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1. 发明授权

US07633175B1 Resonating blade for electric power generation 失效
标题翻译：谐振叶片用于发电
公开(公告)号：US07633175B1
公开(公告)日：2009-12-15
申请号：US12119549
申请日：2008-05-13
申请人： Jack W Wilson, III , Jack W Wilson, Jr.
发明人： Jack W Wilson, III , Jack W Wilson, Jr.
IPC分类号： F03B13/12 , F03B13/10 , H02P9/04
CPC分类号： F01D9/041 , F05D2220/60 , F05D2240/12
摘要： A process and an apparatus for generating electric current from a vibrating blade exposed to a fluid flow, in one embodiment, a plurality of blades are secured within a tail cone of a steam turbine and each blade includes a magnet and a coil associated with the magnet to produce electric current in the coil when the magnet moves across the coil. Each blade is designed to have a natural frequency so that the blade will resonate under the influence of the exhaust flow from the turbine in the tail cone. Abutment members are mounted on the blade or the fixed support to limit the range of motion of the vibrating blade so that it does not exceed the fatigue limit. The blades are made from a low damping material such as titanium so that a low frequency is produced.
摘要翻译：一种用于从暴露于流体流动的振动叶片产生电流的方法和装置，在一个实施例中，多个叶片被固定在蒸汽轮机的尾锥体内，并且每个叶片包括磁体和与磁体相关联的线圈当磁体穿过线圈移动时，在线圈中产生电流。每个叶片被设计成具有固有频率，使得叶片在来自尾锥体中的涡轮机的排气流的影响下将共振。基台部件安装在叶片或固定支架上，以限制振动叶片的运动范围，使其不超过疲劳极限。叶片由诸如钛的低阻尼材料制成，从而产生低频率。

2. 发明授权

US07884490B1 Resonating blade for electric power generation 有权
标题翻译：谐振叶片用于发电
公开(公告)号：US07884490B1
公开(公告)日：2011-02-08
申请号：US12629096
申请日：2009-12-02
申请人： Jack W Wilson, III , Jack W Wilson, Jr.
发明人： Jack W Wilson, III , Jack W Wilson, Jr.
IPC分类号： F03B13/12 , F03B13/10 , H02P9/04
CPC分类号： F01D9/041 , F05D2220/60 , F05D2240/12
摘要： An apparatus for generating electric current from a vibrating blade exposed to a fluid flow. in one embodiment, a plurality of blades are secured within a tail cone of a steam turbine and each blade includes a magnet and a coil associated with the magnet to produce electric current in the coil when the magnet moves across the coil. Each blade is designed to have a natural frequency so that the blade will resonate under the influence of the exhaust flow from the turbine in the tail cone. Abutment members are mounted on the blade or the fixed support to limit the range of motion of the vibrating blade so that it does not exceed the fatigue limit. The blades are made from a low damping material such as titanium so that a low frequency is produced.
摘要翻译：一种用于从暴露于流体流动的振动叶片产生电流的装置。在一个实施例中，多个叶片被固定在蒸汽轮机的尾锥内，并且每个叶片包括磁体和与磁体相关联的线圈，以在磁体移动穿过线圈时在线圈中产生电流。每个叶片被设计成具有固有频率，使得叶片在来自尾锥体中的涡轮机的排气流的影响下将共振。基台部件安装在叶片或固定支架上，以限制振动叶片的运动范围，使其不超过疲劳极限。叶片由诸如钛的低阻尼材料制成，从而产生低频率。

