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1. 发明申请

WO2011106256A3 VERTICAL-AXIS WIND TURBINE HAVING LOGARITHMIC CURVED AIRFOILS 审中-公开
标题翻译：具有对数曲线翼型的垂直轴风力涡轮机
公开(公告)号：WO2011106256A3
公开(公告)日：2011-09-01
申请号：PCT/US2011/025441
申请日：2011-02-18
申请人： NOVASTRON CORPORATION , ROBERTS, Gary, D.
发明人： ROBERTS, Gary, D.
IPC分类号： F03D3/06 , F03D3/02 , F03D11/00
摘要： A vertical-axis, stator-less wind turbine includes a rotor (5) rotatable about a vertical axis. The rotor has a plurality of vertically oriented rotor airfoils (35a-c) disposed circumferentially and with equiangular symmetry about the vertical axis. Each rotor airfoil has a substantially logarithmic curvature with a trailing edge with a trailing edge (82) having a smaller radius of curvature than a leading edge (80), and with the leading edge positioned further from the vertical axis than the trailing edge.
摘要翻译：垂直轴无定子风力涡轮机包括可围绕竖直轴线旋转的转子（5）。该转子具有多个垂直定向的转子翼面（35a-c），该转子翼面沿周向设置并且围绕垂直轴线等角对称。每个转子翼型具有基本对数曲率，其后缘具有后缘（82），后缘具有比前缘（80）更小的曲率半径，并且前缘比后缘更远离竖直轴线定位。 / p>

2. 发明申请

WO9929028A8 SELF-EXCITED ASYNCHRONOUS ALTERNATING CURRENT GENERATOR WITH PARAMUTUAL INDUCTIVE COUPLING 审中-公开
标题翻译：具有辅助电感耦合的自激式异步交流电流发生器
公开(公告)号：WO9929028A8
公开(公告)日：1999-07-29
申请号：PCT/US9723124
申请日：1997-12-04
申请人： ROBERTS GARY D
发明人： ROBERTS GARY D
IPC分类号： H02K17/42 , H02H11/00 , H02K1/00
CPC分类号： H02K17/42
摘要： An asynchronous alternating current motor/generator having an armature winding which includes interspered energy coils (11) and reflux coils (12) which are electrically and inductively isolated from each other, but which are paramutually inductively coupled through the rotor (14). Each reflux coil is positioned at 90 electrical degrees to the adjacent energy coil and is tuned to minimize the inductive reactance of the motor generator.
摘要翻译：一种具有电枢绕组的异步交流电动机/发电机，其包括彼此电感和电感隔离但是通过转子（14）进行辅助电感耦合的交错的能量线圈（11）和回流线圈（12）。每个回流线圈与相邻的能量线圈定位成90度电角，并被调谐以最小化电动发电机的感抗。

3. 发明申请

WO2011106256A2 VERTICAL-AXIS WIND TURBINE HAVING LOGARITHMIC CURVED AIRFOILS 审中-公开
标题翻译：具有对数曲线翼型的垂直轴风力涡轮机
公开(公告)号：WO2011106256A2
公开(公告)日：2011-09-01
申请号：PCT/US2011025441
申请日：2011-02-18
申请人： NOVASTRON CORP , ROBERTS GARY D
发明人： ROBERTS GARY D
IPC分类号： F03D3/06 , F03D3/02 , F03D11/00
CPC分类号： F03D3/02 , F03D3/06 , F05B2200/23 , F05B2250/00 , Y02E10/74
摘要： A vertical-axis, stator-less wind turbine includes a rotor (5) rotatable about a vertical axis. The rotor has a plurality of vertically oriented rotor airfoils (35a-c) disposed circumferentially and with equiangular symmetry about the vertical axis. Each rotor airfoil has a substantially logarithmic curvature with a trailing edge with a trailing edge (82) having a smaller radius of curvature than a leading edge (80), and with the leading edge positioned further from the vertical axis than the trailing edge.
摘要翻译：垂直轴无定子风力涡轮机包括可绕竖直轴线旋转的转子（5）。该转子具有多个垂直定向的转子翼面（35a-c），该转子翼面沿周向设置并且围绕垂直轴线等角对称。每个转子翼型具有基本对数曲率，后缘具有后缘（82），后缘具有比前缘（80）更小的曲率半径，并且前缘比后缘更远离竖直轴线定位。

