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公开(公告)号：US09308986B2
公开(公告)日：2016-04-12
申请号：US14385506
申请日：2013-02-14
发明人： Katsuya Kanaoka
CPC分类号： B64C15/12 , B63B2035/008 , B63H25/04 , B63H25/46 , B63H2025/465 , B64C39/024 , B64C2201/027 , B64C2201/10 , B64C2201/146 , G05D1/10 , G05D1/102
摘要： A holonomic floating mobile object is operated under gravity and includes a main body and six or more thrusters for generating thrust by changing the momentum of a fluid. The six or more thrusters are controlled independently of one another such that the thrust is set at a desired value. The six or more thrusters are arranged in a fuselage coordinate system defined on the main body, such that the range in which a total thrust vector obtained by combining vectors of the thrust generated by all of the thrusters can be generated spans a six-dimensional space with three directions of translation and three directions of rotation. Incoming and outgoing flows to and from one of the thrusters are spaced apart from incoming and outgoing flows to and from the other thrusters and even apart from every other fuselage structure aside from that one thruster.
摘要翻译： 完整的浮动移动物体在重力作用下运行，包括主体和六个或更多个用于通过改变流体动量产生推力的推进器。 六个或更多个推进器彼此独立地控制，使得推力被设定在期望的值。 六个或更多个推进器被布置在限定在主体上的机身坐标系中，使得可以产生通过组合由所有推进器产生的推力的矢量而获得的总推力向量的范围跨越六维空间 具有三个方向的翻译和三个方向的旋转。 来往于其中一个推进器的进出流量与进入和离开其它推进器的进出流量间隔开，甚至除了一个推进器之外的每个其他机身结构。
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公开(公告)号：US09290257B2
公开(公告)日：2016-03-22
申请号：US14187812
申请日：2014-02-24
申请人： Robert A. Morvillo
发明人： Robert A. Morvillo
CPC分类号： B63H25/46 , B63H11/11 , B63H11/113 , B63H21/213 , B63H25/02 , B63H2011/008 , B63H2025/026
摘要： A system for controlling a marine vessel having first and second steering nozzles and corresponding first and second reversing buckets, comprises a processor configured to receive a first vessel control signal including at least a component corresponding to a translational thrust command in a port direction, and that is configured to provide a set of actuator control signals coupled to and control the first and second reversing buckets. The processor is configured to provide the set of actuator control signals so as to maintain the first reversing bucket substantially in a first discrete position and the second reversing bucket substantially in a second discrete position as long as the first vessel control signal includes a component corresponding to a translational thrust command in the port direction.
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23.发明授权Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets 有权通过喷嘴引导通过具有多个出口的喷嘴产生脉冲喷射公开(公告)号：US09108711B2
公开(公告)日：2015-08-18
申请号：US12726826
申请日：2010-03-18
申请人： Paul S. Krueger
发明人： Paul S. Krueger
摘要： A method of producing a pulsatile jet flow from a substantially constant flow primary jet in a way that is mechanically efficient, easy to implement, and allows direct control over pulse duration and pulsing frequency is disclosed herein. The invention includes at least two components: (a) a constant flow fluid jet produced by any normal method (e.g., propeller) that can be directionally vectored fluidically, mechanically, or electromagnetically and (b) a nozzle with multiple outlets (orifices) through which the vectored jet may be directed. By alternately vectoring the jet through different outlets, a transient (pulsatile) flow at an outlet is obtained even with a substantially constant primary jet flow. Additionally, the nozzle outlets may be oriented in different directions to provide thrust vectoring, making the invention useful for maneuvering, directional control, etc.
