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1. 发明申请

US20140364265A1 CONTRA-ROTATING PROPULSOR FOR MARINE PROPULSION 有权
标题翻译：海上推进责任转让计划
公开(公告)号：US20140364265A1
公开(公告)日：2014-12-11
申请号：US14208762
申请日：2014-03-13
申请人： Michigan Marine Propulsion Systems, LLC
发明人： Bernard Bentgen , Brant Savander
IPC分类号： B63H23/06 , B63H23/30 , F16H1/46
CPC分类号： B63H11/00 , B63B2035/738 , B63H5/10 , B63H23/02 , B63H23/06 , B63H23/24 , B63H23/28 , B63H23/30 , B63H2005/106 , B63H2021/202 , B63H2023/0283 , B63H2023/062 , B63H2023/065 , B63H2023/067 , B63H2023/245 , Y02T70/5236 , Y02T70/56
摘要： A system for providing marine propulsion is provided including an input shaft driven by a prime mover, a pinion gear coupled to the input shaft, a plurality of planet gears coupled to the pinion gear, a planet carrier having the plurality of planet gears rotationally mounted thereto, and a ring gear surrounding the planet gears and coupled thereto. The planet carrier and ring gear are coupled to internal and external output shafts that are coaxially aligned, which are coupled to aft and forward propulsor elements. The ring gear and planet carrier rotate in opposite directions to provide contra-rotating forward and aft propulsor elements. The ring gear and planet gear are each coupled to rotation altering devices that, when at least one is activated, the rotation of both the planet carrier and ring gear will be altered, thereby altering the rotation of the propulsor elements.
摘要翻译：提供了一种用于提供船舶推进的系统，包括由原动机驱动的输入轴，联接到输入轴的小齿轮，联接到小齿轮的多个行星齿轮，具有旋转地安装到其上的多个行星齿轮的行星架以及围绕行星齿轮并与其联接的环形齿轮。行星架和环形齿轮联接到同轴对准的内部和外部输出轴，其连接到后部和向前的推进元件。环形齿轮和行星架沿相反方向旋转以提供反向旋转的向前和向后推进元件。环形齿轮和行星齿轮各自联接到旋转改变装置，当至少一个被激活时，行星架和环形齿轮的旋转将被改变，从而改变推进元件的旋转。

2. 发明授权

US08857191B2 Hybrid propulsive engine including at least one independently rotatable propeller/fan 有权
标题翻译：混合推进发动机包括至少一个独立旋转的螺旋桨/风扇
公开(公告)号：US08857191B2
公开(公告)日：2014-10-14
申请号：US12590043
申请日：2009-10-30
申请人： Roderick A. Hyde , Muriel Y. Ishikawa , Edward K. Y. Jung , Jordin T. Kare , Nathan P. Myhrvold , Clarence T. Tegreene , Thomas Allan Weaver , Lowell L. Wood, Jr. , Victoria Y. H. Wood
发明人： Roderick A. Hyde , Muriel Y. Ishikawa , Edward K. Y. Jung , Jordin T. Kare , Nathan P. Myhrvold , Clarence T. Tegreene , Thomas Allan Weaver , Lowell L. Wood, Jr. , Victoria Y. H. Wood
IPC分类号： F02C7/275
CPC分类号： F02C6/00 , F02C6/18 , F02K3/06 , F05D2220/31 , F05D2220/324 , F05D2220/325 , F05D2220/76 , H02K7/1823 , Y02T50/672 , Y02T70/56
摘要： A hybrid propulsive technique includes providing at least some first thrust associated with a flow of a working fluid through at least a portion of an at least one axial flow jet engine. The hybrid propulsive technique includes extracting energy from the working fluid that is at least partially converted into electrical power, and converting at least a portion of the electrical power to torque. The hybrid propulsive technique further includes rotating an at least one independently rotatable propeller/fan of at least one rotatable propeller/fan assembly at least partially responsive to the converting the at least a portion of the electrical power to torque, wherein the rotating of the at least one independently rotatable propeller/fan of the at least one rotatable propeller/fan assembly is arranged to produce at least some second thrust.
摘要翻译：混合推进技术包括通过至少一个轴流式喷气发动机的至少一部分提供与工作流体流相关联的至少一些第一推力。混合推进技术包括从至少部分地转换成电力的工作流体提取能量，以及将至少一部分电功率转换为转矩。混合推进技术还包括至少部分地响应于将至少一部分电功率转换为扭矩来旋转至少一个可旋转螺旋桨/风扇组件的至少一个独立旋转的螺旋桨/风扇，其中，所述至少一个可旋转螺旋桨/风扇组件的至少一个可独立旋转的螺旋桨/风扇布置成产生至少一些第二推力。

