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    • 1. 发明申请
    • Hull having minimized wave-making characteristics
    • 船体具有最小的波浪形特征
    • US20050022713A1
    • 2005-02-03
    • US10718866
    • 2003-11-21
    • Zachary Reynolds
    • Zachary Reynolds
    • B63B1/12B63B1/18B63B1/00
    • B63B1/06B63B1/40B63B2001/066B63B2001/201Y02T70/125Y02T70/126
    • A hull form is presented and dimensioned where the design parameters consist principally of the breadth of the hull at the waterline, taken at specific equal intervals (stations) along the length of the waterline. The waterline reference is that at which the vessel is intended to float in the loaded condition. The waterline breadths describe the entrance or bow of the vessel. The closing run or stem of the vessel is not specifically delineated as a feature of the entrance or related to it. The invention defines two parts of the vessel, the entrance and the run, as discrete segments, each having its own properties and advantages. The entrance of the vessel is concerned with wave-making and the creating of a wave front that opposes vessel forward motion. The invention describes a method of optimizing the entrance of a vessel, and modifying the entrance of an existing vessel to minimize wave-making characteristics.
    • 船体形式被呈现并确定尺寸,其中设计参数主要由水线上的船体的宽度组成,沿着水线长度以特定相等的间隔(站)进行。 水线参考是船舶在负载状态下浮动的参考。 水线宽度描述了船只的入口或弓。 船只的关闭行程或阀杆没有特别描述为入口的特征或与其相关。 本发明将容器的两个部分,入口和运行定义为离散段,每个部分具有其各自的特性和优点。 船舶的入口涉及波浪制作和创建反对船只向前运动的波浪面。 本发明描述了一种优化容器入口的方法,并且修改现有容器的入口以最小化波浪形特征。
    • 3. 发明申请
    • Non-prismatic grooved shank fastener
    • 非棱柱形槽柄紧固件
    • US20070160442A1
    • 2007-07-12
    • US11651781
    • 2007-01-11
    • Zachary Reynolds
    • Zachary Reynolds
    • F16B15/08F16B15/00
    • F16B15/00F16B15/06
    • Non-prismatic shank fasteners, such as nails, for wood and similar soft materials have a plurality of longitudinal extending non-congruent sections having different geometries, different configurations, and varying diameters such that the shank has the widest nominal diameter arranged to span a joint between wood members being fastened. The shank has four circumferentially symmetrically disposed grooves and ridges having dimensions within pre-determined ranges such that the ridges have sufficient strength to withstand the forces imposed on the shank being driven into the parent material and to resist loads imposed upon them by the loads to the parent material. The grooves have a sufficiently wide jaw opening to allow elastically compressed parent material to enter the groove and provide support to the shank. The non-prismatic grooved shanks demonstrate significantly greater load handling capability than that possessed by other known types of fasteners.
    • 用于木材和类似软质材料的非棱柱柄紧固件(例如钉子)具有多个纵向延伸的非全等部分,其具有不同的几何形状,不同的构造和不同的直径,使得柄具有最宽的公称直径, 木件之间被固定。 柄具有四个周向对称设置的槽和脊,其尺寸在预定范围内,使得脊具有足够的强度以承受施加在柄被驱动到母材中的力,并且抵抗由负载施加在它们上的负载 母材。 凹槽具有足够宽的钳口,以允许弹性压缩的母体材料进入凹槽并向柄提供支撑。 非棱柱形沟槽柄显示出比其他已知类型的紧固件所具有的显着更大的载荷处理能力。
    • 6. 发明授权
    • Aircraft terrain warning systems and methods
    • 飞机地形预警系统和方法
    • US07570177B2
    • 2009-08-04
    • US11471401
    • 2006-06-19
    • Zachary ReynoldsRichard RidenourCyro StoneStacey Rowlan
    • Zachary ReynoldsRichard RidenourCyro StoneStacey Rowlan
    • G08G5/04
    • G08G5/045B64D45/04G08G5/0086
    • Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
    • 公开的方法和系统用于基于用于基于飞行中的飞行器的预计飞行路径来评估潜在地形威胁的地形避免概况来防止具有前视地形避免(FLTA)功能的飞机碰撞,以及清晰的地形轮廓以确定是否 地形威胁已被清除。 如果地形回避轮廓与地形冲突,则可能存在碰撞威胁,由此通知飞行员并执行地形回避机动。 在地形回避机动的过程中,清澈的地形轮廓沿与飞机当前高度或接近的地平线大致平行的方向延伸,以检查是否可以安全地返回到先前的飞行路径角度或以其他方式结束地形避免机动。 当清澈的地形不再与地形威胁冲突时,就会向飞行员发出地形清晰的指示。
