公开(公告)号：US20120020806A1

公开(公告)日：2012-01-26

申请号：US13171561

申请日：2011-06-29

申请人： Patrick GIRARD ,  Olivier Kueny ,  Renaud Martet ,  Renaud Royan

发明人： Patrick GIRARD ,  Olivier Kueny ,  Renaud Martet ,  Renaud Royan

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F01D9/041 ,  F05D2220/321 ,  F05D2220/3215 ,  F05D2240/121 ,  F05D2240/303 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane PO situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓的底部的第一参考平面PO所考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US08734113B2

公开(公告)日：2014-05-27

申请号：US13171561

申请日：2011-06-29

申请人： Patrick Girard ,  Olivier Kueny ,  Renaud Martet ,  Renaud Royan

发明人： Patrick Girard ,  Olivier Kueny ,  Renaud Martet ,  Renaud Royan

IPC分类号： F01D9/02 ,  F01D9/04

CPC分类号： F01D5/141 ,  F01D9/041 ,  F05D2220/321 ,  F05D2220/3215 ,  F05D2240/121 ,  F05D2240/303 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US20120051931A1

公开(公告)日：2012-03-01

申请号：US13171734

申请日：2011-06-29

申请人： Jean BLEUZEN ,  Renaud Martet ,  Pascal Routier ,  Renaud Royan

发明人： Jean BLEUZEN ,  Renaud Martet ,  Pascal Routier ,  Renaud Royan

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2250/74 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US08672635B2

公开(公告)日：2014-03-18

申请号：US13171734

申请日：2011-06-29

申请人： Jean Bleuzen ,  Renaud Martet ,  Pascal Routier ,  Renaud Royan

发明人： Jean Bleuzen ,  Renaud Martet ,  Pascal Routier ,  Renaud Royan

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2250/74 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US20120051895A1

公开(公告)日：2012-03-01

申请号：US13171653

申请日：2011-06-29

申请人： Jean-Michel GUIMBARD ,  Pierre Marche ,  Renaud Martet ,  Renaud Royan

发明人： Jean-Michel GUIMBARD ,  Pierre Marche ,  Renaud Martet ,  Renaud Royan

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2220/3213 ,  F05D2240/12 ,  F05D2250/74 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US08734096B2

公开(公告)日：2014-05-27

申请号：US13171653

申请日：2011-06-29

申请人： Jean-Michel Guimbard ,  Pierre Marche ,  Renaud Martet ,  Renaud Royan

发明人： Jean-Michel Guimbard ,  Pierre Marche ,  Renaud Martet ,  Renaud Royan

IPC分类号： F01D9/02

CPC分类号： F01D5/141 ,  F05D2220/3213 ,  F05D2240/12 ,  F05D2250/74 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US20120020799A1

公开(公告)日：2012-01-26

申请号：US13170225

申请日：2011-06-28

申请人： Jean BLEUZEN ,  Jean-Michel Guimbard ,  Pierre Marche ,  Renaud Martet

发明人： Jean BLEUZEN ,  Jean-Michel Guimbard ,  Pierre Marche ,  Renaud Martet

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2250/74 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US20080184694A1

公开(公告)日：2008-08-07

申请号：US12026033

申请日：2008-02-05

申请人： Jean-Michel Bernard Guimbard ,  Renaud Martet ,  Eric Schwartz

发明人： Jean-Michel Bernard Guimbard ,  Renaud Martet ,  Eric Schwartz

IPC分类号： F02K3/02

CPC分类号： F02K3/072 ,  F01D1/26 ,  F02C3/067 ,  F05D2240/12 ,  Y02T50/671

摘要： A gas turbine with contrarotating HP and LP turbines comprises an LP turbine having a plurality of moving wheels alternating with nozzles, the moving wheels of the LP turbine rotating in a direction opposite to the direction of rotation of the moving wheel of the HP turbine, and an inter-turbine casing having inner and outer casing walls defining a stream passage between the HP and LP turbines together with arms extending across the passage between the inner and outer casing walls. The gas turbine does not have a nozzle or device for forming the function of deflecting the stream between the outlet from the HP turbine and the first moving wheel of the LP turbine. The HP turbine is advantageously designed to deliver a stream that gyrates in the inter-turbine casing.