3. 发明授权

US08718842B2 Hydroplaning vessel with reactive suspension and integrated braking, steering system 有权
标题翻译：具有反作用悬挂和集成制动，转向系统的滑水装置
公开(公告)号：US08718842B2
公开(公告)日：2014-05-06
申请号：US13247806
申请日：2011-09-28
申请人： Fred Pereira
发明人： Fred Pereira
IPC分类号： B60L3/00 , B60L15/00 , G05D1/00 , G05D3/00 , G06F7/00 , G06F17/00
CPC分类号： B63B29/02 , B63B39/005 , B63B39/061 , B63H25/44 , Y02T70/56
摘要： A hydroplaning vessel with several stability and handling design improvements. It has an enhanced reactive suspension and inner hull lift system positioned in the vessel between a set of separating inner and outer hulls. The outer hull does not float on its own as it has numerous fixed louvers formed there through and also has an open transom. Steering and braking are accomplished by a set of rear elevon flaps affixed to the outer hull. The drive unit resides in the inner hull and is connected by an annular drive transmission which is connected to the jet or prop drive which resides on the outer hull.
摘要翻译：具有几种稳定性和处理设计改进的滑水船。它具有增强的反应性悬浮和内部船体提升系统，其位于容器内的一组分离的内外壳之间。外壳不会自己浮动，因为它有许多固定的百叶窗，在那里形成，也有一个开放的横梁。转向和制动通过一组固定在外壳上的后升降翼完成。驱动单元位于内部船体中，并通过环形驱动传动装置连接，该驱动传动装置连接到位于外部船体上的喷气式或悬挂式驱动装置。

4. 发明申请

US20080197212A1 Method and device to increase thrust and efficiency of jet engine 有权
标题翻译：提高喷气发动机的推力和效率的方法和装置
公开(公告)号：US20080197212A1
公开(公告)日：2008-08-21
申请号：US11890290
申请日：2007-08-03
申请人： Artem P. Efremkin , Pavel V. Efremkin
发明人： Artem P. Efremkin , Pavel V. Efremkin
IPC分类号： B63H11/103
CPC分类号： F02K1/28 , F02K3/02 , F05D2210/10 , Y02T70/56
摘要： A method and device for adding special substances to the gaseous outflow of the jet engine in order to create a “virtual wall” of increased pressure zone behind the jet engine nozzle which can serve as a support for the jet engine gas outflow to push against, thus increasing the thrust power of the jet engine. This increase in acceleration power results in the accelerated movement of the jet engine equipped vehicle or higher fuel efficiency. A device that adds the special substances to the gaseous outflow is proposed. Characteristics of the special substances, which if added into the jet engine gaseous outflow may create a “virtual wall” of increased pressure zone behind the jet engine, are proposed.
摘要翻译：一种用于向喷气发动机的气体流出物添加特殊物质的方法和装置，以便在喷气发动机喷嘴后面产生增加的压力区的“虚拟壁”，其可以用作喷气发动机气体流出以推动的支撑，从而增加喷气发动机的推力。加速功率的这种增加导致配备喷气发动机的车辆的加速运动或更高的燃料效率。提出了一种将特殊物质添加到气体流出物的装置。特殊物质的特征，如果加入到喷气发动机气体流出中，则可能会在喷气发动机后面产生增加压力区的“虚拟壁”。

