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1. 发明申请

US20080093500A1 Propulsive Anti-Torque System for Rotorcraft 有权
标题翻译：旋翼机推进式反扭矩系统
公开(公告)号：US20080093500A1
公开(公告)日：2008-04-24
申请号：US11662559
申请日：2004-09-28
申请人： Dudley Smith , Walter Joiner , Paul Madej , Charles Hollimon , Daniel Robertson
发明人： Dudley Smith , Walter Joiner , Paul Madej , Charles Hollimon , Daniel Robertson
IPC分类号： B64C27/82
CPC分类号： B64C27/82 , B64C2027/8245
摘要： A rotorcraft having an enhanced configuration in which a simple wing and a propulsive anti-torque system are combined is disclosed. The propulsive anti-torque system includes an anti-torque thruster system in which a variable pitch fan is installed internal to the tail boom of the rotorcraft and an anti-torque thruster nozzle is mounted at the extremity of the tail boom. The fan is driven directly from the main rotor drive. The configuration and location of the fan allows the primary exhaust from the engine to be mixed with the compressed air flow from the fan. The mixed air flow from the fan and the engine passes through the tail boom and out the thruster nozzle.
摘要翻译：公开了一种具有增强结构的旋翼航空器，其中简单翼和推进式反扭矩系统组合在一起。推进式反扭矩系统包括抗扭矩推进器系统，其中可变桨距风扇安装在旋翼航空器尾翼的内部，反扭矩推进器喷嘴安装在尾吊臂的末端。风扇直接从主转子驱动器驱动。风扇的配置和位置允许来自发动机的主排气与来自风扇的压缩空气流混合。来自风扇和发动机的混合空气流通过尾部悬臂并从推进器喷嘴出来。

2. 发明申请

US20060239824A1 Proprotor blade with leading edge slot 有权
标题翻译： Proprotor刀片带前缘槽
公开(公告)号：US20060239824A1
公开(公告)日：2006-10-26
申请号：US10543222
申请日：2003-01-23
申请人： Daniel Robertson , Dudley Smith , Charles Hollimon , Jimmy Narramore , B. Mullins
发明人： Daniel Robertson , Dudley Smith , Charles Hollimon , Jimmy Narramore , B. Mullins
IPC分类号： A23L3/18
CPC分类号： B64C11/16 , B64C27/467 , B64C29/0033
摘要： A proprotor blade (27a, 27b, 127a, 127b) having a fixed, spanwise, leading edge slot (215) located in at least the inboard portion of the proprotor is disclosed. The slot (215) is formed by a selectively shaped slat (217) disposed in a selectively shaped recessed area (219) located at the leading edge (202) of the main portion of the proprotor blade. The slot (215) is selectively shaped so the a portion of the airflow over the lower airfoil surface of the proprotor blade is diverted between the main portion of the proprotor blade and the slat (217) and exits at the upper airfoil surface of the proprotor blade. The present invention may be used on both military-type tiltrotor aircraft (11) and civilian-type tiltrotor aircraft (111) with only minor variations to accommodate the different shapes of the proprotor blades.
摘要翻译：公开了一种具有固定的，翼展方向的前缘槽（215）的推进器叶片（27a，27b，127a，127b），其位于至少在推进器的内侧部分中。狭槽215由位于驱动器叶片的主要部分的前缘（202）上的选择性形状的凹入区域（219）中的选择性地成形的板条（217）形成。狭槽215被选择成形，使得在推进器叶片的下翼面表面上的气流的一部分在推进器叶片的主要部分和板条（217）之间转向并在推进器的上部翼型表面处离开刀。本发明可以用于军用型倾转旋翼飞机（11）和民用型倾转旋翼飞机（111），只有微小的变化来适应不同形状的推进器叶片。

