-
公开(公告)号：US08485466B2
公开(公告)日：2013-07-16
申请号：US12915746
申请日：2010-10-29
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , Y02T10/7258 , Y02T50/823
摘要： A electric taxi system (ETS) for an aircraft may comprise drive units mounted coaxially with wheels of the aircraft and dedicated motor control units for the drive units. The motor control units may be operable independently of one another so that a first one of the drive units can be operated at a speed different from an operating speed of a second one of the drive units. Independent operability of the drive units may provide enhanced maneuverability of the aircraft during taxiing.
摘要翻译： 用于飞机的电动滑行系统（ETS）可以包括与飞行器的车轮同轴安装的驱动单元和用于驱动单元的专用马达控制单元。 电机控制单元可以彼此独立地操作，使得驱动单元中的第一个可以以与第二驱动单元的操作速度不同的速度操作。 驱动单元的独立可操作性可以在滑行期间提供飞机的增强的机动性。
-
2.发明申请BUTTERFLY VALVE ASSEMBLY INCLUDING A BEARING ASSEMBLY FOR SERRATED SPLINE CONSTRAINT 有权蝶阀组件，包括用于压缩线束约束的轴承组件公开(公告)号：US20100270489A1
公开(公告)日：2010-10-28
申请号：US12429819
申请日：2009-04-24
申请人： Anthony Mendoza , Mike Kolic , Doug Smith , Ben Ho , Louie Timothy Gaines
发明人： Anthony Mendoza , Mike Kolic , Doug Smith , Ben Ho , Louie Timothy Gaines
IPC分类号： F16K1/22
CPC分类号： B64D13/02 , F16C19/06 , F16C19/54 , F16C25/083 , F16C41/02 , F16K1/224 , F16K27/0218
摘要： Butterfly valves assemblies are provided that include a flowbody, a butterfly plate, an actuator and an upper chimney and a lower chimney disposed within the flowbody. The flowbody has an inner surface defining a channel. The butterfly plate is disposed in the channel, is rotationally mounted to the flowbody, and has an outer periphery. The actuator has an actuator output shaft that is coupled to the valve shaft via a serrated spline coupling. The upper chimney and the lower chimney are configured to include bearing assemblies that constrain radial loads and thrust loads exerted upon the valve shaft and minimize misalignment of the serrated spline coupling.
摘要翻译： 提供了蝶阀组件，其包括流体，蝶板，致动器和上烟囱以及设置在流体内的下烟囱。 流体体具有限定通道的内表面。 蝶板设置在通道中，旋转地安装在流体上，并具有外周。 致动器具有致动器输出轴，该致动器输出轴通过锯齿形花键联接件联接到阀轴。 上烟囱和下烟囱构造成包括轴承组件，其限制施加在阀轴上的径向载荷和推力载荷，并使锯齿形花键联轴器的未对准最小化。
-
公开(公告)号：US20120104158A1
公开(公告)日：2012-05-03
申请号：US12915746
申请日：2010-10-29
IPC分类号： B64C25/00
CPC分类号： B64C25/405 , Y02T10/7258 , Y02T50/823
摘要： A electric taxi system (ETS) for an aircraft may comprise drive units mounted coaxially with wheels of the aircraft and dedicated motor control units for the drive units. The motor control units may be operable independently of one another so that a first one of the drive units can be operated at a speed different from an operating speed of a second one of the drive units. Independent operability of the drive units may provide enhanced maneuverability of the aircraft during taxiing.
摘要翻译： 用于飞机的电动滑行系统（ETS）可以包括与飞行器的车轮同轴安装的驱动单元和用于驱动单元的专用马达控制单元。 电机控制单元可以彼此独立地操作，使得驱动单元中的第一个可以以与第二驱动单元的操作速度不同的速度操作。 驱动单元的独立可操作性可以在滑行期间提供飞机的增强的机动性。
-
公开(公告)号：US08528856B2
公开(公告)日：2013-09-10
申请号：US12959717
申请日：2010-12-03
IPC分类号： B64C25/42
CPC分类号： B64C25/405 , Y02T50/823
摘要： A electric taxi system (ETS) for an aircraft may comprise drive units mounted coaxially with wheels of the aircraft and dedicated motor control units for the drive units. The motor control units may be operable independently of one another so that a first one of the drive units can be operated at a speed different from an operating speed of a second one of the drive units. Independent operability of the drive units may provide enhanced maneuverability of the aircraft during taxiing.