4. 发明申请

WO2006132923A2 AERODYNAMIC-HYBRID VERTICAL-AXIS WIND TURBINE 审中-公开
公开(公告)号：WO2006132923A2
公开(公告)日：2006-12-14
申请号：PCT/US2006/021289
申请日：2006-06-02
申请人： NOVASTRON CORPORATION , ROBERTS, Gary, D. , ROBERTS, David, W.
发明人： ROBERTS, Gary, D. , ROBERTS, David, W.
IPC分类号： F03D7/06
CPC分类号： F03D3/0409 , F03D3/02 , F03D3/061 , F03D13/20 , F03D80/40 , F03D80/70 , F05B2240/217 , Y02E10/74
摘要： An aerodynamic-hybrid, vertical-axis wind turbine (10) which includes a rotor airfoil (31a-c, 32a-c, 33a-c) and stator blade (21a-e) combination which maximizes energy production by increasing wind velocity and pressure while eliminating back pressure and improving the laminar flow of wind both around and through the device. The rotor airfoils have a horizontal cross-section with a crescent shape including a convex leading side and a concave trailing side with a thicker middle section that tapers to narrower sections at ends. The stator blades have a horizontal cross-section with a planar side and a convex side. Rotor airfoil and stator blade combinations are secured between upper and lower annular sails.
摘要翻译：一种包括转子翼型（31a-c，32a-c，33a-c）和定子叶片（21a-e）的空气动力学混合的垂直轴风力涡轮机（10），其通过增加风速和压力来最大限度地提高能量产生同时消除背压并改善围绕和穿过装置的风的层流。转子翼型件具有水平横截面，其具有新月形形状，包括凸起的前侧和具有较厚中间部分的凹形后侧，其在端部处变窄到较窄的部分。定子叶片具有平面侧和凸侧的水平横截面。转子翼型件和定子叶片组合固定在上下环形帆之间。

5. 发明申请

WO2008156890A3 COMPOSITE CASE ARMOR FOR JET ENGINE FAN CASE CONTAINMENT 审中-公开
公开(公告)号：WO2008156890A3
公开(公告)日：2008-12-24
申请号：PCT/US2008/059092
申请日：2008-04-02
申请人： A & P TECHNOLOGY, INC. , WILLIAMS INTERNATIONAL CO., LLC , THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA) , BRALEY, Michael, Scott , DORER, James, D. , ROBERTS, Gary, D.
发明人： BRALEY, Michael, Scott , DORER, James, D. , ROBERTS, Gary, D.
IPC分类号： F01B25/16
摘要： A gas turbine fan blade containment assembly includes a fan case having an inner surface surrounding a jet engine fan and an outer surface. Mounted on the inner surface and across a blade containing region of the fan case is a load spreader layer for initially receiving a point load from a fan blade release (a "blade-out event"). A band layer is mounted to an outer surface of the fan case for carrying at least a portion of a hoop tensile load on the fan case resulting from the blade-out event, and separator film layer is mounted between the outer surface of the fan case and the band layer to retard the formation of stress concentrations in the band layer. In one embodiment, the load spreader layer includes a plurality of circumferentially-arrayed load spreader layer segments.

6. 发明申请

WO1999029028A1 SELF-EXCITED ASYNCHRONOUS ALTERNATING CURRENT GENERATOR WITH PARAMUTUAL INDUCTIVE COUPLING 审中-公开
标题翻译：具有参数电感耦合的自激式异步交流电流发生器
公开(公告)号：WO1999029028A1
公开(公告)日：1999-06-10
申请号：PCT/US1997023124
申请日：1997-12-04
申请人： ROBERTS, Gary, D.
IPC分类号： H02K17/42
CPC分类号： H02K17/42
摘要： An asynchronous alternating current motor/generator having an armature winding which includes interspered energy coils (11) and reflux coils (12) which are electrically and inductively isolated from each other, but which are paramutually inductively coupled through the rotor (14). Each reflux coil is positioned at 90 electrical degrees to the adjacent energy coil and is tuned to minimize the inductive reactance of the motor generator.
摘要翻译：本发明涉及一种具有感应绕组的异步交流发电机马达，该感应绕组包括插入式能量线圈（11）和回流线圈，这些线圈彼此之间电气地且感应地绝缘，但以这种方式耦合由转子（14）感应和对准。每个回流线圈相对于相邻的能量线圈以90电角度放置，并且被调谐以减小电动发电机的电感性电抗。

