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    • 1. 发明授权
    • Operational ground support system
    • 操作地面支援系统
    • US07275715B2
    • 2007-10-02
    • US10711610
    • 2004-09-28
    • William R. McCoskeyRichard N. JohnsonW. James Renton
    • William R. McCoskeyRichard N. JohnsonW. James Renton
    • B64C9/00
    • B64F1/36B64C25/405B64F1/305B64F1/31Y02T50/82Y02T50/823
    • An integrated operational ground mobility and support system (10) that includes an aircraft (12) having one or more service openings on a side of the aircraft (12). The integrated support system (10) may have an airport interface terminal docking port (14) that has a ground support service sub-system. The docking port (14) mates with the aircraft (12) at the service openings and has multiple service levels. The ground support service sub-system provides services to the aircraft (12) through the service openings and on the service levels. The integrated support system (10) may have in addition to or in replacement of the interface terminal docking port an aircraft loader/unloader. The loader/unloader has ground support service sub-systems and mates with the aircraft (12) at one or more of the service openings. The service sub-systems of the loader/unloader include a passenger ingress/egress system (62) and provide services to the aircraft (12).
    • 一种综合的操作地面机动和支援系统(10),包括在飞机(12)一侧具有一个或多个服务开口的飞机(12)。 集成支撑系统(10)可以具有具有地面支撑服务子系统的机场接口终端对接端口(14)。 对接端口(14)在服务口处与飞机(12)配合,并具有多个服务级别。 地面支援服务子系统通过服务开放和服务水平向飞机(12)提供服务。 集成支持系统(10)可以具有除了接口终端对接端口或替代飞行器装载机/卸载机的附加或替代。 装载机/卸载机具有地面支持服务子系统,并且在一个或多个服务开口处与飞机(12)配合。 装载机/卸载机的服务子系统包括乘客入口/出口系统(62)并向飞行器(12)提供服务。
    • 6. 发明授权
    • Powered nose aircraft wheel system
    • 电动鼻飞机轮系统
    • US07445178B2
    • 2008-11-04
    • US11160191
    • 2005-06-13
    • William R. McCoskeyRichard N. JohnsonMatthew J. Berden
    • William R. McCoskeyRichard N. JohnsonMatthew J. Berden
    • B64C25/50
    • B64C25/42B64C25/405B64C25/50B64F1/002B64F1/22B64F1/28B64F1/32Y02T50/823Y02T50/826
    • A powered nose aircraft wheel system (130) for an aircraft (12) includes landing gear (104) that extends from the aircraft (12). A wheel axel (136) is coupled to the landing gear (104). A wheel (134) is coupled to the wheel axel (136). A wheel motor (106) is coupled to the wheel axel (136) and the wheel (134). A controller (120) is coupled to the wheel motor (106) and rotates the wheel (134). A method of taxiing an aircraft (12) includes permitting the wheel (134) of the aircraft (12) to freely spin during the landing of the aircraft (12). Power is transferred from an auxiliary power unit (73) of the aircraft (12) to the wheel motor (106). The wheel (134) is rotated via the wheel motor (106). The aircraft (12) is steered and the speed of the wheel (134) is controlled via one or more controllers selected from an onboard controller (18, 118, 120) and an offboard controller (45, 58, 59).
    • 用于飞行器(12)的动力鼻飞机轮系统(130)包括从飞行器(12)延伸的起落架(104)。 轮轴(136)联接到起落架(104)。 轮(134)联接到轮轴(136)。 车轮电机(106)联接到车轮轴(136)和车轮(134)。 控制器(120)联接到车轮马达(106)并使车轮(134)旋转。 飞行器(12)的滑行方法包括允许飞机(12)的轮(134)在飞行器(12)的着陆期间自由旋转。 动力从飞行器(12)的辅助动力单元(73)传递到轮马达(106)。 轮(134)经由车轮马达(106)旋转。 飞行器(12)被转向,并且通过从车载控制器(18,118,120)和外侧控制器(45,58,59)中选择的一个或多个控制器控制车轮(134)的速度。
    • 7. 发明申请
    • AIRCRAFT KINETIC LANDING ENERGY CONVERSION SYSTEM
    • 航空运输能量转换系统
    • US20080258014A1
    • 2008-10-23
    • US12106135
    • 2008-04-18
    • William R. McCoskeyMichael M. Vander WelRichard N. Johnson
    • William R. McCoskeyMichael M. Vander WelRichard N. Johnson
    • B64C25/42E01C11/00B64C13/00
    • B64C25/42B60L7/10B60L11/182B60L2200/26B64C25/36B64C25/405Y02T10/7005Y02T10/7072Y02T50/823Y02T90/122Y02T90/14
    • A kinetic energy system which transfers the kinetic landing into recoverable electric energy for an aircraft. The system incorporates at least one wheel supporting the aircraft for landing and takeoff coupled with a dynamic functioning motor/generator mounted to and operated by rotation of the wheel to create electrical energy from kinetic energy. An induction shoe structurally connected to the aircraft and electrically connected to the motor/generator, which shoe draws the converted energy from the generator which supplies the load created by the inductively coupled induction shoe to the an ancillary load provided by the resistive heat sink on by the capacitor storage bank. This provides the generator circuit for conversion of the rotational energy of the wheel to electrical energy and creates braking drag. In exemplary embodiments, the system employs an energy storage system acting as the load to store electrical potential energy created by the generator. Additionally, the generator is employable as a motor, receiving energy from the storage system for traction power to the associated aircraft wheel. An induction grid or a surface mounted conductive layer mounted into or onto a runway is employed for transferring energy to and from the motor/generator.