-
公开(公告)号：US20120104159A1
公开(公告)日：2012-05-03
申请号：US12959717
申请日：2010-12-03
CPC分类号： B64C25/405 , Y02T50/823
摘要： A electric taxi system (ETS) for an aircraft may comprise drive units mounted coaxially with wheels of the aircraft and dedicated motor control units for the drive units. The motor control units may be operable independently of one another so that a first one of the drive units can be operated at a speed different from an operating speed of a second one of the drive units. Independent operability of the drive units may provide enhanced maneuverability of the aircraft during taxiing.
-
公开(公告)号：US20100013226A1
公开(公告)日：2010-01-21
申请号：US12349868
申请日：2009-01-07
CPC分类号： F03D1/00 , B64B1/50 , B64C31/06 , B64C2201/148 , F03D5/00 , F03D7/0204 , F05B2240/921 , Y02E10/28 , Y02E10/70 , Y02E10/723 , Y10S416/06 , Y10T74/19
摘要： A wind turbine energy conversion device that can take advantage of the higher speed and more persistent winds at higher altitudes is hereinafter disclosed. The wind turbine energy conversion device includes an unmanned aerial vehicle (UAV) connected to one end of a tether (which may include multiple shorter tethers), the other end being connected to a terrestrial anchorage point. The UAV flies at altitudes where wind speeds can reach 40 mph or higher. The UAV comprises a flying wing with one or more trailing wind power turbines and flies airborne maneuvers designed to increase relative wind speed up to about four times the true wind speed.
摘要翻译： 以下公开了能够在更高海拔地区利用更高速度和更持久的风的风力涡轮机能量转换装置。 风力涡轮机能量转换装置包括连接到系绳一端的无人驾驶飞行器（UAV），其可以包括多个较短的系绳，另一端连接到陆地锚固点。 无人机在高度达到40英里/小时以上的高空飞行。 无人机包括具有一个或多个尾随风力涡轮机的飞翼，并且飞行空中机动设计，以将相对风速增加到真实风速的大约四倍。
-
公开(公告)号：US08201334B2
公开(公告)日：2012-06-19
申请号：US12411260
申请日：2009-03-25
IPC分类号： F16C43/06
CPC分类号： F16C43/06 , F16C19/26 , F16C2240/40 , F16C2240/84 , Y10T29/49643 , Y10T29/4968 , Y10T29/49686 , Y10T29/49696 , Y10T29/49865
摘要： A roller bearing assembly includes an annular outer ring with first and second outer ring shoulders that define a first raceway in the outer ring. An annular inner ring may be disposed substantially concentrically within the outer ring, the inner ring including a base portion and first and second inner ring shoulders that extend from and are integral with the base portion to define a second raceway in the inner ring. A plurality of rolling elements may be arranged between the inner ring and outer ring and within the first and second raceways to rotatably couple the outer ring to the inner ring.
摘要翻译： 滚子轴承组件包括环形外圈，其具有在外圈中限定第一滚道的第一和第二外圈肩部。 环形内圈可以基本上同心地设置在外圈内，内圈包括基座部分和从底座部分延伸并与之一体的第一和第二内圈肩部，以在内圈中限定第二滚道。 多个滚动元件可以布置在内圈和外圈之间并且在第一和第二滚道内，以将外圈可旋转地连接到内圈。
-
公开(公告)号：US20100247018A1
公开(公告)日：2010-09-30
申请号：US12411260
申请日：2009-03-25
CPC分类号： F16C43/06 , F16C19/26 , F16C2240/40 , F16C2240/84 , Y10T29/49643 , Y10T29/4968 , Y10T29/49686 , Y10T29/49696 , Y10T29/49865
摘要： A roller bearing assembly includes an annular outer ring with first and second outer ring shoulders that define a first raceway in the outer ring. An annular inner ring may be disposed substantially concentrically within the outer ring, the inner ring including a base portion and first and second inner ring shoulders that extend from and are integral with the base portion to define a second raceway in the inner ring. A plurality of rolling elements may be arranged between the inner ring and outer ring and within the first and second raceways to rotatably couple the outer ring to the inner ring.