5. 发明授权

US06983587B2 Method and apparatus for thrust augmentation for rocket nozzles 有权
标题翻译：火箭喷嘴推力增大的方法和装置
公开(公告)号：US06983587B2
公开(公告)日：2006-01-10
申请号：US10282219
申请日：2002-10-28
申请人： James Shumate
发明人： James Shumate
IPC分类号： B63H11/00 , B64G9/00 , F02K9/00 , F03H9/00 , F23R9/00
CPC分类号： F02K9/97 , F02K9/82 , F05D2240/128 , F05D2240/1281 , Y02T70/56
摘要： A method and apparatus for augmenting thrust in a rocket traveling through atmospheric gas. Rocket motor designs are provided where a throat(s) from one or more rocket motors eject high-speed primary exhaust gas in a configuration which peripherally surrounds an outlet for induced, secondary gas. The secondary gas is mixed with the jet of primary exhaust gas to add momentum, and therefore thrust. Either expansion deflection or plug type rocket discharge nozzles can be utilized. In one embodiment, a thrust augmentation of over one hundred percent is achieved. In another embodiment, a plurality of rocket motor assemblies each containing a thrust augmenting rocket motor design is affixed to a rocket body. Such rocket motors enhance rocket thrust performance, and enables more efficient payload to rocket motor selection, or, alternatively, allows higher loads to be carried with the same amount of thrust.
摘要翻译：一种用于增加在大气中行驶的火箭的推力的方法和装置。提供火箭发动机设计，其中来自一个或多个火箭发动机的喉部以周围围绕用于感应的二次气体的出口的构造喷射高速初级废气。二次气体与一次排气的喷气混合，增加动量，因此推力。可以使用膨胀偏转或塞子型火箭喷射喷嘴。在一个实施例中，实现了超过百分之一的推力增加。在另一个实施例中，每个包含推力增强火箭发动机设计的多个火箭发动机组件固定在火箭体上。这种火箭发动机提高了火箭推力性能，并且使得能够更有效地进行火箭发动机的选择，或者允许以相同的推力承载更高的负载。

6. 发明申请

US20040121663A1 Variable venturi 有权
标题翻译：可变文丘里
公开(公告)号：US20040121663A1
公开(公告)日：2004-06-24
申请号：US10617354
申请日：2003-07-11
发明人： Bhaskar Marathe , Gilles Pesant , Dusablon Patrice
IPC分类号： B63H011/00
CPC分类号： B63H11/10 , Y02T70/56
摘要： Variable venturis for use in jet propulsion systems of watercraft include discharge openings with selectively variable discharge areas that enable a venturi controller to selectively maximize top speed, acceleration, and/or fuel efficiency. The variable venturi may include a plurality of circumferentially-spaced, squeezable, flexible sections that selectively move radially inwardly to alter the discharge area. Alternatively, the variable venturi may include a flexible venturi with a variably-shaped flexible discharge opening. Alternatively, the variable venturi may include a main rear discharge opening and a plurality of additional discharge openings with selectively openable valves, whereby selective opening of the valves effectively increases the discharge area. Alternatively, the variable venturi may have a movable end flap that selectively varies the discharge area.
摘要翻译：用于船舶喷气式推进系统的可变风口包括具有选择性可变放电区域的排放口，使得文氏管控制器能够选择性地最大化最大速度，加速度和/或燃料效率。可变文丘里管可以包括多个周向间隔开的可挤压的柔性部分，其选择性地径向向内移动以改变排放区域。或者，可变文丘里管可以包括具有可变形的柔性排出口的柔性文丘里管。或者，可变文丘里管可以包括主后排出口和具有可选择打开的阀的多个附加排出口，由此阀的选择性打开有效地增加了排出面积。或者，可变文丘里管可以具有选择性地改变排放区域的可移动端盖。

7. 发明申请

US20140109821A1 Aquatic Vehicle 有权
标题翻译：水上车
公开(公告)号：US20140109821A1
公开(公告)日：2014-04-24
申请号：US13792689
申请日：2013-03-11
申请人： BOSTON ENGINEERING CORPORATION
发明人： Michael Rufo , David Shane , Michael Conry , Will Ober
IPC分类号： B63G8/08 , F16F3/00 , B63H11/00
CPC分类号： B63G8/08 , B63B7/085 , B63H1/36 , B63H11/00 , F16F1/025 , F16F3/00 , Y02T70/56
摘要： An underwater vehicle includes a fore-body and a flexible aft. The flexible aft includes a flexible body. The flexible body includes a spring body including a spring element extending along a main axis, and a cavity. Related apparatus, systems, techniques, and articles are also described.
摘要翻译：水下航行器包括前身和柔性船尾。灵活的后部包括柔性主体。弹性体包括弹簧体，弹簧体包括沿着主轴线延伸的弹簧元件和空腔。还描述了相关装置，系统，技术和制品。