摘要翻译： 本文公开了以机械效率，易于实施并且允许对脉冲持续时间和脉冲频率的直接控制的方式从基本上恒定的流量初级射流产生脉冲喷射流的方法。 本发明包括至少两个部件：（a）通过任何常规方法（例如，螺旋桨）产生的恒定流动流体射流，其可以流体地，机械地或电磁地定向定向，以及（b）具有多个出口（孔口）通过的喷嘴 向导可以被引导。 通过交替地通过不同的出口引导射流，即使以基本上恒定的一次喷射流也可以获得出口处的瞬态（脉动）流动。 此外，喷嘴出口可以沿不同方向定向以提供推力矢量化，使得本发明可用于操纵，方向控制等。
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公开(公告)号：US08793973B2
公开(公告)日：2014-08-05
申请号：US13320984
申请日：2010-05-18
申请人： Guy Bernard Vauchel
发明人： Guy Bernard Vauchel
CPC分类号： F02K1/72 , F02K1/763 , F05D2270/66 , Y02T50/671
摘要： The invention relates to a thrust reverser (1) for the nacelle of a dual-flow turbine engine, in which the bypass means (4) and the actuation jacks (22) of the sliding cowling (2) and of the reverse flaps (20) are arranged in two substantially parallel planes arranged above one another in the radial direction of the nacelle. The invention also relates to a nacelle for a dual-flow turbine engine that comprises such a thrust reverser.
摘要翻译： 本发明涉及一种用于双流涡轮发动机的机舱的推力反向器（1），其中所述旁通装置（4）和所述滑动罩（2）和所述反向翼片（20）的致动插座（22） ）布置在沿机舱的径向相互布置的两个基本上平行的平面中。 本发明还涉及一种用于双流涡轮发动机的机舱，其包括这种推力反向器。
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公开(公告)号：US08578716B2
公开(公告)日：2013-11-12
申请号：US12871024
申请日：2010-08-30
申请人： Gary A. Schirtzinger
发明人： Gary A. Schirtzinger
CPC分类号： F02K1/386 , F02C9/18 , F02K3/075 , F05D2250/71 , F05D2260/60 , F16K5/0407 , Y02T50/671 , Y10T137/0318
摘要： A valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary airflow into the primary gas flow path and control airflow injected from a higher pressure plenum into a lower pressure flowpath.
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公开(公告)号：US08322127B2
公开(公告)日：2012-12-04
申请号：US11933537
申请日：2007-11-01
CPC分类号： F02K1/28 , F02K1/002 , F02K1/006 , F02K1/04 , Y10T29/494
摘要： A nozzle assembly for a turbine engine has a convergent portion for converging fluid flow from a turbine engine core. A divergent portion for diverging fluid flow from the turbine engine core is in fluid communication with the convergent portion. A conduit is in communication with a bypass fluid flow. The conduit has a thrust vectoring port located near the divergent portion.
摘要翻译： 用于涡轮发动机的喷嘴组件具有用于会聚来自涡轮发动机芯的流体流的收敛部分。 用于使来自涡轮发动机芯的流体流分散的扩散部分与收敛部分流体连通。 管道与旁路流体流动连通。 导管具有位于发散部分附近的推力矢量化端口。
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公开(公告)号：US08286416B2
公开(公告)日：2012-10-16
申请号：US12061021
申请日：2008-04-02
CPC分类号： F02K3/06 , F02K3/075 , F02K3/077 , F05D2250/71 , F05D2270/52 , F05D2270/56
摘要： A valve system intermediate a secondary flow path and a primary flow path to selectively communicate secondary airflow into the primary gas flow path and control airflow injected from a higher pressure plenum into a lower pressure flowpath.
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公开(公告)号：US07972187B2
公开(公告)日：2011-07-05
申请号：US12371412
申请日：2009-02-13
申请人： Robert A. Morvillo
发明人： Robert A. Morvillo
IPC分类号： B63H25/46
CPC分类号： G05G5/005 , B63H11/00 , B63H11/107 , B63H11/11 , B63H11/113 , B63H11/117 , B63H21/213 , B63H21/22 , B63H25/02 , B63H2011/008 , B63H2011/081 , B63H2025/026 , G05G9/047 , G05G2009/04744 , Y10T74/20201
摘要： A method for controlling a marine vessel having a first steering nozzle, a reversing deflector and at least one of a bow thruster and a second steering nozzle is disclosed. The method comprises any of the acts of inducing a net transverse thrust to the marine vessel in response to a transverse thrust component signal, without substantially inducing any forward-reverse thrust or rotational thrust to the marine vessel, or inducing a net forward-reverse thrust to the marine vessel in response to a forward-reverse thrust component signal without substantially inducing any transverse thrust or rotational thrust to the marine vessel, or inducing a net rotational thrust to the marine vessel in response to the rotational thrust component signal without substantially inducing any forward-reverse thrust or transverse thrust to the marine vessel.