摘要翻译： 滚子轴承组件包括环形外圈，其具有在外圈中限定第一滚道的第一和第二外圈肩部。 环形内圈可以基本上同心地设置在外圈内，内圈包括基座部分和从底座部分延伸并与之一体的第一和第二内圈肩部，以在内圈中限定第二滚道。 多个滚动元件可以布置在内圈和外圈之间并且在第一和第二滚道内，以将外圈可旋转地连接到内圈。
-
9.发明授权Butterfly valve assembly including a bearing assembly for serrated spline constraint 有权蝶阀组件包括用于锯齿样条约束的轴承组件公开(公告)号：US08172202B2
公开(公告)日：2012-05-08
申请号：US12429819
申请日：2009-04-24
申请人： Anthony Mendoza , Mike Kolic , Doug Smith , Ben Ho , Louie Timothy Gaines
发明人： Anthony Mendoza , Mike Kolic , Doug Smith , Ben Ho , Louie Timothy Gaines
IPC分类号： F16K1/22
CPC分类号： B64D13/02 , F16C19/06 , F16C19/54 , F16C25/083 , F16C41/02 , F16K1/224 , F16K27/0218
摘要： Butterfly valves assemblies are provided that include a flowbody, a butterfly plate, an actuator and an upper chimney and a lower chimney disposed within the flowbody. The flowbody has an inner surface defining a channel. The butterfly plate is disposed in the channel, is rotationally mounted to the flowbody, and has an outer periphery. The actuator has an actuator output shaft that is coupled to the valve shaft via a serrated spline coupling. The upper chimney and the lower chimney are configured to include bearing assemblies that constrain radial loads and thrust loads exerted upon the valve shaft and minimize misalignment of the serrated spline coupling.
摘要翻译： 提供了蝶阀组件，其包括流体，蝶板，致动器和上烟囱以及设置在流体内的下烟囱。 流体体具有限定通道的内表面。 蝶板设置在通道中，旋转地安装在流体上，并具有外周。 致动器具有致动器输出轴，该致动器输出轴通过锯齿形花键联接件联接到阀轴。 上烟囱和下烟囱构造成包括轴承组件，其限制施加在阀轴上的径向载荷和推力载荷，并使锯齿形花键联轴器的未对准最小化。
-
公开(公告)号：US08109711B2
公开(公告)日：2012-02-07
申请号：US12349868
申请日：2009-01-07
IPC分类号： F03B15/06 , F03B13/00 , F03B7/00 , F03B17/06 , F03D7/00 , F03D11/04 , F03D9/00 , F01D25/28 , F01D15/00 , F01D15/12 , F04D29/60 , B63H1/38
CPC分类号： F03D1/00 , B64B1/50 , B64C31/06 , B64C2201/148 , F03D5/00 , F03D7/0204 , F05B2240/921 , Y02E10/28 , Y02E10/70 , Y02E10/723 , Y10S416/06 , Y10T74/19
摘要： A wind turbine energy conversion device that can take advantage of the higher speed and more persistent winds at higher altitudes is hereinafter disclosed. The wind turbine energy conversion device includes an unmanned aerial vehicle (UAV) connected to one end of a tether (which may include multiple shorter tethers), the other end being connected to a terrestrial anchorage point. The UAV flies at altitudes where wind speeds can reach 40 mph or higher. The UAV comprises a flying wing with one or more trailing wind power turbines and flies airborne maneuvers designed to increase relative wind speed up to about four times the true wind speed.
摘要翻译： 以下公开了能够在更高海拔地区利用更高速度和更持久的风的风力涡轮机能量转换装置。 风力涡轮机能量转换装置包括连接到系绳一端的无人驾驶飞行器（UAV），其可以包括多个较短的系绳，另一端连接到陆地锚固点。 无人机在高度达到40英里/小时以上的高空飞行。 无人机包括具有一个或多个尾随风力涡轮机的飞翼，并且飞行空中机动设计，以将相对风速增加到真实风速的大约四倍。
-
-
-
-
-
-
-
-
-
搜索结果
10 条记录 (耗时 0.011 秒)
