专利检索 ap:"Peter Gaines" 第 1 页

1.

发明申请
RESPONSIVE CELL CULTURE HYDROGEL 有权
标题翻译：反应性细胞培养物HYDROGEL

公开(公告)号：US20130337566A1

公开(公告)日：2013-12-19

申请号：US13976645

申请日：2011-12-30

申请人： Daniel Schmidt , Emmanuelle Reynaud , Peter Gaines

发明人： Daniel Schmidt , Emmanuelle Reynaud , Peter Gaines

IPC分类号： C12N5/00

CPC分类号： C12N5/0018 , C08J3/075 , C08J2371/02 , C08J2379/02 , C08J2379/04 , C08J2383/08 , C12N5/0068 , C12N2533/30

摘要： The present invention provides devices, compositions and methods for maintaining conditions in a cell culture and for measurement of conditions in the cell culture. In particular, the invention provides hydrogel materials, apparatus and methods for several non-invasive techniques of maintaining optimal or near-optimal nutrient and pH levels in cell cultures.

摘要翻译： 本发明提供用于维持细胞培养条件和用于测量细胞培养物中条件的装置，组合物和方法。特别地，本发明提供用于在细胞培养物中保持最佳或接近最佳营养物和pH水平的几种非侵入性技术的水凝胶材料，装置和方法。

2.

发明授权
Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration 有权
标题翻译：外围冷却涡轮机翼型冷却孔的位置，风格及配置

公开(公告)号：US06923623B2

公开(公告)日：2005-08-02

申请号：US10635435

申请日：2003-08-07

申请人： Peter Gaines Cleveland , Thomas Bradley Beddard

发明人： Peter Gaines Cleveland , Thomas Bradley Beddard

IPC分类号： F01D5/18 , F01D5/20

CPC分类号： F01D5/20 , F01D5/141 , F01D5/187 , F05D2260/22141 , Y10S416/02

摘要： A turbine stage one bucket has an airfoil having a plurality of cooling holes passing through the airfoil from 0% span to 100% span whereby cooling air exits the airfoil tip into the hot gas path. X and Y coordinate values are given in Table I, locating the holes relative to the airfoil profile at airfoil profile sections of 5%, 50% and 90% span, Table I also giving the hole diameters. In this manner, cooling hole optimization for this turbine bucket airfoil is achieved. The cooling holes are also located in relation to the profile of the bucket airfoil given by the X, Y and Z coordinate values of Table II, the two coordinate systems having the same origin.

摘要翻译： 涡轮级一桶具有翼型，其具有多个冷却孔，其通过翼型从0％跨度到100％跨度，由此冷却空气从翼型端口进入热气路径。 X和Y坐标值在表I中给出，在5％，50％和90％跨度的翼型剖面上将孔相对于翼型轮廓定位，表I还给出了孔直径。以这种方式，实现了该涡轮机桶翼型件的冷却孔优化。冷却孔也相对于由表II的X，Y和Z坐标值给出的铲斗翼型的轮廓定位，两个坐标系具有相同的起点。

3.

发明授权
Conical tip shroud fillet for a turbine bucket 有权
标题翻译：涡轮桶锥形尖端护罩圆角
公开(公告)号：US07063509B2

公开(公告)日：2006-06-20

申请号：US10655623

申请日：2003-09-05

申请人： Daniel David Snook , Peter Gaines Cleveland

发明人： Daniel David Snook , Peter Gaines Cleveland

IPC分类号： B63H1/16

CPC分类号： F01D5/225 , F01D5/141 , F05D2250/14 , F05D2250/16 , F05D2250/17 , F05D2250/232 , F05D2250/70 , F05D2250/74

摘要： A turbine bucket airfoil has a conical fillet about the intersection of the airfoil tip and tip shroud having a nominal profile in accordance with coordinate values of X and Y, offset 1, offset 2 and Rho set forth in Table I. The shape parameters of offset 1, offset 2 and Rho define the configuration of the fillet at the specified X and Y locations about the fillet to provide a fillet configuration accommodating high localized stresses. The fillet shape may be parabolic, elliptical or hyperbolic as a function of the value of the shape parameter ratio of D1 D1 + D2 at each X, Y location where D1 is a distance between an intermediate point along a chord between edge points determined by offsets O1 and O2 and a shoulder point on the fillet surface and D2 is a distance between the shoulder point and an apex location at the intersection of the airfoil tip and tip shroud.