    • 7. 发明申请
    • AIRCRAFT TERRAIN WARNING SYSTEMS AND METHODS
    • AIRCRAFT TERRAIN警告系统和方法
    • US20060097895A1
    • 2006-05-11
    • US10326544
    • 2002-12-20
    • Zachary ReynoldsRichard RidenourCyro StoneStacey Rowlan
    • Zachary ReynoldsRichard RidenourCyro StoneStacey Rowlan
    • G08G5/04
    • G08G5/045B64D45/04G08G5/0086
    • Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
    • 公开的方法和系统用于基于用于基于飞行中的飞行器的预计飞行路径来评估潜在地形威胁的地形避免概况来防止具有前视地形避免(FLTA)功能的飞机碰撞,以及清晰的地形轮廓以确定是否 地形威胁已被清除。 如果地形回避轮廓与地形冲突,则可能存在碰撞威胁,由此通知飞行员并执行地形回避机动。 在地形回避机动的过程中,清澈的地形轮廓沿与飞机当前高度或接近的地平线大致平行的方向延伸,以检查是否可以安全地返回到先前的飞行路径角度或以其他方式结束地形避免机动。 当清澈的地形不再与地形威胁冲突时,就会向飞行员发出地形清晰的指示。
    • 8. 发明申请
    • Enhanced girder system
    • 增强梁系统
    • US20050257336A1
    • 2005-11-24
    • US11131617
    • 2005-05-18
    • Zachary Reynolds
    • Zachary Reynolds
    • E01D1/00E01D6/00E01D22/00E04C3/02E04C3/04E04C3/06E04C3/11E04C3/18E04C3/29E04C3/292E04G23/02
    • E01D1/00E01D22/00E04C3/06E04C3/11E04C3/18E04C3/29E04C3/292E04C2003/0491E04G23/0218
    • An enhancing mechanism to be placed primarily below the neutral axis of a girder is presented. The movement and deflection of the girder causes the enhancing mechanism to alter the bending moment distribution of the girder. The mechanism is configured so that when combined with the girder, the overall dimensions of the combined system is not much bigger than the dimensions of the girder alone. A tension member may be incorporated into the lower boundary of the enhancing mechanism, and connections are used to attach the mechanism to the girder below the neutral axis. The girder and the enhancing mechanism may be made of the same material or different materials. The compression forces developed in the long diagonal members of the enhancing mechanism become a reaction at the girder end points. A direct connection of the long diagonal members to support points load shear directly to the end supports.
    • 提出了主要位于大梁中性轴线以下的增强机构。 大梁的运动和偏转导致增强机构改变梁的弯矩分布。 该机构被构造成使得当与大梁组合时,组合系统的总体尺寸不比单独的大梁的尺寸大得多。 张力构件可以被结合到增强机构的下边界中,并且连接被用于将机构附接到中性轴线之下的梁。 梁和增强机构可以由相同的材料或不同的材料制成。 在增强机构的长对角构件中产生的压缩力在梁端点成为反应。 长对角构件与支撑点的直接连接负载剪切直接到端部支撑。
    • 9. 发明申请
    • Threat avoidance system and methods using adjustments to built-in values
    • 威胁避免系统和方法使用内置值进行调整
    • US20070198143A1
    • 2007-08-23
    • US11706637
    • 2007-02-12
    • Kathryn YbarraZachary Reynolds
    • Kathryn YbarraZachary Reynolds
    • G01C23/00
    • G05D1/0607
    • A system for enhancing flight safety of a host aircraft receives an adjustment value from a portable memory device; determines a working value of a parameter in accordance with the adjustment value; and provides an advice for threat avoidance in accordance with the working value of the parameter, a terrain database, and an expected climb gradient capability of the host aircraft. The adjustment value may describe an adjustment to at least one of: an aircraft capability parameter, a flight crew capability parameter, a mission parameter, a threat detection technique parameter, a threat advice parameter, or a threat avoidance parameter. Threats include a risk of colliding with other aircraft, colliding with terrain, and encountering adverse weather conditions.
    • 用于增强主机的飞行安全性的系统从便携式存储装置接收调整值; 根据调整值确定参数的工作值; 并根据参数,地形数据库的工作价值和主机飞机的预期爬升梯度能力提供威胁避免的建议。 调整值可以描述对于飞机能力参数,飞行机组能力参数,任务参数,威胁检测技术参数,威胁建议参数或威胁避免参数中的至少一个的调整。 威胁包括与其他飞机相撞的风险,与地形相撞,遇到恶劣天气条件。