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1.发明授权Marine propulsion-and-control system implementing articulated variable-pitch propellers 有权实现铰接式可变螺距螺旋桨的船舶推进和控制系统公开(公告)号：US09022738B1
公开(公告)日：2015-05-05
申请号：US13336348
申请日：2011-12-23
申请人： Eric J. Silberg , Daniel Everson , David J. Haas
发明人： Eric J. Silberg , Daniel Everson , David J. Haas
摘要： According to typical inventive practice, a cylindrical or prolate spheroidal marine hull has two congruent contra-rotative propellers coaxially situated at or near its axial ends. Each propeller has plural blades mechanically and/or flexibly attributed with changeability of blade pitch angles and blade flap angles. A blade-pitch control system adjusts the individual blade pitch angles of both propellers. The blade-pitch control system may be electronically and/or mechanically actuated, and is capable of: (i) cyclically adjusting the blade pitch angles of the two propellers so as to select two respective blade-tip-path planes, each characterized by a direction of thrust that is associated with the blade flap angles and is generally perpendicular to the blade-tip-path plane; (ii) collectively adjusting the blade pitch angles of the two propellers so as to select two respective magnitudes of thrust. The cyclic and collective blade commands, algorithmically coordinated, determine the direction, orientation, and speed of the hull.
摘要翻译： 根据典型的发明实践，圆柱形或长圆形球形海洋船体具有同轴位于其轴向端或其附近的两个全等的反旋转螺旋桨。 每个螺旋桨具有机械和/或柔性归因于叶片桨距角和叶片翼角度的可变性的多个叶片。 叶片桨距控制系统调节两个螺旋桨的单个桨叶桨距角。 叶片桨距控制系统可以是电子和/或机械致动的，并且能够：（i）循环地调节两个螺旋桨的叶片桨距角，以便选择两个相应的叶片尖端路径平面，每个叶片尖端路径平面的特征在于 与叶片翼片角度相关联的推力方向并且大致垂直于叶片尖端路径平面; （ii）共同调整两个螺旋桨的叶片俯仰角，以便选择两个相应的推力大小。 循环和集体叶片命令，算法协调，确定船体的方向，方向和速度。
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公开(公告)号：US07797130B1
公开(公告)日：2010-09-14
申请号：US12006754
申请日：2007-12-20
IPC分类号： G06F17/18
摘要： According to typical inventive practice, a baseline describing a statistical distribution is established for a set of historical occurrences of an event. Comparison is made between the baseline and at least one current occurrence of the same event. Any current occurrence that is anomalous vis-à-vis the baseline is considered a possible leading indicator. According to some inventive embodiments of graphical presentation of such comparison, at least one graphical baseline comparative display component is rendered that includes a “bar” (describing a historical statistical distribution with respect to a criterion pertaining to occurrence of an event) and a “slider” (describing one or more current occurrences of the event). The bar includes at least one band representing a statistical mean range, and at least one band representing a statistical outlier range. Situation of the slider along the bar indicates whether and to what extent the current occurrence(s) is/are anomalous vis-à-vis the baseline.
摘要翻译： 根据典型的创造性实践，建立描述统计分布的基线用于一组事件的历史事件。 在相同事件的基线和至少一个当前事件之间进行比较。 任何与基线相反的当前事件被认为是可能的主要指标。 根据这种比较的图形呈现的一些创造性实施例，呈现至少一个图形基线比较显示组件，其包括“bar”（描述关于与事件发生有关的标准的历史统计分布）和“滑块 “（描述事件的一个或多个当前事件）。 该条包括表示统计平均范围的至少一个带和表示统计异常值范围的至少一个带。 滑块沿着条形的情况表明当前的发生是否以及在多大程度上与基线相反。
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公开(公告)号：US08204637B1
公开(公告)日：2012-06-19
申请号：US12497875
申请日：2009-07-06
CPC分类号： G06Q30/0201 , G06Q30/0202
摘要： A method has been found for assessing an aircraft approach to landing on a shipboard landing surface. The method includes a comparison of an identified aircraft performance with the mean or median of a baseline data set. The baseline data set is assembled from a multiplicity of actual approaches to landing data that are selected for relevance and then statistically evaluated. A high data recording rate captures the pilot's control inputs and allows evaluation of the pilot's manual efficiency of input to controls. The method is particularly useful to evaluate performance under conditions in which evaluation by human observation is limited or evaluation against guidelines produces less meaningful results.