摘要翻译： 涡轮叶片翼型件根据X和Y，偏移1，偏移2和Rho的坐标值，具有围绕翼型尖端和尖端护罩的相交处的圆锥形圆角，其具有标称轮廓。偏移量的形状参数 1，偏移2和Rho定义圆角上指定的X和Y位置处的圆角的配置，以提供适应高局部应力的圆角配置。根据 $\frac{的形状参数比值的函数，圆角形状可以是抛物线形，椭圆形或双曲线}{D1D1+D24. 发明授权 Airfoil shape for a turbine bucket 有权标题翻译：涡轮叶片的翼型公开(公告)号： US06857855B1 公开(公告)日： 2005-02-22 申请号： US10632853 申请日： 2003-08-04 申请人： Daniel David Snook, Robert Romany By, Bruce Loren Smith, Gunnar Leif Siden, Carlos Alberto Collado, Peter Gaines Cleveland 发明人： Daniel David Snook, Robert Romany By, Bruce Loren Smith, Gunnar Leif Siden, Carlos Alberto Collado, Peter Gaines Cleveland IPC分类号： F01D5/14 CPC分类号： F01D5/141, Y10S416/02 摘要： Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0.03 span to 0.95 span convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form the bucket airfoil shape. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelop of \pm0.150 inches in directions normal to the surface of the airfoil. 摘要翻译：第三级涡轮机叶片具有基本上符合X，Y和Z的笛卡尔坐标值的翼型轮廓，其中X和Y值表示在表I中，其中X和Y值以英寸为单位，Z值是从0.03跨度到0.95跨度可变为Z的无量纲值通过将Z值乘以翼型件的高度（英寸），以英寸为单位。 X和Y值是通过平滑连续的弧连接时定义每个距离Z处的翼型轮廓部分的距离。每个距离Z处的轮廓部分彼此平滑地连接以形成铲斗翼型形状。 X，Y和Z距离可以作为相同常数或数字的函数来缩放，以提供用于铲斗的放大或缩小的翼型部分。由X，Y和Z距离给出的额定翼型在垂直于翼面表面的方向上在\pm0.150英寸的范围内。5. 发明授权 Airfoil shape for a turbine bucket 有权标题翻译：涡轮叶片的翼型公开(公告)号： US06769879B1 公开(公告)日： 2004-08-03 申请号： US10616911 申请日： 2003-07-11 申请人： Peter Gaines Cleveland, Thomas Bradley Beddard, Scott Matthew Sparks, Joseph Anthony Weber, James Bernard Fehlberg 发明人： Peter Gaines Cleveland, Thomas Bradley Beddard, Scott Matthew Sparks, Joseph Anthony Weber, James Bernard Fehlberg IPC分类号： F01D514 CPC分类号： F01D5/141, F01D5/187, F05D2250/70, F05D2260/202, Y02T50/673, Y02T50/676, Y10S416/02 摘要： First stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0.05 span to 0.95 span convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelope of \pm0.150 inches in directions normal to the surface of the airfoil. 摘要翻译：第一级涡轮机叶片具有基本上符合X，Y和Z的笛卡尔坐标值的翼型轮廓，其中X和Y值为英寸，Z值为0.05跨度至0.95跨度的无量纲值，可转换为Z 通过将Z值乘以翼型件的高度（英寸），以英寸为单位。 X和Y值是通过平滑连续弧连接时定义每个距离Z处的翼型轮廓部分的距离。每个距离Z处的轮廓部分彼此平滑地连接以形成完整的翼型形状。 X，Y和Z距离可以作为相同常数或数字的函数来缩放，以提供用于铲斗的放大或缩小的翼型部分。由X，Y和Z距离给出的标称翼型在垂直于翼面表面的方向上在\pm0.150英寸的范围内。6. 发明授权 Turbine bucket tip shroud edge profile 有权标题翻译：涡轮斗尖护罩边缘型材公开(公告)号： US06893216B2 公开(公告)日： 2005-05-17 申请号： US10620365 申请日： 2003-07-17 申请人： Daniel David Snook, Peter Gaines Cleveland 发明人： Daniel David Snook, Peter Gaines Cleveland IPC分类号： F01D5/14, F01D5/20, F01D5/22, F01B11/08 CPC分类号： F01D5/225, F05D2250/70 摘要： A turbine bucket includes a bucket airfoil having a tip shroud with leading and trailing edges defining leading and trailing edge profiles substantially in accordance with Cartesian coordinate values of X and Y at points 12-20 and 1-11, respectively, set forth in Table I. The X and Y values are distances in inches which, when respective points 12-20 and 1-11 are connected by smooth, continuing arcs, define the leading and trailing edge tip shroud profiles. An airfoil profile at 95% span is defined by Cartesian coordinate values of X, Y and Z in Table II having the same X, Y origin along the radial Z axis as the origin of Table I. The profiled leading and trailing edges of the tip shroud relative to the airfoil profile afford optimum tip shroud mass distribution which maximizes creep life of the bucket. Stage efficiency is also improved by providing a tip shroud covering the airfoil throat. 