8. 发明授权

US08596036B2 Hybrid propulsive engine including at least one independently rotatable compressor rotor 有权
标题翻译：混合推进式发动机包括至少一个可独立旋转的压缩机转子
公开(公告)号：US08596036B2
公开(公告)日：2013-12-03
申请号：US12590046
申请日：2009-10-30
申请人： Roderick A. Hyde , Muriel Y. Ishikawa , Edward K. Y. Jung , Jordin T. Kare , Nathan P. Myhrvold , Clarence T. Tegreene , Thomas A. Weaver , Lowell L. Wood, Jr. , Victoria Y. H. Wood
发明人： Roderick A. Hyde , Muriel Y. Ishikawa , Edward K. Y. Jung , Jordin T. Kare , Nathan P. Myhrvold , Clarence T. Tegreene , Thomas A. Weaver , Lowell L. Wood, Jr. , Victoria Y. H. Wood
IPC分类号： B63H11/00
CPC分类号： F02C6/00 , F02C6/18 , F02K3/06 , F05D2220/31 , F05D2220/324 , F05D2220/325 , F05D2220/76 , H02K7/1823 , Y02T50/672 , Y02T70/56
摘要： A hybrid propulsive technique, comprises providing at least some first thrust associated with a flow of a working fluid through at least a portion of an at least one axial flow jet engine. The hybrid propulsive technique includes extracting energy at least partially in the form of electrical power from the working fluid, and converting at least a portion of the electrical power to torque. The hybrid propulsive technique further includes rotating an at least one substantially axial-flow independently rotatable compressor rotor at least partially responsive to the converting the at least a portion of the electrical power to torque.
摘要翻译：混合推进技术包括通过至少一个轴流式喷气发动机的至少一部分提供与工作流体流相关联的至少一些第一推力。混合推进技术包括从工作流体至少部分地以电力的形式提取能量，并且将至少一部分电功率转换为扭矩。混合推进技术还包括至少部分地响应于将至少一部分电功率转换为扭矩来旋转至少一个基本上轴向流动的可独立旋转的压缩机转子。