3. 发明授权

US08556576B2 Cooled IBR for a micro-turbine 有权
标题翻译：用于微型涡轮的冷却IBR
公开(公告)号：US08556576B2
公开(公告)日：2013-10-15
申请号：US12894476
申请日：2010-09-30
申请人： Jack W Wilson, Jr. , John E Ryznic , James P Downs
发明人： Jack W Wilson, Jr. , John E Ryznic , James P Downs
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/081 , F01D5/34 , F01D11/001 , F05D2250/80 , F05D2260/202 , F05D2260/205 , Y02T50/676
摘要： A micro gas turbine engine in which the turbine rotor blades are formed as an integral bladed rotor with cooling air passages formed within the blades and the rotor disk by an EDM process. an adjacent stator vane includes an air riding seal with an air cushion supplied through the vanes to provide cooling, and where the air cushion is then passed into the turbine blades and rotor disk to provide cooling for the turbine blades. With cooling of the turbine blades, higher turbine inlet temperatures for micro gas turbine engines can be produced.
摘要翻译：一种微型燃气涡轮发动机，其中涡轮机转子叶片形成为整体叶片转子，其中通过EDM工艺在叶片和转子盘中形成冷却空气通道。相邻的定子叶片包括具有通过叶片提供的气垫的空气骑行密封件以提供冷却，并且其中气垫然后进入涡轮机叶片和转子盘以为涡轮叶片提供冷却。通过涡轮叶片的冷却，可以生产用于微型燃气涡轮发动机的更高的涡轮机入口温度。

4. 发明授权

US08511999B1 Multiple piece turbine rotor blade 有权
标题翻译：多片涡轮转子叶片
公开(公告)号：US08511999B1
公开(公告)日：2013-08-20
申请号：US12731928
申请日：2010-03-25
申请人： Keith D Kimmel , Jack W. Wilson , Russell B Jones
发明人： Keith D Kimmel , Jack W. Wilson , Russell B Jones
IPC分类号： F01D5/14
CPC分类号： F01D5/147 , F01D5/20 , F01D5/30 , F05D2300/13 , F05D2300/131
摘要： A turbine rotor blade of the spar and shell construction, the spar including a tip end with a dovetail shaped groove extending from the top, and a tip cap includes a dovetail shaped slot that engages with the spar groove to retain the tip cap in place. A shell made from a high temperature resistant material is secured in place between the platform and the tip cap. The platform includes a core extending into a hollow space formed by the shell and discharges impingement cooling air against the backside wall of the shell. The spar and the platform include fir tree configurations so that an assembled blade can be inserted into a slot of a rotor disk.
摘要翻译：翼梁和壳体结构的涡轮机转子叶片，翼梁包括具有从顶部延伸的燕尾形槽的末端，并且尖端帽包括与翼梁槽接合以将顶盖保持在适当位置的燕尾形槽。由耐高温材料制成的外壳固定在平台和顶盖之间的适当位置。平台包括延伸到由壳体形成的中空空间中的芯体，并将冲击冷却空气排放到壳体的后壁上。翼梁和平台包括枞树构造，使得组装的叶片可以插入转子盘的槽中。

5. 发明授权

US08235655B1 Variable inlet guide vane assembly 有权
标题翻译：可变入口导叶组件
公开(公告)号：US08235655B1
公开(公告)日：2012-08-07
申请号：US13072687
申请日：2011-03-26
申请人： William W. Pankey , Jack W. Wilson, Jr.
发明人： William W. Pankey , Jack W. Wilson, Jr.
IPC分类号： F01B25/02
CPC分类号： F01D17/162 , F01D17/20 , F05D2200/33
摘要： A variable inlet guide vane assembly for a gas turbine engine, where the guide vanes are pivotably connected to a sync ring that is contained within an annular groove within the casing so that leakage through holes in the casing is minimized. The guide vanes include a slider mechanism on one of the ends that will allow for both an axial and a rotational movement of the guide vane pin when the guide vanes pivot about a fixed pin on an opposite end of the guide vanes. A round rotary vane actuator with a height much less than a diameter is mounted outside of the casing and connects to the sync ring through a driving linkage.
摘要翻译：一种用于燃气涡轮发动机的可变入口引导叶片组件，其中导向叶片可枢转地连接到容纳在壳体内的环形槽内的同步环，使得通过壳体中的孔的泄漏最小化。导向叶片包括在其中一个端部上的滑动机构，当导叶绕导向叶片的相对端上的固定销枢转时，该滑块机构将允许导叶销的轴向和旋转运动。具有远小于直径的高度的圆形旋片式致动器安装在壳体的外部并且通过驱动连杆连接到同步环。

