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    • 1. 发明授权
    • Yaw control system and method
    • 偏航控制系统及方法
    • US07644887B2
    • 2010-01-12
    • US11678044
    • 2007-02-22
    • Edward D. JohnsonHoward C. Kress, Jr.
    • Edward D. JohnsonHoward C. Kress, Jr.
    • B64C27/10B64C27/615
    • B64C27/10B64C27/72B64C2027/7266Y02T50/34
    • A yaw control system and a method of controlling yaw for an aircraft are provided. The yaw control system includes a first wing set and a second wing set which are rotatable in opposite directions. Each of the wing sets includes at least two wings each including a pivotable flap forming a trailing edge of its respective wing. A flap control assembly controls the pivotable flaps of the first wing set and of the second wing set such that when the pivotable flaps of the first wing set are pivoted in a first direction by a first set angle, the pivotable flaps of the second wing set are simultaneously pivoted by a second set angle in an opposite direction, thereby providing yaw control for the aircraft.
    • 提供了一种用于飞行器的偏航控制系统和控制偏航的方法。 偏航控制系统包括可沿相反方向旋转的第一机翼组和第二机翼组。 每个翼组包括至少两个翼,每个翼包括形成其相应翼的后缘的可枢转翼。 翼片控制组件控制第一翼组和第二翼组的可枢转翼片,使得当第一翼组的可枢转翼片沿第一方向枢转第一设定角时,第二翼组的可枢转翼片 同时以相反方向枢转第二设定角度,从而为飞行器提供偏航控制。
    • 2. 发明申请
    • Yaw Control System and Method
    • 偏航控制系统和方法
    • US20080203222A1
    • 2008-08-28
    • US11678044
    • 2007-02-22
    • Edward D. JohnsonHoward C. Kress
    • Edward D. JohnsonHoward C. Kress
    • B64C3/38B64C13/00
    • B64C27/10B64C27/72B64C2027/7266Y02T50/34
    • A yaw control system and a method of controlling yaw for an aircraft are provided. The yaw control system includes a first wing set and a second wing set which are rotatable in opposite directions. Each of the wing sets includes at least two wings each including a pivotable flap forming a trailing edge of its respective wing. A flap control assembly controls the pivotable flaps of the first wing set and of the second wing set such that when the pivotable flaps of the first wing set are pivoted in a first direction by a first set angle, the pivotable flaps of the second wing set are simultaneously pivoted by a second set angle in an opposite direction, thereby providing yaw control for the aircraft.
    • 提供了一种用于飞行器的偏航控制系统和控制偏航的方法。 偏航控制系统包括可沿相反方向旋转的第一机翼组和第二机翼组。 每个翼组包括至少两个翼,每个翼包括形成其相应翼的后缘的可枢转翼。 翼片控制组件控制第一翼组和第二翼组的可枢转翼片,使得当第一翼组的可枢转翼片沿第一方向枢转第一设定角时,第二翼组的可枢转翼片 同时以相反方向枢转第二设定角度,从而为飞行器提供偏航控制。
    • 3. 发明授权
    • Modular circuit breaker housing assembly
    • 模块化断路器外壳组件
    • US06444931B1
    • 2002-09-03
    • US09702780
    • 2000-10-31
    • David A. BartekMarcus L. MelaneEdward D. Johnson
    • David A. BartekMarcus L. MelaneEdward D. Johnson
    • H02B126
    • H01H71/0271H02B1/056
    • A customizable, modular circuit breaker housing assembly having an optimized compact form factor for use with electrical and telecommunications equipment. The housing assembly is comprised of an interlocked arrangement of individual housing portions coupled at one end to an end housing portion, and to an end panel portion at an opposite end. The end housing portion and individual housing portions include a load bus chamber and a line bus chamber for receiving load and line bus members, and one or more alarm contact member receptacles for receiving at least one alarm contact member. The line bus member and the alarm contact members may be provided as individually segmented members. In other embodiments, the individual housing portions may include pass-through slots for inserting a common line bus bar, pass-through apertures for common contact members, or both. The line and load bus members are formed of extruded metallic members having substantially the same cross-sectional surface. Mounting devices are provided on the end housing and individual housing portions for coupling the modular circuit breaker assembly to a mounting panel of the equipment.
