专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20160252074A1 VANE ASSEMBLY FOR A FLUID DYNAMIC MACHINE AND PROPULSION DEVICE 审中-公开
标题翻译：流体动力机和推进装置的组件
公开(公告)号：US20160252074A1
公开(公告)日：2016-09-01
申请号：US15030767
申请日：2014-10-22
申请人： Miroslav NOVAK , SOLATRONIC INTERNATIONAL CORPORATION LIMITED
发明人： Miroslav NOVAK
IPC分类号： F03D3/06 , B63H9/08 , B63H9/06 , F03D3/00 , F03D1/06
CPC分类号： F03D3/067 , B63H9/0607 , B63H9/0685 , B63H9/08 , B63H13/00 , F03B3/14 , F03B17/065 , F03D1/0666 , F03D1/0683 , F03D3/005 , F03D3/061 , F03D3/064 , F03D9/32 , F05B2240/202 , F05B2240/931 , F05B2250/314 , F05B2250/411 , F05B2250/711 , F05B2250/712 , Y02E10/223 , Y02E10/28 , Y02E10/721 , Y02E10/74 , Y02T70/5254 , Y02T70/58
摘要： A vane assembly, particularly suitable for a transverse flow, or vertical axis, turbine or a propulsion device includes a vane with at least one concavo-convex part that is mounted by a pivot so that it is free to rotate about a pivot axis. The pivot connects the vane to a rotor with an axis of rotation. The pivot axis is inclined to the concave face such that, as the rotor turns, the vane is free to rotate about the pivot axis between a first position in which the vane defines a high-drag configuration for retreating with a transverse fluid flow, and a second position in which the vane defines a reduced-drag configuration for advancing against the transverse fluid flow.
摘要翻译：特别适用于横向流动或垂直轴线，涡轮机或推进装置的叶片组件包括具有至少一个凹凸部分的叶片，所述至少一个凹凸部分由枢轴安装，使得其绕枢转轴线自由旋转。枢轴将叶片连接到具有旋转轴的转子。所述枢转轴线相对于所述凹面倾斜，使得当所述转子转动时，所述叶片绕所述枢转轴线自由旋转，所述第一位置在所述第一位置和所述第一位置之间，所述第一位置中所述叶片限定用于与横向流体流动退回的高阻力构造，第二位置，其中叶片限定了减小拖曳构型以抵抗横向流体流动。

2. 发明授权

US09309860B2 Wave energy conversion device 有权
标题翻译：波能量转换装置
公开(公告)号：US09309860B2
公开(公告)日：2016-04-12
申请号：US13508347
申请日：2010-11-04
申请人： Raphael Hon
发明人： Raphael Hon
IPC分类号： F03B13/18 , F03B13/12 , F03B13/16 , F03B13/20 , F03B13/24 , B63B35/44
CPC分类号： F03B13/1815 , B63B2035/4466 , F03B13/12 , F03B13/16 , F03B13/18 , F03B13/1805 , F03B13/181 , F03B13/186 , F03B13/20 , F03B13/24 , F05B2210/404 , F05B2240/40 , F05B2240/93 , F05B2240/95 , F05B2250/411 , F05B2260/4021 , F05B2260/4031 , Y02E10/20 , Y02E10/32 , Y02E10/38
摘要： Several embodiments of a device for economically harvesting wave energy are disclosed. A sealed vessel for air storage, the spar buoy, is mostly submerged under water is also used as an inertial body that surface floats move relative to. The spar buoy may take many geometrical forms, but all have a stem that is above the water surface. Piston pumps are placed at the top of the stem. The pump has a gearing reduction to optimize the rotational motion of the pump drive shaft. Small angular motion at the drive shaft results in multiple cycles of linear reciprocal motion of the piston. Various mechanisms could convert the relative motion between the floats and the spar buoy to a rotational motion of the shaft. The compressed air generated by the pump is stored in the spar buoy and regenerated as electrical energy by expanding the compressed air in a turbine.
摘要翻译：公开了用于经济地收获波能的装置的几个实施例。用于空气储存的密封容器，翼梁浮标主要被淹没在水下，也用作表面浮动相对的惯性体。翼梁浮标可能具有许多几何形状，但都具有位于水面之上的杆。活塞泵位于阀杆顶部。泵具有齿轮减速以优化泵驱动轴的旋转运动。驱动轴处的小角度运动导致活塞的线性往复运动的多个循环。各种机构可以将浮子和翼梁浮标之间的相对运动转换成轴的旋转运动。由泵产生的压缩空气被储存在翼梁浮标中，并通过在涡轮机中膨胀压缩空气而再生为电能。