摘要翻译： 已经发现一种评估飞机降落在船上着陆表面上的方法。 该方法包括将所识别的飞机性能与基线数据集的平均值或中值进行比较。 基线数据集从多个实际方法组合到着陆数据，登陆数据被选择用于相关性，然后进行统计学评估。 高数据记录速率捕获飞行员的控制输入，并允许评估飞行员手动输入控制效率。 该方法对于在人类观察评估有限的条件下评估表现特别有用，或者对指南进行评估产生较少有意义的结果。
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公开(公告)号：US08094154B1
公开(公告)日：2012-01-10
申请号：US12006753
申请日：2007-12-20
IPC分类号： G06T11/20
CPC分类号： G01C23/00
摘要： According to typical inventive practice, a baseline describing a statistical distribution is established for a set of historical occurrences of an event. Comparison is made between the baseline and at least one current occurrence of the same event. Any current occurrence that is anomalous vis-à-vis the baseline is considered a possible leading indicator. According to some inventive embodiments of graphical presentation of such comparison, at least one graphical baseline comparative display component is rendered that includes a “bar” (describing a historical statistical distribution with respect to a criterion pertaining to occurrence of an event) and a “slider” (describing one or more current occurrences of the event). The bar includes at least one band representing a statistical mean range, and at least one band representing a statistical outlier range. Situation of the slider along the bar indicates whether and to what extent the current occurrence(s) is/are anomalous vis-à-vis the baseline.
摘要翻译： 根据典型的创造性实践，建立描述统计分布的基线用于一组事件的历史事件。 在相同事件的基线和至少一个当前事件之间进行比较。 任何与基线相反的当前事件被认为是可能的主要指标。 根据这种比较的图形呈现的一些创造性实施例，呈现至少一个图形基线比较显示组件，其包括“bar”（描述关于与事件发生有关的标准的历史统计分布）和“滑块 “（描述事件的一个或多个当前事件）。 该条包括表示统计平均范围的至少一个带和表示统计异常值范围的至少一个带。 滑块沿着条形的情况表明当前的发生是否以及在多大程度上与基线相反。
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5.发明授权Battery charging arrangement for unmanned aerial vehicle utilizing the electromagnetic field associated with utility power lines to generate power to inductively charge energy supplies 有权利用与公用电力线相关联的电磁场的无人驾驶飞行器的电池充电装置产生电力以感应地充电能量供应公开(公告)号：US07714536B1
公开(公告)日：2010-05-11
申请号：US11789128
申请日：2007-04-05
申请人： Eric J. Silberg , Judah H. Milgram
发明人： Eric J. Silberg , Judah H. Milgram
IPC分类号： H02J7/00
CPC分类号： B64C39/024 , B60L11/002 , B60L11/1801 , B60L11/182 , B60L2200/10 , B60L2200/20 , B60L2260/32 , B64C2201/042 , B64C2201/063 , Y02T10/7005 , Y02T10/7072 , Y02T90/122 , Y02T90/14
摘要： A method and apparatus for charging energy supplies in an unmanned aerial vehicle (UAV). The present invention relates to a UAV that comprises an inductive charging device that utilizes the electromagnetic field emanated by overhead/utility power lines, to charge the energy supplies. The UAV also includes a releasable latch for holding power lines to allow for the perching of the UAV on power lines during the charging process. The latch and the inductive charging device may be provided on a single device, a battery augmentation trap (BAT). The UAV may be perched in an upright orientation to allow for takeoff after the charging of energy supplies on the power line.
摘要翻译： 一种在无人机（UAV）中为能量供给充电的方法和装置。 本发明涉及一种UAV，其包括利用由架空/公用电力线发出的电磁场来对能量供应充电的感应充电装置。 无人机还包括可释放的闩锁，用于保持电力线以允许充电过程中的电力线上的UAV的栖息。 闩锁和感应充电装置可以设置在单个装置，电池增压阱（BAT）上。 无人机可以处于垂直方向，以允许在电力线上的能量供应充电之后起飞。
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