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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

US08272644B1 Floating card seal 有权
标题翻译：浮动卡片密封
公开(公告)号：US08272644B1
公开(公告)日：2012-09-25
申请号：US12835107
申请日：2010-07-13
申请人： Wilho V Aho, Jr. , Jack W Wilson, Jr. , Vincent P Laurello
发明人： Wilho V Aho, Jr. , Jack W Wilson, Jr. , Vincent P Laurello
IPC分类号： F16J15/44
CPC分类号： F16J15/3292 , F01D11/00 , F05D2240/57 , F05D2250/75
摘要： A card seal with an annular arrangement of leaf elements, where each leaf element has a T shape with an upper ear section and a leaf section extending from the ear section. the leaf elements each include a first raised portion and a second raised portion that form a cross, the raised portions allowing for air to pass to bend ends on the leaf sections to form a floating air seal and to limit leakage flow across the leaf elements from one side to the opposite side.
摘要翻译：一种具有叶片元件的环形布置的卡片密封件，其中每个叶片元件具有T形形状，具有上耳部分和从耳部延伸的叶片部分。叶片元件各自包括形成十字架的第一凸起部分和第二凸起部分，凸起部分允许空气通过以在叶片部分上弯曲端部以形成浮动空气密封并且限制穿过叶片元件的泄漏流动一边到另一边。

4. 发明授权

US07506555B2 Process and apparatus for testing a material under a high temperature and pressure environment 有权
标题翻译：在高温高压环境下测试材料的工艺和设备
公开(公告)号：US07506555B2
公开(公告)日：2009-03-24
申请号：US11642256
申请日：2006-12-20
申请人： Joseph D Brostmeyer , Jack W Wilson, Jr. , Todd A Ebert
发明人： Joseph D Brostmeyer , Jack W Wilson, Jr. , Todd A Ebert
IPC分类号： G01N17/00
CPC分类号： G01N25/00 , G01M15/14 , G01M99/002 , G01N3/18 , G01N17/002 , G01N2203/0042 , G01N2203/0057 , G01N2203/0226 , G01N2203/0232
摘要： A test facility is provided for testing materials under high temperature, pressure, and mechanical loads. The facility provides a physically sealed system that simulates conditions in hot sections or gas turbine engines. A test article is coated with a test material and exposed to a hot combusting flow in a test section housing. The article may be a pipe or conduit member oriented at any direction to the flow. A second cooler flow of fluid is channeled through the test article to create a sharp temperature gradient in the test article and through the test material. A liquid-cooled sleeve is disposed about the test article to create an annular channel of combusting flow over the test article. The downstream end of the second cooler flow is connected to the upstream end of the main hot flow at the combustion chamber.
摘要翻译：提供测试设备用于在高温，高压和机械负载下测试材料。该设施提供了一个物理密封的系统，可模拟热段或燃气轮机的条件。测试物品涂覆有测试材料并暴露于测试部分壳体中的热燃烧流。制品可以是在流动的任何方向上定向的管道或管道构件。流体的第二个较冷的流动通过测试物品，以在测试物品和测试材料中产生尖锐的温度梯度。液体冷却的套筒围绕测试物品设置以产生在测试物品上燃烧的环形通道。第二冷却器流的下游端连接到燃烧室的主热流的上游端。

5. 发明授权

US07750492B1 Bearingless floating wind turbine 有权
标题翻译：无轴承浮动风力发电机
公开(公告)号：US07750492B1
公开(公告)日：2010-07-06
申请号：US12613305
申请日：2009-11-05
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 and 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而窄的主支撑结构，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，垂直轴涡轮机叶片从主支撑结构并在风中一起旋转，并且非旋转轴通过主支撑结构延伸，其中垂直轴直接驱动发电机连接在主支撑结构和非旋转轴之间，以在主支撑结构旋转时产生电力。连接到非旋转轴的锚定线防止浮动风力涡轮机在水体中漂移。

6. 发明授权

US07736131B1 Turbine blade with carbon nanotube shell 失效
标题翻译：带碳纳米管壳的涡轮叶片
公开(公告)号：US07736131B1
公开(公告)日：2010-06-15
申请号：US12244368
申请日：2008-10-02
申请人： Jack W Wilson, Jr.
发明人： Jack W Wilson, Jr.
IPC分类号： F01D5/14
CPC分类号： F01D5/147 , B82Y30/00 , F01D5/28 , F01D5/282 , F05D2300/224
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 formed from carbon or molybdenum nanotubes arranged in a direction such that the nanotubes are under tension when the blade is rotating in the engine. The carbon nanotubes are allotropes of carbon in which the length to diameter ratio exceeds 1,000,000 in order to produce very high tensile strength, unique electrical properties, and a very efficient conductor of heat. The nanotube shell includes a metal insert having a tear drop shape and the lower end of the shell wraps around the metal insert to form a wedge in which the shell is held in place against radial displacement between the platform and the attachment portion of the blade.
摘要翻译：一种用于燃气涡轮发动机的涡轮机叶片，其中涡轮叶片由翼梁和壳体构造制成，其中薄壁壳由碳或钼纳米管形成，所述碳或钼纳米管沿着使得当叶片在发动机中旋转。碳纳米管是长度比直径比超过1,000,000的碳的同素异形体，以产生非常高的拉伸强度，独特的电性能和非常有效的热导体。纳米管壳包括具有泪滴形状的金属插入物，并且壳的下端围绕金属插入物缠绕以形成楔，其中壳保持在适当位置，以防止平台与叶片的附接部分之间的径向位移。

7. 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。

8. 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。

9. 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。

10. 发明授权

US08015705B2 Spar and shell blade with segmented shell 有权
公开(公告)号：US08015705B2
公开(公告)日：2011-09-13
申请号：US12843935
申请日：2010-07-27
申请人： Jack W Wilson, Jr. , Wesley D Brown
发明人： Jack W Wilson, Jr. , Wesley D Brown
IPC分类号： F01D5/18
CPC分类号： F01D5/147 , F01D5/189 , F01D5/20 , Y10T29/49327 , Y10T29/49339 , Y10T29/49341
摘要： A turbine rotor blade with a spar and shell construction, where the shell has an airfoil shape and is formed of two shell segments with an upper shell half and a lower shell half. The upper shell half is radially supported by a tip of the spar while the lower shell half is radially loaded by an attachment so that its load is not carried by the upper shell half and the tip of the spar in order to reduce overall stress levels.

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