3. 发明申请

US20140110944A1 FLAG INSTABILITY FOR DIRECT MECHANICAL POWER GENERATION 审中-公开
标题翻译：直接机械发电的标志不稳定性
公开(公告)号：US20140110944A1
公开(公告)日：2014-04-24
申请号：US14062509
申请日：2013-10-24
申请人： Morteza Gharib , Julia Cosse , Daegyoum Kim
发明人： Morteza Gharib , Julia Cosse , Daegyoum Kim
IPC分类号： F03D5/06 , F03B13/00
CPC分类号： F03D5/06 , F01D5/147 , F03B17/06 , F03D1/0658 , F03D3/06 , F05B2250/411 , Y02E10/28 , Y02E10/70 , Y02E10/721 , Y02P80/158 , Y10T29/49336
摘要： Flag-type wind and/or water power generation features are described. Fluid-filled embodiments are described. The fluid may be employed for pumping effect and/or dynamic physical property change. Leading-edge and trailing-edge mounted flag architectures are described with various applications including flapping flag arrays and Vertical Axis Wind Turbines (VAWTs).
摘要翻译：描述了旗型风和/或水发电特征。描述流体填充的实施例。流体可用于泵送效应和/或动态物理性能变化。前沿和后缘安装的标志结构被描述为各种应用，包括拍动标志阵列和垂直轴风力发电机（VAWT）。

4. 发明授权

US08314506B2 Direct drive rotary wave energy conversion 有权
标题翻译：直接驱动旋转波能量转换
公开(公告)号：US08314506B2
公开(公告)日：2012-11-20
申请号：US12656950
申请日：2010-02-22
申请人： Kenneth Edward Rhinefrank , Bradford Storrs Lamb , Joseph Horan Prudell , Alphonse Aloysius Schacher
发明人： Kenneth Edward Rhinefrank , Bradford Storrs Lamb , Joseph Horan Prudell , Alphonse Aloysius Schacher
IPC分类号： F03B13/10 , F03B13/12 , H02P9/04
CPC分类号： F03B13/264 , F03B13/20 , F05B2250/411 , F05B2260/403 , Y02E10/28 , Y02E10/38
摘要： An apparatus and method for converting wave energy using the relative rotational movement between two interconnected float assemblies and the relative rotational movement between each of the float assemblies and a spar which extends from a connection with the float assemblies at the water surface into the water.
摘要翻译：一种用于使用两个相互连接的浮子组件之间的相对旋转运动并且在每个浮子组件之间的相对旋转运动以及从与水表面处的浮子组件的连接延伸到水中的翼梁来转换波能的装置和方法。

5. 发明申请

US20120171035A1 LEVERAGE-MAXIMIZING VERTICAL AXIS RECIPROCATING BLADE HYDRO POWER GENERATOR 审中-公开
标题翻译：垂直轴最大化叶片式水力发电机
公开(公告)号：US20120171035A1
公开(公告)日：2012-07-05
申请号：US13342639
申请日：2012-01-03
申请人： Paul Fransen
发明人： Paul Fransen
IPC分类号： F03B17/02
CPC分类号： F03B17/06 , F03B13/264 , F03B17/067 , F05B2250/411 , Y02E10/28
摘要： The present invention relates in general to the field of hydropower devices using a reciprocating or oscillating blade system. It aims at utilizing the currents of oceans and seas and rivers to generate electricity. Its distinguishing design makes it possible to realize a leverage factor, much larger than existing devices using a reciprocating or oscillating blade system, and by this it will introduce leverage as a main characteristic for harnessing the power of relatively slow river and ocean currents by devices using a reciprocating or oscillating blade system.
摘要翻译：本发明一般涉及使用往复式或摆动式叶片系统的水力发电装置领域。它的目的是利用海洋和河流的电力来发电。其独特的设计使得可以实现比使用往复式或摆动式叶片系统的现有装置更大的杠杆因子，并且通过这种方式将引入杠杆作为利用相对较慢的河流和洋流的功率的主要特征，往复式或摆动式叶片系统。