6. 发明授权

US07893556B1 Vertical axis wind turbine with direct drive generator 有权
标题翻译：具有直接驱动发电机的立轴风力发电机
公开(公告)号：US07893556B1
公开(公告)日：2011-02-22
申请号：US12780967
申请日：2010-05-17
申请人： John E Ryznic , Joseph D Brostmeyer , Jack W Wilson, Jr.
发明人： John E Ryznic , Joseph D Brostmeyer , Jack W Wilson, Jr.
IPC分类号： F03D3/04
CPC分类号： F03D3/005 , F03D13/25 , F05B2220/7066 , F05B2220/7068 , F05B2240/212 , F05B2240/301 , F05B2240/61 , F05B2240/93 , F05B2240/95 , F05B2260/85 , F05B2260/90 , Y02E10/727 , Y02E10/74
摘要： A bearingless floating wind turbine has a tall narrow main support structure with a center of buoyancy located well above the center of gravity to provide stability to the wind turbine while supported for rotation in a body of water, a vertical axis turbine blade extends from the main support structure and rotates together under a wind, and a non-rotating shaft extends through the main support structure with a vertical axis direct drive generator connected between the main support structure and the non-rotating shaft to produce electricity when the main support structure rotates. An anchor line connected to the non-rotating shaft prevents the floating wind turbine from drifting in a body of water.
摘要翻译：无轴承浮动风力涡轮机具有高的窄的主要支撑结构，其浮力中心位于重心之上，以便在风力涡轮机同时被支撑以在水体中旋转时提供稳定性，垂直轴线涡轮机叶片从主体支撑结构并在风中一起旋转，并且非旋转轴通过连接在主支撑结构和非旋转轴之间的垂直轴直接驱动发生器延伸通过主支撑结构，以在主支撑结构旋转时产生电力。连接到非旋转轴的锚线防止浮动风力涡轮机在水体中漂移。

7. 发明授权

US07866950B1 Turbine blade with spar and shell 有权
标题翻译：涡轮叶片与翼梁和壳
公开(公告)号：US07866950B1
公开(公告)日：2011-01-11
申请号：US12176622
申请日：2008-07-21
申请人： Jack W Wilson, Jr.
发明人： Jack W Wilson, Jr.
IPC分类号： F01D5/30
CPC分类号： F01D5/147 , F01D5/20 , F05D2230/50 , F05D2300/131 , F05D2300/506
摘要： A turbine blade for use in a gas turbine engine, where the turbine blade is made from a spar and shell construction in which a thin walled shell is held in place between the blade tip and the platform by only a mechanical fastener without using any bonding, welding or brazing. The spar is connected to an attachment by a tie bolt, and a separate platform is secured, over the attachment t in which the shell is held against. This provides for a thermally free platform and shell connection. With this arrangement, the shell is held under compression within the 2% yield stress range such that the turbine blade shell can have an infinite life. Also, the turbine blade is much lighter than prior art blades. As a result, the spar and shell blade produces less stress on the rotor disk during engine operation.
摘要翻译：一种用于燃气涡轮发动机的涡轮机叶片，其中涡轮机叶片由翼梁和壳体结构制成，其中薄壁壳体仅通过机械紧固件而保持在叶片尖端和平台之间的适当位置，而不使用任何接合，焊接或钎焊。翼梁通过连接螺栓连接到附件，并且单独的平台固定在附接件t上，壳体被固定在其上。这提供了一个无热平台和外壳连接。通过这种布置，壳体在2％屈服应力范围内保持压缩，使得涡轮机叶片壳体可以具有无限的寿命。此外，涡轮叶片比现有技术的叶片要轻得多。结果，在发动机运转时，翼梁和壳叶片在转子盘上产生较小的应力。