摘要翻译： 公开了一种用于控制具有第一转向喷嘴，反转偏转器和船首推进器和第二转向喷嘴中的至少一个的船舶的方法。 该方法包括响应于横向推力分量信号而引起海洋船舶的净横向推力的任何行为，而基本上不引起任何向前/向后的推力或向海洋船舶转动的推力，或者引起净前向推力 响应于正向反向推力分量信号到海洋船舶，而不会基本上引起任何横向推力或旋转推力到海洋船舶，或响应于旋转推力分量信号而引起到海洋船舶的净旋转推力，而基本上不引起任何 前向推力或向海洋船舶的横向推力。
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公开(公告)号：US20110120364A1
公开(公告)日：2011-05-26
申请号：US12929395
申请日：2011-01-20
申请人： Peter A. Mueller
发明人： Peter A. Mueller
CPC分类号： B63H25/42 , B63B39/061 , B63H21/213
摘要： A method for controlling a watercraft with a steering wheel, a steering device and twin motors, the method includes: maneuvering the watercraft at a first speed using side thrusters, controllable pitch propellers, or side thrusters with a deflection device as the steering device, wherein, when the watercraft travels in reverse and the watercraft makes a turn at the first speed, the steering wheel and the watercraft turn in a same direction, and maneuvering the watercraft at a second speed higher than the first speed using the controllable pitch propellers as the steering device, wherein, when the watercraft makes a turn at the second speed, a constant speed is maintained for both of the twin motors.
摘要翻译： 一种用方向盘，转向装置和双电机控制船舶的方法，所述方法包括：使用侧推进器，可调俯仰螺旋桨或侧向推进器以第一速度操纵船舶，其中偏转装置作为转向装置，其中 当船只反向行驶，船只以第一速度转弯时，方向盘和船只转向相同的方向，并以第一速度高于第一速度的第二速度使用可调俯仰螺旋桨作为 转向装置，其中，当船舶以第二速度转弯时，对于两个双电动机都保持恒定的速度。
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公开(公告)号：US20110061579A1
公开(公告)日：2011-03-17
申请号：US12698601
申请日：2010-03-10
CPC分类号： B63B1/28 , B62D35/007 , B63B35/7926 , B63H1/26 , B63H25/38 , B64C3/48 , B64C5/06 , B64C5/10 , B64C9/02 , F01D5/147 , F01D5/148 , F04D29/323 , Y02E10/727 , Y02T10/82 , Y02T50/673
摘要： A dynamic or aerodynamic fin comprising at least two parallel arranged fin sections. At least one fin section comprises a rotational axis for installing the fin section by a rotation shaft. An end stop is provided for stopping the rotational movement of the fin section to define an extreme position. In the extreme position the fin sections provide a substantially cambered shape to the fin. The dynamic fin is improved in that it comprises a pair of coupling elements. A first fin section is coupled to a second adjacent fin section by a pair of a first and second coupling elements. The first coupling element is complementary to the second coupling element. The first coupling element is part of, preferably integral, with the first fin section and the second coupling element is part of, preferably integral, with the second fin section.
摘要翻译： 包括至少两个平行布置的翅片部分的动态或空气动力学翅片。 至少一个翅片部分包括用于通过旋转轴安装翅片部分的旋转轴线。 设置有用于停止翅片部分的旋转运动以限定极限位置的止挡件。 在极端位置，翅片部分为翅片提供了基本弧形的形状。 改进了动态翅片，其包括一对耦合元件。 第一翅片部分通过一对第一和第二联接元件联接到第二相邻翅片部分。 第一耦合元件与第二耦合元件互补。 第一联接元件是与第一翅片部分的一部分，优选地是一体的，并且第二联接元件是与第二翅片部分的一部分，优选地是一体的。
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