    • 将动能着陆转变为飞机可恢复电能的动能系统。 该系统包括至少一个支撑飞机的轮子,用于着陆和起飞,其与通过轮的旋转安装到其上并由动能产生电能的动态功能马达/发电机相结合。 一种结构上连接到飞行器并与电动机/发电机电连接的感应瓦,该滑靴将来自发电机的转换的能量从电感耦合感应靴产生的负载拉到由电阻散热器所提供的辅助负载上 电容器存储库。 这提供了用于将车轮的旋转能量转换为电能并且产生制动阻力的发电机电路。 在示例性实施例中,系统采用充当负载的能量存储系统来存储由发电机产生的电势。 此外,发电机可用作电动机,从存储系统接收能量以用于牵引力到相关的飞行器轮。 安装在跑道中或导轨上的感应电网或表面安装的导电层用于将电能传送到电动机/发电机。
    • 8. 发明授权
    • Aircraft kinetic landing energy conversion system
    • 飞机动能降落能量转换系统
    • US08123163B2
    • 2012-02-28
    • US12106135
    • 2008-04-18
    • William R. McCoskeyMichael M. Vander WelRichard N. Johnson
    • William R. McCoskeyMichael M. Vander WelRichard N. Johnson
    • B64C25/42
    • B64C25/42B60L7/10B60L11/182B60L2200/26B64C25/36B64C25/405Y02T10/7005Y02T10/7072Y02T50/823Y02T90/122Y02T90/14
    • A kinetic energy system which transfers the kinetic landing into recoverable electric energy for an aircraft. The system incorporates at least one wheel supporting the aircraft for landing and takeoff coupled with a dynamic functioning motor/generator mounted to and operated by rotation of the wheel to create electrical energy from kinetic energy. An induction shoe structurally connected to the aircraft and electrically connected to the motor/generator, which shoe draws the converted energy from the generator which supplies the load created by the inductively coupled induction shoe to the an ancillary load provided by the resistive heat sink on by the capacitor storage bank. This provides the generator circuit for conversion of the rotational energy of the wheel to electrical energy and creates braking drag. In exemplary embodiments, the system employs an energy storage system acting as the load to store electrical potential energy created by the generator. Additionally, the generator is employable as a motor, receiving energy from the storage system for traction power to the associated aircraft wheel. An induction grid or a surface mounted conductive layer mounted into or onto a runway is employed for transferring energy to and from the motor/generator.
    • 将动能着陆转变为飞机可恢复电能的动能系统。 该系统包括至少一个支撑飞机的轮子,用于着陆和起飞,其与通过轮的旋转安装到其上并由动能产生电能的动态功能马达/发电机相结合。 一种结构上连接到飞行器并与电动机/发电机电连接的感应瓦,该滑靴将来自发电机的转换的能量从电感耦合感应靴产生的负载拉到由电阻散热器所提供的辅助负载上 电容器存储库。 这提供了用于将车轮的旋转能量转换为电能并且产生制动阻力的发电机电路。 在示例性实施例中,系统采用充当负载的能量存储系统来存储由发电机产生的电势。 此外,发电机可用作电动机,从存储系统接收能量以用于牵引力到相关的飞行器轮。 安装在跑道中或导轨上的感应电网或表面安装的导电层用于将电能传送到电动机/发电机。
    • 10. 发明授权
    • Multi-purpose aircraft servicing bridge
    • 多功能飞机维修桥梁
    • US06863243B2
    • 2005-03-08
    • US10242179
    • 2002-09-12
    • Kazuhide KonyaWilliam R. McCoskey
    • Kazuhide KonyaWilliam R. McCoskey
    • B64F1/305B64F1/32B64D9/00
    • B64F1/305
    • A multi-purpose aircraft servicing system (10) for an aircraft (12) is provided. The system (10) includes a multi-servicing bridge 16 having a main bridge section (26) with a plurality of bridge servicing units (56). A bridgehead (28) is mechanically coupled to the main bridge section (26) and mates to the aircraft (12). A method of servicing the aircraft (12) is also provided including parking the aircraft (12) at a terminal (24). The multi-purpose aircraft servicing system (10) is rotated to mate with the aircraft (12). The aircraft (12) is serviced from at least one side of the aircraft (12).
    • 提供了一种用于飞机(12)的多功能飞机维修系统(10)。 系统(10)包括具有主桥部分(26)和多个桥梁维修单元(56)的多维护桥梁16。 桥头(28)机械地联接到主桥段(26)并与飞机(12)配合。 还提供维修飞行器(12)的方法,包括将飞行器(12)停放在终端(24)处。 多用途飞机维修系统(10)旋转以与飞机(12)配合。 飞机(12)从飞机(12)的至少一侧提供服务。