8. 发明授权

US07670116B1 Turbine vane with spar and shell construction 有权
标题翻译：涡轮叶片与翼梁和壳结构
公开(公告)号：US07670116B1
公开(公告)日：2010-03-02
申请号：US11243308
申请日：2005-10-04
申请人： Jack W. Wilson, Jr. , Wesley D Brown
发明人： Jack W. Wilson, Jr. , Wesley D Brown
IPC分类号： F01D5/14
CPC分类号： F01D5/147 , F01D5/189 , F01D5/20 , Y10T29/49327 , Y10T29/49339 , Y10T29/49341
摘要： The present invention is a vane for us in a gas turbine engine, in which the vane is made of an exotic, high temperature material that is difficult to machine or cast. The vane includes a shell made from either Molybdenum, Niobium, alloys of Molybdenum or Niobium (Columbium), Oxide Ceramic Matrix Composite (CMC), or SiC—SiC ceramic matrix composite, and is formed from a wire electric discharge process. The shell is positioned in grooves between the outer and inner shrouds, and includes a central passageway within the spar, and forms a cooling fluid passageway between the spar and the shell. Both the spar and the shell include cooling holes to carry cooling fluid from the central passageway to an outer surface of the vane for cooling. This cooling path eliminates a serpentine pathway, and therefore requires less pressure and less amounts of cooling fluid to cool the vane.
摘要翻译：本发明是一种用于燃气涡轮发动机的叶片，其中叶片由难以加工或铸造的外来高温材料制成。叶片包括由钼，铌，钼或铌（铌），氧化物陶瓷基复合材料（CMC）或SiC-SiC陶瓷基体复合材料制成的壳体，并由导线放电工艺形成。壳体定位在外护罩之间的凹槽中，并且在翼梁内部包括中心通道，并且在翼梁和壳体之间形成冷却流体通道。翼梁和壳都包括冷却孔，以将冷却流体从中心通道运送到叶片的外表面用于冷却。该冷却路径消除了蛇形通道，因此需要较少的压力和较少量的冷却流体来冷却叶片。

9. 发明申请

US20120104762A1 Large floating vertical axis wind turbine 有权
标题翻译：大浮动垂直轴风力发电机
公开(公告)号：US20120104762A1
公开(公告)日：2012-05-03
申请号：US12913023
申请日：2010-10-27
申请人： Jack W. Wilson, JR. , John E. Ryznic
发明人： Jack W. Wilson, JR. , John E. Ryznic
IPC分类号： F03D9/00 , B23P17/00 , B23P17/04
CPC分类号： F03D3/061 , F03D13/25 , F03D80/70 , F05B2240/93 , F05B2250/86 , Y02E10/727 , Y02E10/74 , Y10T29/49229 , Y10T29/49826
摘要： A large floating vertical axis wind turbine with a floating inner cylinder having rotor blades that rotate together as an assembly, and a floating outer cylinder with a central opening in which the floating inner cylinder rotates for support against tipping. Outriggers with floating devices on the ends extend out from the floating outer cylinder for additional stability. The floating inner cylinder is partially supported by a top bearing on the outer cylinder to carry some of the load from the rotor blades.
摘要翻译：具有浮动内筒的大浮动垂直轴风力涡轮机，其具有作为组件一起旋转的转子叶片，以及具有中心开口的浮动外筒，浮动内筒旋转以支撑以防止倾翻。具有浮动装置的外伸支架从浮动外筒延伸出来以获得额外的稳定性。浮动内筒由外筒上的顶部轴承部分支撑，以承载来自转子叶片的一些载荷。

10. 发明授权

US07922445B1 Variable inlet guide vane with actuator 失效
标题翻译：可变入口导向叶片带执行机构
公开(公告)号：US07922445B1
公开(公告)日：2011-04-12
申请号：US12558901
申请日：2009-09-14
申请人： William W Pankey , Jack W. Wilson, Jr.
发明人： William W Pankey , Jack W. Wilson, Jr.
IPC分类号： F01B25/02
CPC分类号： F01D17/162 , F01D17/20 , F05D2200/33
摘要： A variable inlet guide vane assembly for a gas turbine engine, where the guide vanes are pivotably connected to a sync ring that is contained within an annular groove within the casing so that leakage through holes in the casing is minimized. The guide vanes include a slider mechanism on one of the ends that will allow for both an axial and a rotational movement of the guide vane pin when the guide vanes pivot about a fixed pin on an opposite end of the guide vanes. a round rotary vane actuator with a height much less than a diameter is mounted outside of the casing and connects to the sync ring through a driving linkage.
摘要翻译：一种用于燃气涡轮发动机的可变入口引导叶片组件，其中导向叶片可枢转地连接到容纳在壳体内的环形槽内的同步环，使得通过壳体中的孔的泄漏最小化。导向叶片包括在其中一个端部上的滑动机构，当导叶绕导向叶片的相对端上的固定销枢转时，该滑块机构将允许导叶销的轴向和旋转运动。具有远小于直径的高度的圆形旋转叶片致动器安装在壳体的外部并通过驱动连杆连接到同步环。

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