摘要翻译： 具有相反HP和LP涡轮机的燃气轮机包括具有与喷嘴交替的多个移动轮的LP涡轮机，LP涡轮机的移动轮沿与HP涡轮机的移动轮的旋转方向相反的方向旋转，以及 涡轮机外壳具有内壳体外壳壁和外壳体壁，其在HP和LP涡轮机之间限定流动通道以及跨过内壳壁和外壳壁之间的通道延伸的臂。 燃气轮机不具有用于形成在HP涡轮机的出口与LP涡轮机的第一移动轮之间偏转流的功能的喷嘴或装置。 HP涡轮机有利地设计成输送在涡轮机外壳内旋转的流。

公开(公告)号：US08734115B2

公开(公告)日：2014-05-27

申请号：US13170225

申请日：2011-06-28

申请人： Jean Bleuzen ,  Jean-Michel Guimbard ,  Pierre Marche ,  Renaud Martet

发明人： Jean Bleuzen ,  Jean-Michel Guimbard ,  Pierre Marche ,  Renaud Martet

IPC分类号： F01D9/02 ,  F01D5/12

CPC分类号： F01D5/141 ,  F05D2250/74 ,  Y02T50/673

摘要： When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the Cartesian coordinates X,Y,Z′ given in Table 1, in which the coordinate Z′ is the quotient D/H where D is the distance of the point under consideration from a first reference plane P0 situated at the base of the nominal profile, and H is the height of said profile measured from the first reference plane to a second reference plane P1. The measurements D and H are taken radially relative to the axis of the turbine, while the X coordinate is measured in the axial direction of the turbine.

摘要翻译： 当冷和处于非涂覆状态时，空气动力学特性与由表1中给出的笛卡尔坐标X，Y，Z'确定的标称轮廓基本相同，其中坐标Z'是商D / H，其中D 是从位于标称轮廓底部的第一参考平面P0考虑的点的距离，H是从第一参考平面测量到第二参考平面P1的所述剖面的高度。 测量D和H相对于涡轮机的轴线径向地获得，而X坐标是在涡轮的轴向方向上测量的。

公开(公告)号：US08128375B2

公开(公告)日：2012-03-06

申请号：US12333969

申请日：2008-12-12

申请人： Patrick Joseph Marie Girard ,  Jean-Claude Marcel Auguste Hanny ,  Renaud Martet ,  Olivier Charles Henri Massy ,  Philippe Jean-Pierre Pabion ,  Stephanie Dominique Roger

发明人： Patrick Joseph Marie Girard ,  Jean-Claude Marcel Auguste Hanny ,  Renaud Martet ,  Olivier Charles Henri Massy ,  Philippe Jean-Pierre Pabion ,  Stephanie Dominique Roger

IPC分类号： B63H1/26

CPC分类号： F01D5/147 ,  B22D27/045 ,  F01D5/141 ,  F05D2240/121 ,  F05D2240/303 ,  F05D2300/607

摘要： The monocrystalline turbomachine blade according to the invention that is cast and directionally solidified, is disclosed. The blade includes an airfoil with a leading edge, a pressure face, a suction face, a trailing edge, a skeleton and having a longitudinal axis, the faces and having a neck line, respectively a pressure face neck and a suction face neck relative to the adjacent blade in the turbomachine rotor of which it forms an element; an endpiece of the airfoil, such as a heel or a platform, having an airfoil end face, on the stream side, forming an angle with the axis ZZ; and a connection zone between the airfoil and the airfoil end face. The connection zone forms a fattening of the airfoil. The connection zone extends about the leading edge between a point P1 situated on the suction face of the airfoil upstream of the suction face neck and a point P3 situated on the pressure face of the airfoil upstream of the pressure face neck.

摘要翻译： 公开了铸造和定向凝固的根据本发明的单晶涡轮机叶片。 叶片包括具有前缘的翼型，压力面，吸力面，后缘，骨架并具有纵向轴线，所述面部分别具有颈部线，压力面颈部和吸力面颈部相对于 涡轮机转子中相邻的叶片形成一个元件; 在流动侧，具有与轴线ZZ形成角度的翼型件（例如脚跟或平台）的端部具有翼型端面， 以及翼型件和翼型件端面之间的连接区域。 连接区形成机翼的育肥。 连接区域围绕位于吸力面颈部上游的翼型件的吸力面上的点P1和位于压力面颈上游的翼型件的压力面上的点P3之间的前缘延伸。