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1. 发明申请

US20110266104A1 DEVICE AND PROCESS FOR OSCILLATION INSULATION IN A TRANSMISSION PATH 失效
标题翻译：传输路径振荡绝缘的装置和过程
公开(公告)号：US20110266104A1
公开(公告)日：2011-11-03
申请号：US10838233
申请日：2004-05-05
申请人： Marius Bebesel , Peter Janker , Rudolf Maier , Henning Strehlow
发明人： Marius Bebesel , Peter Janker , Rudolf Maier , Henning Strehlow
IPC分类号： F16F7/00 , F16F15/02 , F16F15/00
CPC分类号： F16F15/005 , B64C2027/003
摘要： Device and process for oscillation insulation in a transmission path. The device includes a first body structured and arranged to undergo an oscillation movement, at least one rigid connection element, a second body connected to the first body via the at least one rigid connection element, and an actuator device attached to the at least one connection element. A sensor unit is arranged in an interface area of the at least one connection element, and a regulator unit, connected to the sensor unit, is arranged to control the actuator device to perform an elastic deformation equivalent to an oscillation movement of the first body. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：传输路径中振荡绝缘的装置和过程。该装置包括构造和布置成经历振荡运动的第一主体，至少一个刚性连接元件，经由至少一个刚性连接元件连接到第一主体的第二主体，以及附接到至少一个连接的致动器装置元件。传感器单元布置在所述至少一个连接元件的接口区域中，并且连接到所述传感器单元的调节器单元布置成控制所述致动器装置执行与所述第一主体的振荡运动相当的弹性变形。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

2. 发明授权

US08037981B1 Device and process for oscillation insulation in a transmission path 失效
标题翻译：传输路径中振荡绝缘的装置和过程
公开(公告)号：US08037981B1
公开(公告)日：2011-10-18
申请号：US10838233
申请日：2004-05-05
申请人： Marius Bebesel , Peter Jänker , Rudolf Maier , Henning Strehlow
发明人： Marius Bebesel , Peter Jänker , Rudolf Maier , Henning Strehlow
IPC分类号： F16F15/00
CPC分类号： F16F15/005 , B64C2027/003
摘要： Device and process for oscillation insulation in a transmission path. The device includes a first body structured and arranged to undergo an oscillation movement, at least one rigid connection element, a second body connected to the first body via the at least one rigid connection element, and an actuator device attached to the at least one connection element. A sensor unit is arranged in an interface area of the at least one connection element, and a regulator unit, connected to the sensor unit, is arranged to control the actuator device to perform an elastic deformation equivalent to an oscillation movement of the first body. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
摘要翻译：传输路径中振荡绝缘的装置和过程。该装置包括构造和布置成经历振荡运动的第一主体，至少一个刚性连接元件，经由至少一个刚性连接元件连接到第一主体的第二主体，以及附接到至少一个连接的致动器装置元件。传感器单元布置在所述至少一个连接元件的接口区域中，并且连接到所述传感器单元的调节器单元布置成控制所述致动器装置执行与所述第一主体的振荡运动相当的弹性变形。本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

3. 发明授权

US06178246B1 Apparatus for the active suppression of noise radiated by a surface 有权
标题翻译：用于主动抑制由表面辐射的噪声的装置
公开(公告)号：US06178246B1
公开(公告)日：2001-01-23
申请号：US09315770
申请日：1999-05-20
申请人： Marius Bebesel , Rudolf Maier , Klaus Schmidts
发明人： Marius Bebesel , Rudolf Maier , Klaus Schmidts
IPC分类号： A61F1106
CPC分类号： G10K11/178 , G10K2210/128 , G10K2210/1291 , G10K2210/32291
摘要： Noise generated by a noise radiating surface is actively suppressed by at least two axially sensitive noise sensors which produce a control signal for controlling a noise suppression actuator. The sensors integrate the sensed signal in an axially selective manner. The at least two sensors are sensing the signal in two directions which preferably cross each other orthogonally. The control signal activates the actuator in such a way that the actuator counteracts deflections or vibrations of the noise generating surface such as a vehicle body wall.
摘要翻译：由噪声辐射表面产生的噪声由至少两个轴向敏感的噪声传感器主动抑制，这些噪声传感器产生用于控制噪声抑制致动器的控制信号。传感器将感测到的信号以轴向选择的方式进行集成。至少两个传感器在两个方向上感测信号，这两个方向最好是正交地交叉。控制信号激励致动器，使得致动器抵消噪声产生表面（例如车体壁）的偏转或振动。

