OIL SUPPLY IN RENEWABLE ENERGY TURBINE GENERATOR
    22.
    发明申请
    OIL SUPPLY IN RENEWABLE ENERGY TURBINE GENERATOR 审中-公开
    可再生能源涡轮发电机的供油

    公开(公告)号:US20130049371A1

    公开(公告)日:2013-02-28

    申请号:US13390897

    申请日:2011-08-30

    Abstract: A renewable energy turbine generator (1), such as a wind turbine generator, comprises a hydraulic pump (20), a hydraulic motor (24) and an oil circuit (26, 28) connecting the hydraulic pump and the hydraulic motor. Oil in the low pressure side (28) of the oil circuit is cooled and supplied to the working chambers (95) of the hydraulic pump. A reduced temperature oil feed provides additionally cooled oil to the bearings of the hydraulic pump and the hydraulic motor. Thus, cooler and more viscous oil is supplied to the bearings (84) of the hydraulic pump and/or hydraulic motor and warmer and less viscous oil is supplied to the working chambers, increasing the efficiency and lifetime of the bearings and of the working portions of the hydraulic pump and motor.

    Abstract translation: 诸如风力涡轮发电机的可再生能量涡轮发电机(1)包括连接液压泵和液压马达的液压泵(20),液压马达(24)和油路(26,28)。 油路的低压侧(28)中的油被冷却并供给到液压泵的工作室(95)。 降温油进料为液压泵和液压马达的轴承提供另外冷却的油。 因此,冷却器和更粘稠的油被供应到液压泵和/或液压马达的轴承(84),并且较暖和较低粘度的油被供应到工作室,从而提高轴承和工作部分的效率和使用寿命 的液压泵和电机。

    Inertia Valve Vehicle Suspension Assembly
    25.
    发明申请
    Inertia Valve Vehicle Suspension Assembly 审中-公开
    惯性阀门悬架组件

    公开(公告)号:US20080007017A1

    公开(公告)日:2008-01-10

    申请号:US11852735

    申请日:2007-09-10

    Applicant: Robert Fox

    Inventor: Robert Fox

    Abstract: A damper including an inertia valve movable between an open position and a closed position to selectively alter the compression damping rate of the shock absorber is disclosed. In these embodiments, the damper has at least one chamber that at least partially surrounds two other chambers.

    Abstract translation: 公开了一种阻尼器,其包括可在打开位置和关闭位置之间运动的惯性阀,以选择性地改变减震器的压缩阻尼率。 在这些实施例中,阻尼器具有至少部分地围绕两个其它腔室的至少一个腔室。

    Bicycle Suspension Assembly With Inertia Valve and External Controller
    26.
    发明申请
    Bicycle Suspension Assembly With Inertia Valve and External Controller 审中-公开
    具有惯性阀和外部控制器的自行车悬架组件

    公开(公告)号:US20070262555A1

    公开(公告)日:2007-11-15

    申请号:US11741074

    申请日:2007-04-27

    Applicant: Robert Fox

    Inventor: Robert Fox

    Abstract: A bicycle suspension assembly is first provided with an inertia valve for selectively altering the compression damping rate of the shock absorber. The bicycle suspension assembly is also provided with at least one adjustable fluid damping circuit through which fluid may flow during operation of the suspension assembly. The fluid flow resistance through the adjustable fluid damping circuit may be adjusted without requiring any disassembly of the bicycle suspension assembly by using a movable external controller.

    Abstract translation: 首先设置有自行车悬架组件,其具有用于选择性地改变减震器的压缩阻尼率的惯性阀。 自行车悬架组件还设置有至少一个可调节的流体阻尼回路,流体可在悬架组件的操作期间流过。 通过可调节流体阻尼回路的流体阻力可以通过使用可移动的外部控制器而不需要拆卸自行车悬架组件进行调整。

    METHOD FOR MAKING AN ENERGETIC MATERIAL
    27.
    发明申请
    METHOD FOR MAKING AN ENERGETIC MATERIAL 失效
    制造能量材料的方法

    公开(公告)号:US20070232840A1

    公开(公告)日:2007-10-04

    申请号:US11231142

    申请日:2005-09-19

    Applicant: Robert Fox

    Inventor: Robert Fox

    CPC classification number: C07C201/08 Y02P20/544 C07C205/06

    Abstract: A method for making an energetic material is described, and which includes the steps of providing a source of aqueous nitric acid having a concentration of less than about 95% by weight; mixing a surfactant with the source of the aqueous nitric acid so as to dehydrate the aqueous nitric acid to produce a source of nitronium ions; providing a carbon dioxide environment; providing a source of an organic material to be nitrated to the carbon dioxide environment; and controllably mixing the source of nitronium ions with the carbon dioxide environment to nitrate the organic material and produce a resulting energetic material.