3. 发明申请

US20070137956A1 Dual spring rate damper 有权
标题翻译：双弹簧减震器
公开(公告)号：US20070137956A1
公开(公告)日：2007-06-21
申请号：US10568170
申请日：2004-08-27
申请人： Frank Stamps , Michael Smith , Christopher Bothwell , Lawrence Corso , James Braswell, Jr , David Popelka , Emst Schellhase , Charles Hollimon , Thomas Newman , Bryan Baskin , Thomas Campbell , Daniel Robertson
发明人： Frank Stamps , Michael Smith , Christopher Bothwell , Lawrence Corso , James Braswell, Jr , David Popelka , Emst Schellhase , Charles Hollimon , Thomas Newman , Bryan Baskin , Thomas Campbell , Daniel Robertson
IPC分类号： F16F9/00
CPC分类号： F16F13/08 , B64C27/35 , B64C27/39 , B64C27/51 , F16F13/24 , F16F13/26 , F16F2230/30
摘要： A damper has a piston having an axis, an outer surface, and opposing ends. Elastomeric seals are in sealing contact with the outer surface of the piston, the seals being coaxial with the piston and limiting movement of the piston to a path along the axis of the piston. The seals also define fluid chambers adjacent the ends of the piston. A primary passage communicates the fluid chambers, and a selectively switchable valve for controls a flow of fluid from one of the chambers to another of the chambers through the primary passage. When the flow of fluid through the primary passage is permitted, movement of the piston is resisted by a first spring rate due to a shear force required to cause shear deflection of the seals. When the flow of fluid through the primary passage is restricted, movement of the piston is resisted by a second spring rate due to a fluid force required to cause bulging deflection of the seals.
摘要翻译：阻尼器具有具有轴线，外表面和相对端的活塞。弹性密封件与活塞的外表面密封接触，密封件与活塞同轴并且限制活塞沿着活塞轴线的路径运动。密封件还限定了邻近活塞端部的流体室。主要通道连通流体室，以及可选择地可切换的阀，用于控制通过主通道从一个室到另一个腔的流体流。当允许通过主通道的流体流动时，活塞的运动由于需要剪切力而引起密封件的剪切偏转而抵抗第一弹簧刚度。当通过主通道的流体流被限制时，活塞的运动由于需要使密封件凸起偏转所需的流体力而受到第二弹簧刚度的抵抗。

4. 发明授权

US08419361B2 Anti fret liner assembly 有权
标题翻译：防油衬垫组件
公开(公告)号：US08419361B2
公开(公告)日：2013-04-16
申请号：US13222583
申请日：2011-08-31
申请人： Daniel Robertson
发明人： Daniel Robertson
IPC分类号： F01D25/24
CPC分类号： F01D25/246 , B01D46/02 , F01D9/042 , F05D2230/64
摘要： An anti-fret assembly for a turbine engine, the assembly comprising an elongated liner having first and second walls connected by a base to provide a generally U-shaped channel, the liner having an outer surface adapted to lie against a first component and an inner surface adapted to lie against a second component at least the first wall being provided with a notch for receipt of an anti-translation pin, the assembly further comprising an anti-translation pin.
摘要翻译：一种用于涡轮发动机的防油组件，该组件包括细长衬套，其具有通过基座连接以提供大致U形通道的第一和第二壁，所述衬套具有适于抵靠第一部件和内部至少所述第一壁具有用于接收反平移销的凹口的表面，所述表面适合于抵靠第二部件，所述组件还包括防翻转销。