4. 发明授权

US06480609B1 Apparatus for suppressing structure borne noises 失效
标题翻译：抑制结构噪声的装置
公开(公告)号：US06480609B1
公开(公告)日：2002-11-12
申请号：US09277483
申请日：1999-03-26
申请人： Henning Strehlow , Peter Jaenker , Rudolf Maier
发明人： Henning Strehlow , Peter Jaenker , Rudolf Maier
IPC分类号： H03B2900
CPC分类号： F16F15/005 , B64C27/001 , B64C2027/002 , G10K11/178 , G10K2210/121 , G10K2210/1281 , G10K2210/1291 , G10K2210/32291
摘要： Body or structural noise transmitted through a connector such as a strut, that connects a noise source, such as an engine, to an enclosure, such as a passenger cabin or cell of a helicopter, is suppressed by at least one piezoactuator which is excited to counteract any vibrations of the strut caused by body noise so that body noise vibrations are cancelled or at least substantially suppressed. The excitation of the piezoactuator is controlled in closed loop fashion in response to feedback signals from a sensor secured to the connector.
摘要翻译：通过连接诸如发动机等噪声源的连接器（例如直升机的乘客舱或电池等）的连接器传递的主体或结构噪声被至少一个被激励的压电致动器抑制抵消由身体噪音引起的支柱的任何振动，使得身体噪音振动被消除或至少基本上被抑制。响应于来自固定到连接器的传感器的反馈信号，压电致动器的激励以闭环方式被控制。

5. 发明授权

US6099790A Method of manufacturing hollow bodies and blow molding machine for effecting the method 失效
标题翻译：制造中空体的方法和吹塑机的实施方法
公开(公告)号：US6099790A
公开(公告)日：2000-08-08
申请号：US189651
申请日：1998-11-10
申请人： Dirk Wehrens , Rudolf Maier , Frank Schuller , Willi Dohmen
发明人： Dirk Wehrens , Rudolf Maier , Frank Schuller , Willi Dohmen
IPC分类号： B29C49/04 , B29C49/32 , B29C49/42
CPC分类号： B29C49/4205 , B29C49/32 , B29C49/04
摘要： A method of manufacturing hollow bodies including inserting into spaced mold halves of a blow mold of a blow molding machine plastic hose-shaped blanks at an extrusion station of the blow molding machine and closing the blow mold, displacing the closed blow mold from the extrusion station to a calibration station of the blow molding machine, inserting thereat blow mandrels into respective cavities of the closed blow mold, lifting, after expiration of predetermined blow time, the blow mandrels, together with the blown hollow bodies to an intermediate position and removing the blown hollow bodies from the blow mandrels lifting the blow mandrels to their initial position thereof, and displacing the blow mold from the calibration station to the extrusion station, with the displacing of the blow mold between the extrusion station and the calibration station being effected by displacing the blow mold at a right angle to a connection line of arranged side-by-side cavities of the blow mold.
摘要翻译：一种制造中空体的方法，包括在吹塑机的挤出站处插入吹塑机塑料软管形坯料的吹塑模具的隔开的半模中，并关闭吹塑模具，使封闭的吹塑模具从挤出站到吹塑机的校准站，将吹塑心轴插入封闭的吹塑模具的相应的空腔中，在预定吹塑时间期满之后将吹塑心轴与吹制的中空体一起提升到中间位置，来自吹制心轴的中空体将打击心轴提升到其初始位置，并且将吹塑模具从校准站移动到挤出站，吹塑模具在挤出站和校准站之间的移位是通过将吹塑模具移位吹塑模具与吹塑模具的排列的并排空腔的连接线成直角。

