Battery charger and method of charging a battery
    3.
    发明授权
    Battery charger and method of charging a battery 失效
    电池充电器和充电方法

    公开(公告)号:US06963186B2

    公开(公告)日:2005-11-08

    申请号:US10603879

    申请日:2003-06-24

    Applicant: Raymond Hobbs

    Inventor: Raymond Hobbs

    Abstract: Stationary and on-board battery chargers, methods of charging batteries, electric-vehicle chargers, and vehicles with chargers, including electric vehicles and hybrid electric vehicles. Chargers may automatically charge at the correct battery voltage for various types of batteries. Chargers have variable AC power supplies controlled by digital controllers, isolation transformers, and rectifiers. Transformers may be foil-type, and may have copper foil. Power supplies may be variable-frequency generators and the controllers may control the frequency. Electric vehicle chargers may have card readers, and vehicles may have batteries and a charger. Methods of charging include identifying the battery type and gradually increasing the charging at different rates of increase while monitoring charging voltage, charging current, or both, until a current lid is reached. Charging may occur at constant current and then at constant voltage.

    Abstract translation: 固定和车载电池充电器,电池充电方法,电动车充电器以及充电器车辆,包括电动汽车和混合电动汽车。 充电器可能会以正确的电池电压为各种类型的电池充电。 充电器具有由数字控制器,隔离变压器和整流器控制的可变交流电源。 变压器可以是箔型,并且可以具有铜箔。 电源可以是可变频率发生器,并且控制器可以控制频率。 电动汽车充电器可能有读卡器,车辆可能有电池和充电器。 充电方法包括识别电池类型,并以不同的增加速率逐渐增加充电,同时监测充电电压,充电电流或两者,直到达到当前的盖子。 充电可能发生在恒定电流,然后在恒定电压。

    Battery charger and method of charging a battery
    5.
    发明授权
    Battery charger and method of charging a battery 失效
    电池充电器和充电方法

    公开(公告)号:US07411371B2

    公开(公告)日:2008-08-12

    申请号:US11162107

    申请日:2005-08-29

    Applicant: Raymond Hobbs

    Inventor: Raymond Hobbs

    Abstract: Stationary and on-board battery chargers, methods of charging batteries, electric-vehicle chargers, and vehicles with chargers, including electric vehicles and hybrid electric vehicles. Chargers may automatically charge at the correct battery voltage for various types of batteries. Chargers have variable AC power supplies controlled by digital controllers, isolation transformers, and rectifiers. Transformers may be foil-type, and may have copper foil. Power supplies may be variable-frequency generators and the controllers may control the frequency. Use of the variable frequency generator supply facilitates reduced component size and weight and better battery charging performance. Electric vehicle chargers may have card readers, and vehicles may have batteries and a charger. Methods of charging include identifying the battery type and gradually increasing the charging at different rates of increase while monitoring charging voltage, charging current, or both, until a current lid is reached. Charging may occur at constant current and then at constant voltage.

    Abstract translation: 固定和车载电池充电器,电池充电方法,电动车充电器以及充电器车辆,包括电动汽车和混合电动汽车。 充电器可能会以正确的电池电压为各种类型的电池充电。 充电器具有由数字控制器,隔离变压器和整流器控制的可变交流电源。 变压器可以是箔型,并且可以具有铜箔。 电源可以是可变频率发生器,并且控制器可以控制频率。 使用可变频率发生器电源有助于减少组件尺寸和重量以及更好的电池充电性能。 电动汽车充电器可能有读卡器,车辆可能有电池和充电器。 充电方法包括识别电池类型,并以不同的增加速率逐渐增加充电,同时监测充电电压,充电电流或两者,直到达到当前的盖子。 充电可能发生在恒定电流,然后在恒定电压。

    Method of supporting a solar energy collection unit
    6.
    发明申请
    Method of supporting a solar energy collection unit 审中-公开
    支撑太阳能收集单元的方法

    公开(公告)号:US20070199560A1

    公开(公告)日:2007-08-30

    申请号:US11361771

    申请日:2006-02-24

    Abstract: A method (92) of supporting a solar energy collection unit (22, 54, 76) of a solar energy system (20, 52, 78) calls for redistributing (96) earth at a worksite (26) to form an elevated earthen structure (24) having a sun facing surface (28), compacting (102) the earthen structure (24), and arranging (106) the solar energy collection unit (22, 54, 76) upon the sun facing surface (28) of the earthen structure (24). The earthen structure (24) may include internal strengthening material (32) detached from the energy collection unit (22, 54, 76) and the earthen structure (24) may be encased in a binder material (34) for additional stability. Channels (48, 50) may be provided proximate the earthen structure (24) for fluid supply and release functions.

    Abstract translation: 支撑太阳能系统(20,52,78)的太阳能收集单元(22,54,76)的方法(92)要求在工地(26)处重新分配(96)地球以形成升高的土层结构 (24),具有朝阳表面(28),压实(102)所述土体结构(24),并且将所述太阳能收集单元(22,54,76)布置(106)到所述太阳能收集单元(28)的所述朝阳表面(28)上 土结构(24)。 土层结构(24)可以包括从能量收集单元(22,54,76)分离的内部加强材料(32),并且土层结构(24)可以被包裹在粘合剂材料(34)中以用于额外的稳定性。 通道(48,50)可以设置在土体结构(24)附近,用于流体供应和释放功能。

    SPECIALLY TINTED LENSES FOR SUNGLASSES FOR USE DURING FLYING
    9.
    发明申请
    SPECIALLY TINTED LENSES FOR SUNGLASSES FOR USE DURING FLYING 有权
    特殊用途的镜片,用于飞行时使用的太阳镜

    公开(公告)号:US20070285613A1

    公开(公告)日:2007-12-13

    申请号:US11421355

    申请日:2006-05-31

    Applicant: Raymond Hobbs

    Inventor: Raymond Hobbs

    CPC classification number: G02C7/102 G02C7/104 G02C7/105 G02C7/12 G02C7/16

    Abstract: The present invention is directed toward specially tinted lenses for use in flying airplanes. In the present invention, the far field of vision is highly tinted to reduce the light from a sunlit sky, over sunlit cloud tops, or in clouds. This enables an aircraft pilot to easily see out of the cockpit into highly illuminated environments. The intermediate field of vision is essentially clear to enable the pilot to easily see a dimly illuminated instrument panel as compared to outside the aircraft. The near field of vision may have a range of tinting from clear to up to a medium tinted value for reading maps and other material. In addition, the change in tinting is discontinuous, that is, sharp, from one field of vision to another. The present invention works because the aircraft structure, that is, the nose and instrument panel, blocks outside light from coming into the intermediate field of vision where the lens is clear.

    Abstract translation: 本发明涉及用于飞行飞机的特殊着色透镜。 在本发明中,远视野是高度着色的,以减少来自阳光照射的天空,阳光照射的云顶或云中的光。 这使飞机驾驶员能够轻松地从驾驶舱中看到高度照明的环境。 中间视野基本上是清晰的,以使飞行员能够轻松地看到与飞机外部相比较暗的照明仪表板。 近视野可能具有从清晰到高达中等有色值的范围,用于阅读地图和其他材料。 此外,着色的变化是不连续的,也就是说,从一个视野到另一个视野。 本发明的作用是因为飞机结构,即鼻子和仪表板,阻止外部光线进入透镜清晰的中间视野。

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