5. 发明申请

US20130008173A1 POWER GENERATION ASSEMBLY AND METHOD 审中-公开
标题翻译：发电总成及方法
公开(公告)号：US20130008173A1
公开(公告)日：2013-01-10
申请号：US13580551
申请日：2011-02-09
申请人： Paul Fletcher , Andrew C Graham , Daniel Robertson , Anthony J Donaldson
发明人： Paul Fletcher , Andrew C Graham , Daniel Robertson , Anthony J Donaldson
IPC分类号： F02C7/26 , F01K23/10 , F02C3/30 , F01K13/02
CPC分类号： F01K3/22 , F01K23/10 , Y02E20/16
摘要： A method of starting a gas turbine cycle including a gas turbine and a heat recovery steam generator, the method including: heating water in a steam cycle with a base load heat source; powering one or more steam turbines with steam from said steam cycle; and diverting a portion of the steam from the steam cycle to the gas turbine cycle. Also disclosed is a power generation assembly connectable to a base load heat source arranged to heat water in a steam cycle and power a steam turbine, the power generation assembly including: a gas turbine cycle including a gas turbine and a heat recovery steam generator; and diverting apparatus configured to selectively divert a portion of steam from the steam cycle to the gas turbine cycle on start up of the gas turbine.
摘要翻译：一种起动包括燃气轮机和热回收蒸汽发生器的燃气轮机循环的方法，所述方法包括：用基本负荷热源加热蒸汽循环中的水; 为来自所述蒸汽循环的蒸汽供电一个或多个蒸汽轮机; 并将一部分蒸汽从蒸汽循环转移到燃气轮机循环。还公开了一种可连接到基座负载热源的发电组件，其布置成在蒸汽循环中加热水并为蒸汽涡轮机供电，所述发电组件包括：燃气轮机循环，包括燃气轮机和热回收蒸汽发生器; 以及转向装置，其构造成在燃气轮机启动时选择性地将一部分蒸汽从蒸汽循环转移到燃气轮机循环。

6. 发明申请

US20100034648A1 Method of assembling a multi-stage turbine or compressor 有权
标题翻译：组装多级涡轮或压缩机的方法
公开(公告)号：US20100034648A1
公开(公告)日：2010-02-11
申请号：US12457750
申请日：2009-06-19
申请人： Daniel Robertson
发明人： Daniel Robertson
IPC分类号： F02C3/06 , B23P11/00
CPC分类号： F01D25/28 , F01D5/06 , F01D5/3007 , F01D9/042 , F01D25/285 , F05D2230/60 , Y10T29/4932 , Y10T29/49321 , Y10T29/49323
摘要： A method is disclosed for assembling a multi-stage compressor or a multi-stage turbine for use in a gas-turbine engine. The method comprises the steps of assembling a rotor drum so as to comprise a plurality of rotor discs 17, 18, and then releasably connecting a plurality of static components 38 to the assembled rotor drum 19, thus forming an intermediate structure. The intermediate structure is then inserted within an outer casing 50, preferably by lowering the outer casing 50 over the intermediate structure, whereafter the static components 38 are fixed to the outer casing 50. The static components 38 are then released from their connection to the rotor drum 19 in order to permit rotation of the drum 19 relative to the static components 38 and the outer casing 50.
摘要翻译：公开了用于组装用于燃气涡轮发动机的多级压缩机或多级涡轮机的方法。该方法包括以下步骤：组装转子鼓以包括多个转子盘17,18，然后将多个静态部件38可释放地连接到组装的转子鼓19上，从而形成中间结构。然后将中间结构插入外壳50中，优选地通过将外壳50降低到中间结构上方，然后将静态部件38固定到外壳50.静电部件38然后从与转子鼓19以允许滚筒19相对于静态部件38和外壳50旋转。

7. 发明申请

US20060239251A1 Multi-user media client for communication devices 审中-公开
标题翻译：用于通信设备的多用户媒体客户端
公开(公告)号：US20060239251A1
公开(公告)日：2006-10-26
申请号：US11370151
申请日：2006-03-07
申请人： Jesse Bennett , William Osborn , Daniel Robertson
发明人： Jesse Bennett , William Osborn , Daniel Robertson
IPC分类号： H04L12/66
CPC分类号： H04L65/103 , H04L29/06027 , H04L65/1006 , H04L65/104 , H04L65/1069
摘要： A SIP client for a communication device includes a user agent to communicate with a user application in the communication device. The user agent provides a high-level application interface to the user application and translates user commands into corresponding signaling and media operations. The same user agent may be shared by a plurality of user applications. A signaling agent controlled by the user agent performs signaling operations necessary to establish and maintain communication sessions. To avoid signaling overhead on a high cost network, the SIP client can be located in a remote network so signaling messages do not need to traverse the high cost network.
摘要翻译：用于通信设备的SIP客户端包括用于与通信设备中的用户应用通信的用户代理。用户代理向用户应用提供高级应用接口，并将用户命令转换为相应的信令和媒体操作。相同的用户代理可以由多个用户应用共享。由用户代理控制的信令代理执行建立和维护通信会话所需的信令操作。为了避免高成本网络上的信令开销，SIP客户端可以位于远程网络中，因此信令消息不需要遍历高成本网络。