6. 发明授权

US5720918A Method and apparatus for closing tool of plastics processing machine 失效
标题翻译：塑料加工机械关闭工具的方法和装置
公开(公告)号：US5720918A
公开(公告)日：1998-02-24
申请号：US637107
申请日：1996-04-24
申请人： Dieter Wollschlager , Rudolf Maier , Axel Helmenstein
发明人： Dieter Wollschlager , Rudolf Maier , Axel Helmenstein
IPC分类号： B29C33/24 , B29C45/67 , B29C49/04 , B29C49/56
CPC分类号： B29C45/6728 , B29C49/56 , B29C49/04
摘要： A method and an apparatus for closing the tool of a plastics-processing machine, especially a blow-molding machine, concerns a two-part tool (1, 2) which is supported by two tool mounting plates (3, 4), at least one run drive (5), at least two closure drives (8), and such that the closure drives (8) each have a hydraulic piston-cylinder system with a cylinder (9), a piston (10), and a cylinder rod (11), and such that an inflow (14) and an outflow (15) for hydraulic oil is situated at the cylinder (9). Also, the end of the piston rod (11) has an interlock element (12) which interacts with a counter-piece (13), such that the piston rod (11) does not interlock with the closure piece (13), in order to apply the closure force, until the tool (1, 2) is situated near its closed position. According to the invention, all the closure drives (8) for closing the tool (1, 2) with a high force are actuated by a common control or regulation mechanism; no synchronization devices between the individual closure drives 8 are present. The entire closure motion of the tool (1, 2) takes place continuously and without interruption of the closure process. In this way, a more economical mode of operation is achieved by a simpler and more economical design.
摘要翻译：用于封闭塑料加工机械，特别是吹塑机的工具的方法和装置涉及至少由两个工具安装板（3,4）支撑的两部分工具（1,2）一个行驶驱动器（5），至少两个闭合驱动器（8），并且使得闭合驱动器（8）各自具有液压活塞 - 气缸系统，其具有气缸（9），活塞（10）和气缸杆（11），并且使得用于液压油的流入物（14）和流出物（15）位于气缸（9）处。此外，活塞杆（11）的端部具有互锁元件（12），其与相对件（13）相互作用，使得活塞杆（11）不依次与闭合件（13）互锁施加闭合力，直到工具（1,2）位于其关闭位置附近。根据本发明，用于以高力关闭工具（1,2）的所有封闭驱动器（8）由共同的控制或调节机构致动; 在各个闭合驱动器8之间不存在同步装置。工具（1,2）的整个闭合运动连续发生，而不会中断闭合过程。以这种方式，通过更简单和更经济的设计实现更经济的操作模式。

7. 发明授权

US08302733B2 Acoustic absorber for aircraft engines 有权
标题翻译：飞机发动机吸声器
公开(公告)号：US08302733B2
公开(公告)日：2012-11-06
申请号：US11718366
申请日：2005-10-28
申请人： Alexander Peiffer , Rudolf Maier
发明人： Alexander Peiffer , Rudolf Maier
IPC分类号： E04B1/82 , B31F1/00
CPC分类号： G10K11/172 , F01N1/04 , F02C7/045 , F05D2250/283 , Y10T428/24149
摘要： The present invention relates to an acoustic absorber that is particularly suitable for aircraft engines and has a honeycomb-shaped 3-dimensional structure, which absorbs engine noise when used in an engine. The structure has a plurality of folded honeycomb structures formed by folding a flat semi-finished product.
摘要翻译：本发明涉及一种特别适用于飞机发动机的吸声器，并且具有蜂窝状的三维结构，其在发动机中使用时吸收发动机噪声。该结构具有通过折叠扁平半成品形成的多个折叠蜂窝结构体。

