公开(公告)号：US08079817B2

公开(公告)日：2011-12-20

申请号：US10774399

申请日：2004-02-10

申请人： Benjamin Arnette Lagrange ,  Timothy Brian Lloyd

发明人： Benjamin Arnette Lagrange ,  Timothy Brian Lloyd

IPC分类号： F01D5/30

CPC分类号： F01D5/3007 ,  F05D2220/321 ,  F05D2220/3213

摘要： A turbine bucket and wheelpost assembly reduces the number of buckets in the third stage of the turbine from ninety-two to ninety while reducing stresses at the assembly points of the buckets and wheelposts. The buckets and wheelposts are formed with complementary fillets and tangs that provide for the insertion of the bucket into the broach slot between two wheelposts. The angles of the fillets on both the bucket and wheelpost range from 50° to 59°. The upper surface of the wheelpost is scalloped to reduce weight and the tangs and fillets of both the bucket and wheelpost are formed from curved and straight surfaces to reduce stresses on the assembly.

摘要翻译： 涡轮机桶和轮胎组件将涡轮机第三级的铲斗数量从九十二减少到九十，同时减少了在铲斗和轮轨的装配点处的应力。 铲斗和轮辋形成有互补的鱼片和脚趾，其用于将桶插入两个车轮柱之间的拉刀槽中。 铲斗和轮辋两侧的鱼角角度范围为50°至59°。 轮辋的上表面是扇形的，以减轻重量，铲斗和轮辋的柄脚和圆角由弯曲和直的表面形成，以减少组件上的应力。

公开(公告)号：US07905709B2

公开(公告)日：2011-03-15

申请号：US10774400

申请日：2004-02-10

申请人： Benjamin Arnette Lagrange ,  Timothy Brian Lloyd

发明人： Benjamin Arnette Lagrange ,  Timothy Brian Lloyd

IPC分类号： F01D5/30

CPC分类号： F01D5/3007 ,  F05D2250/70 ,  F05D2260/94 ,  F05D2260/941

摘要： A turbine bucket and wheelpost assembly reduces the number of buckets in at least one of the stages of the turbine from 92 to 60 while reducing stresses at the assembly points of the buckets and wheelposts. The buckets and wheelposts being formed with complementary fillets and tangs that provide for the insertion of the bucket into the broach slot between two wheelposts. The angles of the tang surfaces on both the bucket and wheelpost range from 50° to 57°. The upper surface of the wheelpost is scalloped to reduce weight and the tangs and fillets of both the bucket and wheelpost are formed from curved and straight surfaces to reduce stresses on the assembly.

摘要翻译： 涡轮机桶和轮辋组件将涡轮机的至少一个级中的铲斗数量从92减少到60，同时减小了在铲斗和轮辋的组装点处的应力。 铲斗和轮辋形成有互补的圆角和柄脚，其用于将铲斗插入两个车轮柱之间的拉刀槽中。 铲斗和车轮柱两侧的铲斗表面的角度范围为50°至57°。 轮辋的上表面是扇形的，以减轻重量，铲斗和轮辋的柄脚和圆角由弯曲和直的表面形成，以减少组件上的应力。

公开(公告)号：US06779977B2

公开(公告)日：2004-08-24

申请号：US10320655

申请日：2002-12-17

申请人： Benjamin Arnette Lagrange ,  Edward Lee McGrath ,  James Bernard Fehlberg ,  Anthony Aaron Chiurato

发明人： Benjamin Arnette Lagrange ,  Edward Lee McGrath ,  James Bernard Fehlberg ,  Anthony Aaron Chiurato

IPC分类号： F01D514

CPC分类号： F01D5/142 ,  F05D2220/3213 ,  F05D2250/74 ,  Y10S416/02

摘要： Second 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 to 1 convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. 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 ±0.160 inches in directions normal to the surface of the airfoil.

摘要翻译： 第二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值为从0到1的可转换为Z距离的无量纲值 将Z值乘以翼型件的高度（英寸）。 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±0.160英寸的范围内。

公开(公告)号：US07534090B2

公开(公告)日：2009-05-19

申请号：US11423795

申请日：2006-06-13

申请人： Randall Richard Good ,  Benjamin Arnette Lagrange ,  Gary Charles Liotta ,  James William Vehr ,  Jonathan David Crim ,  Stephen Paul Wassynger ,  Anthony Aaron Chiurato

发明人： Randall Richard Good ,  Benjamin Arnette Lagrange ,  Gary Charles Liotta ,  James William Vehr ,  Jonathan David Crim ,  Stephen Paul Wassynger ,  Anthony Aaron Chiurato

IPC分类号： F01D5/26

CPC分类号： F01D5/22 ,  F01D5/10 ,  F01D5/26 ,  F05D2240/80 ,  F05D2260/96

摘要： An enhanced damping system for a turbine bucket. The damping system includes a damper pocket and a damper pin with an offset center of gravity positioned within the damper pocket.

摘要翻译： 一种用于涡轮机桶的增强型阻尼系统。 阻尼系统包括阻尼器袋和阻尼器销，偏置重心位于阻尼口袋内。

公开(公告)号：US20070286734A1

公开(公告)日：2007-12-13

申请号：US11423789

申请日：2006-06-13

申请人： Benjamin Arnette Lagrange ,  Randall Richard Good ,  Gary Charles Liotta ,  Jon Robert DeLong ,  Matthew Durham Collier ,  James William Vehr

发明人： Benjamin Arnette Lagrange ,  Randall Richard Good ,  Gary Charles Liotta ,  Jon Robert DeLong ,  Matthew Durham Collier ,  James William Vehr

IPC分类号： F03B3/12

CPC分类号： F01D5/22 ,  F05D2240/80 ,  F05D2250/70 ,  Y10S416/50

摘要： A damping system for a turbin bucket. The damping system includes a damper pocket with a variable tangential depth and a damper pin positional within the damper pocket.