8. 发明申请

US20050081410A1 System and method for distributed reporting of machine performance 有权
标题翻译：分布式报告机器性能的系统和方法
公开(公告)号：US20050081410A1
公开(公告)日：2005-04-21
申请号：US10920104
申请日：2004-08-17
申请人： Ken Furem , Daniel Robertson , Gopal Madhavarao
发明人： Ken Furem , Daniel Robertson , Gopal Madhavarao
IPC分类号： E02F9/26 , E02F5/02 , E02D17/06 , E02D17/13 , E02F5/10 , G06F15/16 , H04B7/00
CPC分类号： E02F9/267
摘要： Certain exemplary embodiments can comprise obtaining and analyzing data from at least one discrete machine, automatically determining relationships related to the data, taking corrective action to improve machine operation and/or maintenance, automatically and heuristically predicting a failure associated with the machine and/or recommending preventative maintenance in advance of the failure, and/or automating and analyzing mining shovels, etc.
摘要翻译：某些示例性实施例可以包括获得和分析来自至少一个离散机器的数据，自动确定与数据相关的关系，采取纠正措施来改进机器操作和/或维护，自动和启发式地预测与机器相关联的故障和/或推荐故障之前的预防性维护，和/或挖掘挖掘机的自动化分析等。

9. 发明授权

US09386731B2 Magnetic shield 有权
标题翻译：磁屏蔽
公开(公告)号：US09386731B2
公开(公告)日：2016-07-05
申请号：US13816223
申请日：2011-07-14
申请人： Daniel Robertson , Kunal Bhargava , Fady Mishriki , Saining Sunny Ren
发明人： Daniel Robertson , Kunal Bhargava , Fady Mishriki , Saining Sunny Ren
IPC分类号： H01F27/00 , H05K9/00 , H02J17/00
CPC分类号： H01F38/14 , H01F27/289 , H01F27/365 , H01F2027/348 , H02J17/00 , H02J50/10 , H02J50/40 , H02J50/70 , H05K9/00 , H05K9/0075
摘要： A magnetic shield for shielding adjacent coils of an ICPT system. One or more conductors are configured to distribute induced eddy currents from the surface of the shield to below the surface and thus reduce heating due to eddy currents.The magnetic shield may be employed to transfer power over rotary couplings, such as the shaft of a wind turbine.
摘要翻译：用于屏蔽ICPT系统的相邻线圈的磁屏蔽。一个或多个导体被配置为将感应涡流从屏蔽表面分布到表面下方，从而减少由涡流引起的加热。磁屏蔽可用于通过诸如风力涡轮机的轴的旋转联接器传递动力。

10. 发明申请

US20140232330A1 WIRELESSLY RECHARGEABLE BATTERY AND POWER TRANSMITTER 有权
标题翻译：无线充电电池和发电机
公开(公告)号：US20140232330A1
公开(公告)日：2014-08-21
申请号：US13885805
申请日：2011-11-16
申请人： Daniel Robertson , Kunal Bhargava , Thushari Gomes
发明人： Daniel Robertson , Kunal Bhargava , Thushari Gomes
IPC分类号： H02J7/02 , H01M10/46 , H01F38/14
CPC分类号： H02J7/025 , H01F38/14 , H01M2/1022 , H01M10/425 , H01M10/46 , H02J5/005 , H02J7/0042 , H02J50/10 , H02J50/12 , H02J50/40 , H02J50/60 , H02J50/80 , H02J50/90
摘要： A wirelessly rechargeable battery is provided having coils oriented off major battery axes to facilitate good coupling with power transmitter magnetic fields. A magnetic core may house charging electronics for a compact form factor. A wireless power transmitter that produces fields to maximize coupling with receiver coils.
摘要翻译：提供了一种无线充电电池，其具有取决于主电池轴线的线圈，以便于与功率发射器磁场的良好耦合。磁芯可以容纳紧凑形状的充电电子元件。无线电力发射器，产生场以最大程度地与接收器线圈耦合。

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