    • 一种可定制的模块化断路器外壳组件,其具有用于电气和电信设备的优化的紧凑外形。 壳体组件包括一端连接到端部壳体部分的单独壳体部分和相对端部的端部板部分的联锁装置。 端部壳体部分和单个壳体部分包括用于接收负载和线路总线构件的负载总线室和线路总线室,以及用于接收至少一个报警接触构件的一个或多个报警接触构件容器。 线路总线构件和报警接触构件可以被设置为单独的分段构件。 在其他实施例中,各个壳体部分可以包括用于插入公共线母线的通孔,用于公共接触构件的通孔或两者。 线路和负载总线构件由具有基本相同横截面的挤压金属构件形成。 安装装置设置在端部壳体和单独的壳体部分上,用于将模块化断路器组件耦合到设备的安装面板。
    • 4. 发明授权
    • Battery temperature stabilization system and method
    • 电池温度稳定系统及方法
    • US06407533B1
    • 2002-06-18
    • US09703073
    • 2000-10-31
    • David A. BartekMarcus L. MelaneEdward D. Johnson
    • David A. BartekMarcus L. MelaneEdward D. Johnson
    • H02J704
    • H05K7/20618H01M10/613H01M10/615H01M10/627H01M10/6562H01M10/6565H01M10/6566
    • A system and method for the stabilization of battery temperature by alternating airflow through an internal ductwork of a cabinet housing electronic equipment and circuitry. Ambient air is drawn through one or more intake vents or louvers provided with the cabinet housing. Regulated airflow through the ductwork allows the cabinet housing's thermal management system to direct either cooler ambient air during warm periods or heated air during colder periods through the cabinet to stabilize the battery temperature as well electronics equipment and circuitry housed in the cabinet. At least a portion of the heated air is expelled through one or more exhaust vents. Because no active components are used for stabilizing battery temperature, thermal regulation is achieved even during utility power outages. Further, thermal energy is provided without the possibility of igniting hydrogen gas products generated by the battery units present in the cabinet.
    • 通过交换气流通过容纳电子设备和电路的机柜的内部管道系统来稳定电池温度的系统和方法。 环境空气通过设置有机柜外壳的一个或多个进气口或百叶窗抽吸。 通过管道系统调节的气流允许机柜外壳的热管理系统通过机柜在温暖期间或更冷的时段内将冷却的环境空气引导到室内,以稳定电池温度以及容纳在机柜中的电子设备和电路。 至少一部分加热的空气通过一个或多个排气口排出。 由于没有活性组分用于稳定电池温度,因此即使在公用电源中断期间也实现了热调节。 此外,提供热能,而不会点燃存在于柜中的电池单元产生的氢气产物。
    • 7. 发明授权
    • Apparatus for protecting multiple output rectifiers in a current-fed
DC-to DC converter
    • 用于保护电流馈电DC-DC转换器中多路输出整流器的装置
    • US5673186A
    • 1997-09-30
    • US673010
    • 1996-07-01
    • Edward D. Johnson
    • Edward D. Johnson
    • H02H7/12H02M3/337H02M7/06H02H7/125
    • H02M7/062H02H7/1213H02M3/3372
    • A current-fed DC-to-DC converter (10) includes an input choke (20) which reduces current fluctuation in the converter (10). A power transformer (26), which is coupled to the input choke (20), transforms electrical energy at one voltage magnitude into electrical energy at another voltage magnitude. A first output rectifier (32) is coupled to the input choke (20). A second output rectifier (34, 36) is coupled to the power transformer (26). A first isolation diode (38) and a second isolation diode (40, 42) are coupled to the anodes of the first output rectifier (32) and the second output rectifier (34, 36), respectively. A transient voltage suppression element (12) is coupled to the first isolation diode (38) and the second isolation diode (40, 42). The transient voltage suppression element (12) limits the magnitude of voltage transients created by the input choke (20) and the power transformer (26) during operation of the converter (10), thereby preventing damage to the first and second output rectifiers (32, 34, 36).
    • 电流馈送DC-DC转换器(10)包括减小转换器(10)中的电流波动的输入扼流圈(20)。 耦合到输入扼流器(20)的电力变压器(26)将处于一个电压幅度的电能转换成另一个电压幅度的电能。 第一输出整流器(32)耦合到输入扼流圈(20)。 第二输出整流器(34,36)耦合到电力变压器(26)。 第一隔离二极管(38)和第二隔离二极管(40,42)分别耦合到第一输出整流器(32)和第二输出整流器(34,36)的阳极。 瞬态电压抑制元件(12)耦合到第一隔离二极管(38)和第二隔离二极管(40,42)。 瞬变电压抑制元件(12)限制在转换器(10)操作期间由输入扼流圈(20)和电源变压器(26)产生的电压瞬变的幅值,从而防止对第一和第二输出整流器(32)的损坏 ,34,36)。