摘要翻译： 用于涡轮桶的阻尼系统。 阻尼系统包括具有可变切向深度的阻尼口袋和位于阻尼口袋内的阻尼器销。

公开(公告)号：US06966756B2

公开(公告)日：2005-11-22

申请号：US10753341

申请日：2004-01-09

申请人： Edward Lee McGrath ,  Benjamin Arnette Lagrange

发明人： Edward Lee McGrath ,  Benjamin Arnette Lagrange

IPC分类号： F01D5/18

CPC分类号： F01D5/187

摘要： A turbine bucket comprising an airfoil portion, a shank portion and a dovetail mounting portion; an internal cooling circuit including inlet passages in the shank portion and the dovetail mounting portion connected to a cooling circuit in the airfoil portion, the inlet passages including a primary inlet passage on one side of a radial centerline of the bucket, and a secondary inlet cavity on an opposite side of the radial centerline; and a purge passage connecting the secondary inlet passage to the primary inlet passage.

公开(公告)号：US06739838B1

公开(公告)日：2004-05-25

申请号：US10388476

申请日：2003-03-17

申请人： Craig Allen Bielek ,  Robert Alan Brittingham ,  Jeff Brian Thompson ,  Benjamin Arnette Lagrange ,  Robert Walter Coign

发明人： Craig Allen Bielek ,  Robert Alan Brittingham ,  Jeff Brian Thompson ,  Benjamin Arnette Lagrange ,  Robert Walter Coign

IPC分类号： F01D514

CPC分类号： F01D5/141 ,  F01D5/225 ,  F05D2240/301 ,  F05D2240/80 ,  Y10S416/05

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 to 1 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 envelop of ±0.060 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的笛卡尔坐标值的机翼型材，其中X和Y值为英寸，Z值为从0到1的可转换为Z距离的无量纲值 将Z值乘以翼型件的高度（英寸）。 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距离给出的额定翼型在垂直于翼面表面的方向上处于±0.060英寸的包络内。

公开(公告)号：US07731483B2

公开(公告)日：2010-06-08

申请号：US11882373

申请日：2007-08-01

申请人： Jon Robert DeLong ,  Craig Allen Bielek ,  Tommy Dee Hayes ,  Benjamin Arnette Lagrange ,  Scott F. Johnson

发明人： Jon Robert DeLong ,  Craig Allen Bielek ,  Tommy Dee Hayes ,  Benjamin Arnette Lagrange ,  Scott F. Johnson

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2250/74 ,  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 to 1 convertible to Z distances in inches by multiplying the Z′ values by the height of the airfoil in inches and adding the radius of the airfoil base. 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 +/−0.0.060 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按照X表示的X，Y和Z'的笛卡尔坐标值的翼型，其中X和Y值以英寸计，Z'值是从0到1可转换为Z的无量纲值 通过将Z'值乘以翼型件的高度（英寸）并增加翼型件底座的半径，以英寸为单位的距离。 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距离给出的额定翼型在垂直于翼面表面的方向上在+/- 0.0.060英寸的包络内。

公开(公告)号：US07731482B2

公开(公告)日：2010-06-08

申请号：US11423789

申请日：2006-06-13

申请人： Benjamin Arnette Lagrange ,  Randall Richard Good ,  Gary Charles Liotta ,  Jon Robert DeLong ,  Matthew Durham Collier ,  James William Vehr ,  Anthony Aaron Chiurato

发明人： Benjamin Arnette Lagrange ,  Randall Richard Good ,  Gary Charles Liotta ,  Jon Robert DeLong ,  Matthew Durham Collier ,  James William Vehr ,  Anthony Aaron Chiurato

IPC分类号： F01D5/26

CPC分类号： F01D5/22 ,  F05D2240/80 ,  F05D2250/70 ,  Y10S416/50

摘要： A damping system for a turbine bucket. The damping system includes a damper pocket with a variable tangential depth and a damper pin positional within the damper pocket.

摘要翻译： 一种涡轮叶片的阻尼系统。 阻尼系统包括具有可变切向深度的阻尼口袋和位于阻尼口袋内的阻尼器销。

公开(公告)号：US20090035145A1

公开(公告)日：2009-02-05

申请号：US11882373

申请日：2007-08-01

申请人： Jon Robert DeLong ,  Craig Allen Bielek ,  Tommy Dee Hayes ,  Benjamin Arnette Lagrange ,  Scott F. Johnson

发明人： Jon Robert DeLong ,  Craig Allen Bielek ,  Tommy Dee Hayes ,  Benjamin Arnette Lagrange ,  Scott F. Johnson

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2250/74 ,  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 to 1 convertible to Z distances in inches by multiplying the Z′ values by the height of the airfoil in inches and adding the radius of the airfoil base. 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 ±0.0.060 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按照X表示的X，Y和Z'的笛卡尔坐标值的翼型，其中X和Y值以英寸计，Z'值是从0到1可转换为Z的无量纲值 通过将Z'值乘以翼型件的高度（英寸）并增加翼型件底座的半径，以英寸为单位的距离。 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，以提供铲斗的按比例放大或缩小的翼型部分。 由X，Y和Z距离给出的额定翼型位于垂直于翼面表面方向的±0.0.060英寸的包络内。