供了一种用于发动机的混合冷却系统。该系统包括块油冷却回路，头部冷却剂冷却回路，头部和块状回路具有共同的热交换器。该系统还包括头部冷却回路中的流动装置，用于至少在内燃机的预热阶段的第一阶段期间防止冷却剂在头部冷却回路中的流动;块冷却回路中的输送装置，其输送发动机在压力下通过块体冷却回路将油保持在气缸体中的轴承点和气缸盖中的轴承点，以及布置在控制线中的控制元件，以至少通过块冷却回路减少输送装置的输送能力在预热阶段的第一阶段。以这种方式，可以基本上防止公共热交换器中的热传递。

7. 发明授权

US08821865B2 High concentration anti-TNFα antibody liquid formulations 有权
标题翻译：高浓度抗TNFα抗体液体制剂
公开(公告)号：US08821865B2
公开(公告)日：2014-09-02
申请号：US13294692
申请日：2011-11-11
申请人： Michael Neu , Markus Tschoepe , Carsten Weber , Wolfgang Fraunhofer , Laura Redden , Martin Gastens , Alexander Feick
发明人： Michael Neu , Markus Tschoepe , Carsten Weber , Wolfgang Fraunhofer , Laura Redden , Martin Gastens , Alexander Feick
IPC分类号： A61K39/395 , C07K16/24 , A61K39/00
CPC分类号： C07K16/241 , A61K9/0019 , A61K39/39591 , A61K47/26 , A61K2039/505 , C07K2317/21 , C07K2317/565 , C07K2317/76 , C07K2317/90 , C07K2317/94 , Y02A50/412
摘要： The invention provides a liquid aqueous pharmaceutical formulation comprising a human anti-TNFa antibody, or antigen-binding portion thereof, which reduces pain associated with injection in a subject by at least about 50% when compared to injecting an otherwise identical formulation comprising at least one salt and/or at least one buffer. The invention also provides a liquid aqueous pharmaceutical formulation comprising a human anti-TNFa antibody, or antigen-binding portion thereof, having increased bioavailability upon subcutaneous administration into a subject. The formulation may comprise a therapeutic protein, such as a human anti-TNF-alpha antibody, or an antigen-binding portion thereof, or a biosimilar thereof.
摘要翻译：本发明提供了包含人抗TNFα抗体或其抗原结合部分的液体水性药物制剂，当与注射包含至少一种抗体的相同的制剂相比时，将与受试者中注射相关的疼痛降低至少约50％盐和/或至少一种缓冲液。本发明还提供了包含人抗TNFα抗体或其抗原结合部分的液体水性药物制剂，其在皮下施用于受试者时具有增加的生物利用度。制剂可以包含治疗性蛋白质，例如人抗TNF-α抗体或其抗原结合部分，或其生物相似物。

8. 发明授权

US08607639B2 Method and device for determining mechanical stress load and interface effects on particles dispersed in a fluid 有权
标题翻译：用于确定分散在流体中的颗粒的机械应力负荷和界面效应的方法和装置
公开(公告)号：US08607639B2
公开(公告)日：2013-12-17
申请号：US13049362
申请日：2011-03-16
申请人： Hans-Jürgen Krause , Carsten Weber , Sonja Simon , Wolfgang Peukert
发明人： Hans-Jürgen Krause , Carsten Weber , Sonja Simon , Wolfgang Peukert
IPC分类号： G01N3/00
CPC分类号： G01N1/286 , G01N11/04 , G01N33/487
摘要： The present invention concerns a method and a device for determining mechanical stress load, and optionally interface effects, on particles dispersed in a fluid. According to the invention, fluid comprising dispersed particles such as biomolecules is fed into a sample space of a device comprising a jacket which encloses a sample chamber and at least two rolls arranged within said jacket such that said sample space is defined between said rolls, said rolls being independently rotatable with respect to each other, wherein said jacket has an inner surface which is essentially adapted to the outer surface of the rolls, rotational movement is imparted to at least one of the rolls of said device, and changes in the state of said particles are determined from which mechanical stress load acting on the particles can be determined.
摘要翻译：本发明涉及一种用于确定分散在流体中的颗粒的机械应力负荷和任选的界面效应的方法和装置。根据本发明，包含分散颗粒如生物分子的流体被送入装置的样品空间中，所述装置包括封套样品室的外套和布置在所述夹套内的至少两个辊，使得所述样品空间限定在所述辊之间，所述辊可以相对于彼此独立地旋转，其中所述护套具有基本适合于辊的外表面的内表面，旋转运动被赋予所述装置的至少一个辊，并且转动状态的变化从确定作用在颗粒上的机械应力载荷确定所述颗粒。

9. 发明申请

US20120031191A1 METHOD AND DEVICE FOR DETERMINING MECHANICAL STRESS LOAD AND INTERFACE EFFECTS ON PARTICLES DISPERSED IN A FLUID 有权
标题翻译：用于确定液体中分散的颗粒的机械应力载荷和界面效应的方法和装置
公开(公告)号：US20120031191A1
公开(公告)日：2012-02-09
申请号：US13049362
申请日：2011-03-16
申请人： Hans-Jürgen Krause , Carsten Weber , Sonja Simon , Wolfgang Peukert
发明人： Hans-Jürgen Krause , Carsten Weber , Sonja Simon , Wolfgang Peukert
IPC分类号： G01B5/30
CPC分类号： G01N1/286 , G01N11/04 , G01N33/487
摘要： The present invention concerns a method and a device for determining mechanical stress load, and optionally interface effects, on particles dispersed in a fluid. According to the invention, fluid comprising dispersed particles such as biomolecules is fed into a sample space of a device comprising a jacket which encloses a sample chamber and at least two rolls arranged within said jacket such that said sample space is defined between said rolls, said rolls being independently rotatable with respect to each other, wherein said jacket has an inner surface which is essentially adapted to the outer surface of the rolls, rotational movement is imparted to at least one of the rolls of said device, and changes in the state of said particles are determined from which mechanical stress load acting on the particles can be determined
摘要翻译：本发明涉及一种用于确定分散在流体中的颗粒的机械应力负荷和任选的界面效应的方法和装置。根据本发明，包含分散颗粒如生物分子的流体被送入装置的样品空间中，所述装置包括封套样品室的外套和布置在所述夹套内的至少两个辊，使得所述样品空间限定在所述辊之间，所述辊可以相对于彼此独立地旋转，其中所述护套具有基本适合于辊的外表面的内表面，旋转运动被赋予所述装置的至少一个辊，并且转动状态的变化从确定作用在颗粒上的机械应力载荷确定所述颗粒

10. 外观设计

USD645623S1 Laundry appliance 有权
标题翻译：洗衣用具
公开(公告)号：USD645623S1
公开(公告)日：2011-09-20
申请号：US29387183
申请日：2011-03-10
申请人： Jacques Helot , Andrew Roberson , Carsten Weber
设计人： Jacques Helot , Andrew Roberson , Carsten Weber

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