6. 发明申请

US20110058956A1 HYBRID MULTI-ELEMENT TAPERED ROTATING TOWER 失效
标题翻译：混合多元旋转塔
公开(公告)号：US20110058956A1
公开(公告)日：2011-03-10
申请号：US12836089
申请日：2010-07-14
申请人： Michael D. Zuteck
发明人： Michael D. Zuteck
IPC分类号： F03D11/04
CPC分类号： F03D13/20 , F03D1/00 , F03D1/04 , F03D7/02 , F03D7/0204 , F03D80/00 , F03D80/70 , F05B2240/12 , F05B2240/54 , F05B2240/912 , F05B2250/411 , F05B2250/70 , Y02E10/723 , Y02E10/728 , Y10S415/908
摘要： The specification discloses a rotating turbine tower. The tower rotates to maintain the turbine facing into the wind. This allows structural optimization. The tower structure is comprised of a leading edge and a trailing edge, with joining panels between the edge structures. The tower edges are the main structural components of the tower. The separation of the edges tapers to follow the thrust bending moment on the tower, reducing the need to taper material thickness. The tapering shape of the tower structure matches the primary edgewise moment distribution. The tower can be assembled on site from components, thereby facilitating transportation to the tower site. The material properties and shape can be selected based upon the tower maintaining a near constant orientation with the wind. This can save weight and costs. The tower architecture can be of differing shapes such as a triangle or a structure tapering at each end.
摘要翻译：本说明书公开了一种旋转涡轮机塔架。塔架旋转以保持涡轮机面向风。这允许结构优化。塔架结构由前缘和后缘组成，其边缘结构之间具有接合面板。塔边是塔的主要结构部件。边缘的分离随着塔上的推力弯曲力矩逐渐变细，减少了材料厚度的渐缩。塔结构的锥形形状与主边缘力矩分布相匹配。该塔可以从现场组装，从而便于运输到塔楼。材料性质和形状可以基于塔保持与风接近恒定的方向来选择。这可以节省重量和成本。塔架构可以具有不同的形状，例如三角形或在每一端逐渐变细的结构。

7. 发明申请

US20100189565A1 SECTIONAL VANE FOR VERTICAL AXIS WIND POWER GENERATOR 失效
标题翻译：垂直轴风力发电机的分段
公开(公告)号：US20100189565A1
公开(公告)日：2010-07-29
申请号：US12691748
申请日：2010-01-22
申请人： Dong-Hua YEH
发明人： Dong-Hua YEH
IPC分类号： F03D3/06
CPC分类号： F03D3/067 , F05B2250/411 , Y02E10/74
摘要： A sectional vane for vertical axis wind power generator includes a frame unit and a plurality of vane units. The frame unit is fixedly mounted to a main shaft of the wind power generator, and includes an upper frame member and at least one lower frame member. The upper and lower frame members are provided on inner side with an upper and a lower guide rail, respectively. The vane unit includes a vane body having an upper and a lower guide channel provided on a top and a bottom, respectively, corresponding to the upper and the lower guide rail. The vane units are assembled to the frame unit between the upper and the lower frame member through engagement of the guide channels with the guide rails. The sectional vane can be varied in height and area by providing different numbers of lower frame members and vane units.
摘要翻译：用于垂直轴风力发电机的截面叶片包括框架单元和多个叶片单元。框架单元固定地安装到风力发电机的主轴上，并且包括上框架构件和至少一个下框架构件。上框架构件和下框架构件分别在内侧设置有上导轨和下导轨。叶片单元包括叶片体，该叶片体具有分别设置在上下导向槽的顶部和底部的上部和下部引导通道。叶片单元通过引导通道与导轨的接合而组装到上框架构件和下框架构件之间的框架单元。通过提供不同数量的下框架构件和叶片单元，分段叶片可以在高度和面积上变化。

8. 发明授权

US4825641A Control mechanism for injector diaphragms 失效
标题翻译：喷油器隔膜的控制机构
公开(公告)号：US4825641A
公开(公告)日：1989-05-02
申请号：US69103
申请日：1987-07-02
申请人： Gerard M. F. Mandet , Rodolphe Martinez
发明人： Gerard M. F. Mandet , Rodolphe Martinez
IPC分类号： F23R3/26 , F23R3/50 , F02C9/00 , F02C1/00
CPC分类号： F23R3/26 , F23R3/50 , F05B2250/411
摘要： A control mechanism for injector diaphragms in a turbojet engine is disclosed wherein an annular fairing is utilized to synchronize the movement of the individual air-fuel injector diaphragms. The fairing member is interconnected to each of the diaphragms and a single control element controls the rotational movement of the annular fairing. This minimizes the turbulence of the air flow passing around the control system.
摘要翻译：公开了一种用于涡轮喷气发动机中的喷射器隔膜的控制机构，其中使用环形整流罩来同步各个空气 - 燃料喷射器隔膜的运动。整流罩构件互连到每个隔膜，单个控制元件控制环形整流罩的旋转运动。这样可以最大限度地减少通过控制系统的气流的紊流。