7. 发明申请

WO2006132923A3 AERODYNAMIC-HYBRID VERTICAL-AXIS WIND TURBINE 审中-公开
标题翻译： AERODYNAMIC-混合式垂直轴风力涡轮机
公开(公告)号：WO2006132923A3
公开(公告)日：2009-04-23
申请号：PCT/US2006021289
申请日：2006-06-02
申请人： NOVASTRON CORP , ROBERTS GARY D , ROBERTS DAVID W
发明人： ROBERTS GARY D , ROBERTS DAVID W
IPC分类号： H02P9/04 , F03B13/00 , F03B13/12 , F03D9/00
CPC分类号： F03D3/02 , F03D3/061 , F03D80/40 , F05B2240/217 , Y02E10/74
摘要： An aerodynamic-hybrid, vertical-axis wind turbine (10) which includes a rotor airfoil (31a-c, 32a-c, 33a-c) and stator blade (21a-e) combination which maximizes energy production by increasing wind velocity and pressure while eliminating back pressure and improving the laminar flow of wind both around and through the device. The rotor airfoils have a horizontal cross-section with a crescent shape including a convex leading side and a concave trailing side with a thicker middle section that tapers to narrower sections at ends. The stator blades have a horizontal cross-section with a planar side and a convex side. Rotor airfoil and stator blade combinations are secured between upper and lower annular sails.
摘要翻译：包括转子翼型件（31a-c，32a-c，33a-c）和定子叶片（21a-e）的空气动力学混合的垂直轴风力涡轮机（10），其通过增加风速和压力来最大限度地提高能量产生同时消除背压并改善围绕和穿过装置的风的层流。转子翼型件具有水平横截面，其具有新月形形状，其包括凸起的前侧和具有较厚中间部分的凹形后侧，其在端部处变窄到较窄的部分。定子叶片具有平坦的侧面和凸面的水平横截面。转子翼型件和定子叶片组合固定在上下环形帆之间。

8. 发明申请

WO2008156890A2 COMPOSITE CASE ARMOR FOR JET ENGINE FAN CASE CONTAINMENT 审中-公开
标题翻译：用于喷气发动机风箱壳体的复合壳体装甲
公开(公告)号：WO2008156890A2
公开(公告)日：2008-12-24
申请号：PCT/US2008059092
申请日：2008-04-02
申请人： A & P TECHNOLOGY INC , DORER JAMES D , ROBERTS GARY D , BRALEY MICHAEL SCOTT
发明人： DORER JAMES D , ROBERTS GARY D , BRALEY MICHAEL SCOTT
IPC分类号： F02C7/04
CPC分类号： F02C7/05 , F01D21/045 , F05D2300/603 , Y02T50/672
摘要： A gas turbine fan blade containment assembly includes a fan case having an inner surface surrounding a jet engine fan and an outer surface. Mounted on the inner surface and across a blade containing region of the fan case is a load spreader layer for initially receiving a point load from a fan blade release (a "blade-out event"). A band layer is mounted to an outer surface of the fan case for carrying at least a portion of a hoop tensile load on the fan case resulting from the blade-out event, and separator film layer is mounted between the outer surface of the fan case and the band layer to retard the formation of stress concentrations in the band layer. In one embodiment, the load spreader layer includes a plurality of circumferentially-arrayed load spreader layer segments.
摘要翻译：燃气轮机风扇叶片容纳组件包括具有围绕喷气发动机风扇和外表面的内表面的风扇壳体。安装在内表面上并且跨过风扇壳体的刀片容纳区域是用于最初从风扇叶片释放（“刮刀事件”）接收点负载的负载撒布层。带状层安装在风扇壳体的外表面上，用于承载由刮板输出事件导致的风扇壳体上的环向拉伸载荷的至少一部分，并且分离膜层安装在风扇壳体的外表面之间和带状层，以延缓带状层中应力集中的形成。在一个实施例中，负载撒布层包括多个周向排列的负载扩展层分段。

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