    Abstract translation: 描述了制备高能材料的方法,其包括以下步骤:提供浓度小于约95重量%的硝酸水溶液源; 将表面活性剂与硝酸水溶液混合,以使硝酸水溶液脱水以产生硝鎓离子源; 提供二氧化碳环境; 提供要对二氧化碳环境进行硝化的有机材料的来源; 并可控制地将硝酸根源与二氧化碳环境混合以使有机材料硝酸化并产生所得的能量材料。

    Quick coupler hitch operated with single handle
    28.
    发明申请
    Quick coupler hitch operated with single handle 审中-公开
    快速连接器搭接单手柄操作

    公开(公告)号:US20070169951A1

    公开(公告)日:2007-07-26

    申请号:US11337885

    申请日:2006-01-23

    CPC classification number: B60D1/141 A01B59/062 B60D1/04

    Abstract: A quick coupler hitch has a one piece curved tube frame, rearwardly projecting upwardly opening hooks on each leg of the frame, each hook having a latch pivotable between an unlocked position and a locked position. A central pivot mechanism is mounted on the curved tube frame and has a shaft with a generally vertical axis. Flexible links extend through the curved tube frame between the central pivot mechanism and each of the latches. The central pivot mechanism is manually pivotable about the generally vertical axis of the shaft to retract or extend the flexible links to lock or unlock the latches.

    Abstract translation: 快速联接器挂钩具有单件弯曲管架,向后突出在框架的每个腿上的向上打开的钩,每个钩具有可在解锁位置和锁定位置之间枢转的闩锁。 中心枢轴机构安装在弯曲的管架上,并具有大致垂直轴线的轴。 柔性连杆通过中心枢轴机构和每个闩锁之间的弯曲管架延伸。 中心枢转机构可以围绕轴的大致垂直轴线手动地枢转,以缩回或延伸柔性连杆以锁定或解锁闩锁。

    Self-Contained Avionics Sensing And Flight Control System For Small Unmanned Aerial Vehicle
    29.
    发明申请
    Self-Contained Avionics Sensing And Flight Control System For Small Unmanned Aerial Vehicle 有权
    用于小型无人机的自包含航空电子传感和飞行控制系统

    公开(公告)号:US20070069083A1

    公开(公告)日:2007-03-29

    申请号:US11422984

    申请日:2006-06-08

    CPC classification number: G05D1/101

    Abstract: A self-contained avionics sensing and flight control system is provided for an unmanned aerial vehicle (UAV). The system includes sensors for sensing flight control parameters and surveillance parameters, and a Global Positioning System (GPS) receiver. Flight control parameters and location signals are processed to generate flight control signals. A Field Programmable Gate Array (FPGA) is configured to provide a look-up table storing sets of values with each set being associated with a servo mechanism mounted on the UAV and with each value in each set indicating a unique duty cycle for the servo mechanism associated therewith. Each value in each set is further indexed to a bit position indicative of a unique percentage of a maximum duty cycle for the servo mechanism associated therewith. The FPGA is further configured to provide a plurality of pulse width modulation (PWM) generators coupled to the look-up table. Each PWM generator is associated with and adapted to be coupled to one of the servo mechanisms.

    Abstract translation: 为无人机(UAV)提供独立的航空电子感测和飞行控制系统。 该系统包括用于感测飞行控制参数和监视参数的传感器,以及全球定位系统(GPS)接收器。 飞行控制参数和位置信号被处理以产生飞行控制信号。 现场可编程门阵列(FPGA)被配置为提供存储各组值的查找表,其中每组与安装在UAV上的伺服机构相关联,并且每组中的每个值表示伺服机构的唯一占空比 相关联。 每组中的每个值进一步被索引到指示与其相关联的伺服机构的最大占空比的唯一百分比的位位置。 FPGA还被配置为提供耦合到查找表的多个脉宽调制(PWM)发生器。 每个PWM发生器与伺服机构中的一个相关联并且适于耦合到其中一个伺服机构。

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