9. 发明授权

US4498287A Combustors and methods of operating same 失效
标题翻译：燃烧器和操作方法相同
公开(公告)号：US4498287A
公开(公告)日：1985-02-12
申请号：US427250
申请日：1982-09-29
申请人： Robert M. Schirmer , Ellsworth H. Fromm
发明人： Robert M. Schirmer , Ellsworth H. Fromm
IPC分类号： F23C6/04 , F23R3/26 , F02C3/14
CPC分类号： F23R3/26 , F23C6/04 , F05B2250/411
摘要： New combustors which produce lower emissions, particularly lower emissions of nitrogen oxides and CO, are provided. The combustors are provided with a first combustion region that is cylindrical, short and of small diameter and an adjacent downstream second combustion region comprising an abrupt enlargement in diameter to provide a relatively larger capacity than the first combustion region. A first stream of air is introduced, either radially, axially, or tangentially, into the first combustion region and the amount of said air is varied in accordance with fuel flow to the first combustion region. A second stream of air is introduced tangentially into the first combustion region. A third stream of air is introduced tangentially into the second combustion region. In preferred embodiments of the invention the air stream pressure drop across an air assist fuel nozzle is varied in accordance with fuel flow to the nozzle.
摘要翻译：提供了产生较低排放，特别是较低排放的氮氧化物和CO的新型燃烧器。燃烧器设置有圆柱形，短径和小直径的第一燃烧区域和相邻的下游第二燃烧区域，其包括直径突然增大以提供比第一燃烧区域相对更大的容量。第一空气流沿径向，轴向或切向地引入第一燃烧区域，并且所述空气的量根据到第一燃烧区域的燃料流量而变化。第二个空气流切向地引入第一燃烧区域。第三气流被切向地引入第二燃烧区域。在本发明的优选实施例中，穿过空气辅助燃料喷嘴的气流压降根据到喷嘴的燃料流量而变化。

10. 发明授权

US3744242A Recirculating combustor 失效
标题翻译：再生燃烧器
公开(公告)号：US3744242A
公开(公告)日：1973-07-10
申请号：US3744242D
申请日：1972-01-25
申请人： GEN MOTORS CORP
发明人： STETTLER R , VERDOUW A
IPC分类号： F23C9/00 , F02C3/30 , F02C3/34 , F23C99/00 , F23R3/00 , F23R3/02 , F23R3/16 , F23R3/26 , F02C3/00
CPC分类号： F23R3/02 , F05B2250/411 , F23C9/006 , F23C2202/30 , F23C2202/50 , F23R3/005 , F23R3/16 , F23R3/26
摘要： Combustor structure particularly adapted for supplying motive fluid to a gas turbine engine or the like. A combustion liner is mounted within an inner casing, the two defining between them a recirculation duct for combustion products. The inner casing is mounted within an outer casing, these two defining between them a dilution air duct in which the dilution air is heated while cooling the recirculating combustion products. The combustion liner wall is double and defines combustion air duct between the walls with a Coanda nozzle at its downstream end which is the nozzle of a jet pump to effect the recirculation. The combustion liner is supported from the forward wall of the casing by tubes which conduct combustion air into the liner. A valve arrangement controls the ratio of combustion air to dilution air.
摘要翻译：特别适用于向燃气涡轮发动机等供应动力流体的燃烧器结构。燃烧衬套安装在内壳内，两者在它们之间形成用于燃烧产物的再循环管道。内壳安装在外壳内，这两个在它们之间限定稀释空气管道，稀释空气在此冷却循环燃烧产物的同时被加热。燃烧衬套壁是双层的，并且在其下游端具有Coanda喷嘴的壁之间的燃烧空气管道，其是作为喷射泵的喷嘴以实现再循环的下游端。燃烧衬套通过将燃烧空气进入衬管的管从壳体的前壁支撑。阀门装置控制燃烧空气与稀释空气的比例。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式