摘要翻译：涡轮机桶包括具有尖端护罩的铲斗翼型件，其前缘和后缘基本上根据表I中所示的点12-20和1-11处的X和Y的笛卡尔坐标值来定义前缘和后缘轮廓 X和Y值是以英寸为单位的距离，当各个点12-20和1-11通过平滑连续的弧连接时，可以定义前缘和后缘尖端护罩轮廓。 95％跨度的翼型轮廓由表II中的X，Y和Z的笛卡尔坐标值定义为具有相同的X，Y原点沿着径向Z轴作为表I的原点。尖端的成型前缘和后缘相对于翼型轮廓的护罩提供最佳的尖端护罩质量分布，其最大化铲斗的蠕变寿命。通过提供覆盖翼型喉部的尖端护罩也提高了阶段效率。7. 发明授权 Responsive cell culture hydrogel 有权标题翻译：响应性细胞培养水凝胶公开(公告)号： US09506029B2 公开(公告)日： 2016-11-29 申请号： US13976645 申请日： 2011-12-30 申请人： Daniel Schmidt, Emmanuelle Reynaud, Peter Gaines 发明人： Daniel Schmidt, Emmanuelle Reynaud, Peter Gaines IPC分类号： C12N5/00, C08J3/075 CPC分类号： C12N5/0018, C08J3/075, C08J2371/02, C08J2379/02, C08J2379/04, C08J2383/08, C12N5/0068, C12N2533/30 摘要： The present invention provides devices, compositions and methods for maintaining conditions in a cell culture and for measurement of conditions in the cell culture. In particular, the invention provides hydrogel materials, apparatus and methods for several non-invasive techniques of maintaining optimal or near-optimal nutrient and pH levels in cell cultures. 摘要翻译：本发明提供用于维持细胞培养条件和用于测量细胞培养物中条件的装置，组合物和方法。特别地，本发明提供用于在细胞培养物中保持最佳或接近最佳营养物和pH水平的几种非侵入性技术的水凝胶材料，装置和方法。8. 发明授权 Air foil shape for a compressor blade 失效标题翻译：用于压缩机叶片的气翼形状公开(公告)号： US07186090B2 公开(公告)日： 2007-03-06 申请号： US10986162 申请日： 2004-11-12 申请人： Steven Eric Tomberg, Roger Beharrysingh, Timothy E. DeJoris, William J. Miller, Paul Deivernois, Venkata Siva P. Chaluvadi, Adrian Mircea Mistreanu, Michael James Dutka, Nathan S. Race, Jeffrey Boyd, Christopher David McGowan, Peter Gaines Cleveland, Jason Thomas Harrell, Carl G. Schott, John David Stampfli, Ronald Stuart Denmark, Steven Mark Schirle, Jennifer B. Michenfelder, John F. Ryman 发明人： Steven Eric Tomberg, Roger Beharrysingh, Timothy E. DeJoris, William J. Miller, Paul Deivernois, Venkata Siva P. Chaluvadi, Adrian Mircea Mistreanu, Michael James Dutka, Nathan S. Race, Jeffrey Boyd, Christopher David McGowan, Peter Gaines Cleveland, Jason Thomas Harrell, Carl G. Schott, John David Stampfli, Ronald Stuart Denmark, Steven Mark Schirle, Jennifer B. Michenfelder, John F. Ryman IPC分类号： F01D5/14 CPC分类号： F01D5/141, F05D2240/301, Y10S416/02, Y10S416/05 摘要： An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a table. The table selected from the group of tables consisting of TABLES 1S-16S, 1R-17R, and IGV. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape. 摘要翻译：一种具有基本上符合表中列出的X，Y和Z的笛卡尔坐标值的公称轮廓的制品。该表从由表1S-16S，1R-17R和IGV组成的表格中选择。其中X和Y是以英寸为单位的距离，当通过平滑连续的弧连接时，以每英寸的距离Z限定翼型轮廓部分。 Z距离处的轮廓部分彼此平滑地连接以形成完整的翼型形状。PDF内容加载中...$(document).ready(function() {
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