9. 发明申请

US20070292278A1 Axial Flow Pump and Marine Propulsion Device 审中-公开
标题翻译：轴流泵和船用推进装置
公开(公告)号：US20070292278A1
公开(公告)日：2007-12-20
申请号：US10591025
申请日：2005-03-15
申请人： Donald Cornell , William Farrell
发明人： Donald Cornell , William Farrell
IPC分类号： B63H11/00 , F04B1/00 , F04B49/00
CPC分类号： F04D15/0022 , B63H11/08 , B63H11/103 , B63H11/11 , B63H2011/046 , B63H2011/081 , B63H2011/084 , F04D3/00 , F04D29/566 , Y02T70/56
摘要： A mechanically reconfigurable marine propulsion device that adapts to engine torque and/or vessel speed thereby providing improved propulsive efficiency and performance. The axial flow propulsion device has two or more stages each having an impeller section and a stator section. Stator vanes and/or the pumping chamber provide a flow diffusion that generates increased hydrostatic pressure from ram pressure recovered from high velocity working fluid which, due to reduced fluid velocity and increased hydrostatic pressure, lowers cavitation events and frictional losses within the propulsion device. Optionally, variable-pitch vanes in the stator section control the amount of ram pressure imparted to the working fluid. Also optionally, variable-pitch inlet guide vanes control the whirl angle and/or mass flow rate of incoming fluid independently of rotor or vessel speed. A set of fixed or variable exit guide vanes aft of the pumping chamber provides flow straightening and pressure maintenance at a discharge nozzle. Other options include a dual flow concentric pumping arrangement that improves performance at low to moderate vessel speeds, an inlet diffuser that recovers ram pressure within an intake duct, and/or a variable area throat in the discharge nozzle that controls the water jet exit velocity according to vessel speed in order to maintain propulsive efficiency. Advantageously, the variable geometry propulsion device enables a shipmaster to achieve improved performance and fuel efficiency over a wide range of vessel speed, vessel loading, sea state conditions, power settings, and/or engine set points in order to achieve higher vessel speeds (e.g., 10 to 30 kts) and/or greater range (e.g., 25-40%) over conventional marine pump jets (i.e., centrifugal or mixed-flow waterjets), which is particularly useful for vessels utilizing 10 to 100 megawatt power plants.
摘要翻译：适用于发动机转矩和/或容器速度的机械可重构船用推进装置，从而提供改进的推进效率和性能。轴流推进装置具有两个或更多个阶段，每个阶段具有叶轮部分和定子部分。定子叶片和/或泵送室提供流量扩散，其从高速工作流体回收的压力压力产生增加的静水压力，由于降低的流体速度和增加的静水压力，降低推进装置内的气蚀事件和摩擦损失。可选地，定子部分中的可变节流叶片控制施加到工作流体的压头压力的量。也可选地，可变间距入口导向叶片独立于转子或容器速度控制进入流体的旋转角度和/或质量流率。泵送室后面的一组固定的或可变的出口导向叶片在排放喷嘴处提供流动矫正和压力维持。其他选择包括双流同心泵送装置，其改善了在低至中等容器速度下的性能，入口扩散器，其恢复进气管道内的压头压力，和/或排放喷嘴中的可变区域喉部，其控制水射流出口速度，以船舶速度，以保持推进效率。有利地，可变几何推进装置使得船主能够在宽范围的船舶速度，船舶装载，海况状态，功率设置和/或发动机设定点上实现改进的性能和燃料效率，以便实现更高的船舶速度（例如，10至30kts）和/或更大的范围（例如，25-40％）超过常规船用泵射流（即离心式或混流式喷水器），这对于使用10至100兆瓦发电厂的船舶特别有用。

10. 发明授权

US07114323B2 Jet exhaust noise reduction system and method 有权
标题翻译：喷气排气降噪系统及方法
公开(公告)号：US07114323B2
公开(公告)日：2006-10-03
申请号：US10794968
申请日：2004-03-05
申请人： Robert Schlinker , Satish Narayanan , Wesley K. Lord , Gregory A. Kohlenberg , Ramons Reba , John Simonich , Marios C. Soteriou , Thierry Maeder
发明人： Robert Schlinker , Satish Narayanan , Wesley K. Lord , Gregory A. Kohlenberg , Ramons Reba , John Simonich , Marios C. Soteriou , Thierry Maeder
IPC分类号： B63H11/00 , B64G9/00 , F02K9/00 , F03H9/00 , F23R9/00
CPC分类号： F02K1/386 , Y02T70/56
摘要： A system for reducing jet noise emission from an internally mixed gas turbine engine exhaust, comprising a fan/core flow mixer having a plurality of mixer lobes and a common flow nozzle having an equal number of tabs located along a circumferential edge of an aft end of the nozzle. There is a predetermined clocking relationship between the plurality of mixer lobes and the plurality of nozzle tabs that results in reduced exhaust noise emission, most evident in the lower frequency range. A method for reducing jet noise emission from an internally mixed gas turbine engine exhaust comprises selectively aligning a circumferential distribution of a mixed flow vorticity field produced by a fan/core mixer with a circumferentially distributed exhaust flow vorticity field produced by a modified common flow nozzle at an exit plane of the engine exhaust.
摘要翻译：一种用于减少来自内部混合燃气涡轮发动机排气的喷射噪声发射的系统，包括具有多个混合器叶片的风扇/芯流混合器和具有相同数量的翼片的公共流动喷嘴，所述翼片沿着沿着喷嘴。在多个混合器叶片和多个喷嘴翼片之间存在预定的时钟关系，其导致减少的排气噪声发射，在较低的频率范围中最明显。一种用于减少内部混合燃气涡轮发动机废气排放的喷射噪声的方法包括：选择性地将由风扇/核心混合器产生的混合涡流场的周向分布与由改进的公共流动喷嘴产生的周向分布的排气涡流场对齐发动机排气口的出口面。

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