8. 发明申请

US20140341737A1 DEVICE FOR REDUCING STRUCTURAL VIBRATIONS OF AIRFOILS 有权
标题翻译：减少飞机结构振动的装置
公开(公告)号：US20140341737A1
公开(公告)日：2014-11-20
申请号：US14124961
申请日：2012-05-25
申请人： Stefan Storm , Rudolf Maier , Andreas Wildschek
发明人： Stefan Storm , Rudolf Maier , Andreas Wildschek
IPC分类号： B64C9/00
CPC分类号： B64C9/00 , B64C5/08 , B64C13/16 , B64C2027/004 , B64D2045/0085 , F16F7/1011 , Y02T50/44
摘要： A device for reducing structural vibrations of aerofoils in an aircraft comprises, in the region of the aerfoil tips, at least one force generator (24a) acting substantially in the direction of movement of the vibrations. This arrangement has the advantage that such a force generator (24a) is considerably less susceptible to wear than conventional aerodynamic flaps and therefore effective vibration damping is possible with a reduced outlay on maintenance and greater efficiency.
摘要翻译：用于减少飞行器中的机翼的结构振动的装置包括在翼型尖端的区域中至少一个作用在振动运动方向上的力发生器（24a）。这种布置的优点是，这种力发生器（24a）比传统的空气动力襟翼明显不易磨损，因此有效的减振是可能的，同时在维护和降低的效率方面减少了花费。

9. 发明授权

US08255096B2 Minimizing dynamic structural loads of an aircraft 有权
标题翻译：最大限度地减少飞机的动态结构载荷
公开(公告)号：US08255096B2
公开(公告)日：2012-08-28
申请号：US12161878
申请日：2007-01-19
申请人： Andreas Wildschek , Rudolf Maier , Falk Hoffmann , Matthieu Jeanneau , Nicky Aversa
发明人： Andreas Wildschek , Rudolf Maier , Falk Hoffmann , Matthieu Jeanneau , Nicky Aversa
IPC分类号： G01C23/00
CPC分类号： G05D1/0066
摘要： Minimizing dynamic structural loads of an aircraft, introduced by an external excitation, which, includes generating a signal (x) indicative of the external excitation; deriving signals (y) of pre-controlling for actuating control elements of the aircraft from the excitation indicating signal (x) in accordance with a pre-controlling rule, so as to reduce the dynamic structural loads introduced to the aircraft; generating an error signal (e, e*) representing performance of said pre-controlling; optimizing the pre-controlling rule by the error signal (e, e*) and/or the excitation indicating signal (x) so as to minimize the dynamic structural loads.
摘要翻译：最小化由外部激励引入的飞行器的动态结构负载，其包括产生指示外部激励的信号（x）; 根据预先控制的规则从激励指示信号（x）导出用于致动飞行器的控制元件的预控制信号（y），以便减少引入飞机的动态结构载荷; 产生表示所述预控制性能的误差信号（e，e *）; 通过误差信号（e，e *）和/或激励指示信号（x）优化预控制规则，以使动态结构负载最小化。

10. 发明申请

US20090084908A1 MINIMIZING DYNAMIC STRUCTURAL LOADS OF AN AIRCRAFT 有权
标题翻译：最小化飞机的动态结构载荷
公开(公告)号：US20090084908A1
公开(公告)日：2009-04-02
申请号：US12161878
申请日：2007-01-19
申请人： Andreas Wildschek , Rudolf Maier , Falk Hoffmann , Matthieu Jeanneau , Nicky Aversa
发明人： Andreas Wildschek , Rudolf Maier , Falk Hoffmann , Matthieu Jeanneau , Nicky Aversa
IPC分类号： B64C13/16
CPC分类号： G05D1/0066
摘要： Minimizing dynamic structural loads of an aircraft (2), introduced by an external excitation (1), which, comprises generating a signal (x) indicative of the external excitation (1); deriving signals (y) of pre-controlling for actuating control elements of the aircraft (2) from said excitation indicating signal (x) in accordance with a pre-controlling rule, so as to reduce the dynamic structural loads introduced to the aircraft (2); generating an error signal (e, e*) representing performance of said pre-controlling; optimizing the pre-controlling rule by said error signal (e, e*) and/or said excitation indicating signal (x) so as to minimize the dynamic structural loads.
摘要翻译：最小化由外部激励（1）引入的飞行器（2）的动态结构负载，其包括产生指示外部激励（1）的信号（x）; 根据预先控制的规则从所述激励指示信号（x）导出用于致动飞行器（2）的控制元件的预控制信号（y），以便减少引入飞行器的动态结构负载（2 ）; 产生表示所述预控制性能的误差信号（e，e *）; 通过所述误差信号（e，e *）和/或所述激励指示信号（x）优化预控制规则，以使动态结构负载最小化。

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