公开(公告)号：EP2841711A4

公开(公告)日：2016-06-01

申请号：EP13796983

申请日：2013-03-12

Applicant: UNITED TECHNOLOGIES CORP ,  LEVINE JEFFREY R ,  BEATTIE JEFFREY S ,  STADDON MALCOLM C

Inventor： LEVINE JEFFREY R ,  BEATTIE JEFFREY S ,  STADDON MALCOLM C

IPC: F01D5/18 ,  B22C9/10 ,  F02C7/00 ,  F02C7/18

CPC classification number: F01D5/188 ,  B22C9/103 ,  B22C9/108 ,  F01D5/187 ,  F05D2200/33 ,  F05D2230/211 ,  F05D2260/22141 ,  F05D2260/607 ,  F05D2300/13 ,  Y02E10/721

Abstract: An airfoil includes a body. The body includes leading and trailing edges adjoining pressure and suction sides to provide an exterior airfoil surface. First and second cooling passages extend in a radial direction from a root to a tip. The first cooling passage includes a tip flag passage that is radially inboard from the tip and extends in a chord-wise direction to a first end that penetrates the trailing edge. The second cooling passage includes a second end terminates adjacent the tip flag passage and a dirt purge passage interconnects the second end to the tip flag passage. A core for making the airfoil is also disclosed.

公开(公告)号：EP2841711A2

公开(公告)日：2015-03-04

申请号：EP13796983.8

申请日：2013-03-12

Applicant: United Technologies Corporation ,  Levine, Jeffrey R. ,  Beattie, Jeffrey S. ,  Staddon, Malcolm C.

Inventor： LEVINE, Jeffrey, R. ,  BEATTIE, Jeffrey, S. ,  STADDON, Malcolm, C.

IPC: F01D5/18 ,  F02C7/18 ,  F02C7/00

CPC classification number: F01D5/188 ,  B22C9/103 ,  B22C9/108 ,  F01D5/187 ,  F05D2200/33 ,  F05D2230/211 ,  F05D2260/22141 ,  F05D2260/607 ,  F05D2300/13 ,  Y02E10/721

Abstract: An airfoil includes a body. The body includes leading and trailing edges adjoining pressure and suction sides to provide an exterior airfoil surface. First and second cooling passages extend in a radial direction from a root to a tip. The first cooling passage includes a tip flag passage that is radially inboard from the tip and extends in a chord-wise direction to a first end that penetrates the trailing edge. The second cooling passage includes a second end terminates adjacent the tip flag passage and a dirt purge passage interconnects the second end to the tip flag passage. A core for making the airfoil is also disclosed.

Abstract translation: 翼型具有主体，该主体包括邻接压力侧和吸力侧以提供外部翼型表面的前缘和后缘。 冷却通道沿径向从根部延伸到尖端。 后缘冷却通道将冷却通道互连到后缘。 后缘冷却通道包括不同尺寸的第一和第二基座，所述第一和第二基座以相对于相同尺寸的基座和相对于不同尺寸基座的重复图案布置。

公开(公告)号：WO2013180792A3

公开(公告)日：2014-02-13

申请号：PCT/US2013030332

申请日：2013-03-12

Applicant: UNITED TECHNOLOGIES CORP ,  LEVINE JEFFREY R ,  BEATTIE JEFFREY S ,  STADDON MALCOLM C

Inventor： LEVINE JEFFREY R ,  BEATTIE JEFFREY S ,  STADDON MALCOLM C

IPC: F01D5/18 ,  F02C7/00 ,  F02C7/18

CPC classification number: F01D5/188 ,  B22C9/103 ,  B22C9/108 ,  F01D5/187 ,  F05D2200/33 ,  F05D2230/211 ,  F05D2260/22141 ,  F05D2260/607 ,  F05D2300/13 ,  Y02E10/721

Abstract: An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.

Abstract translation: 机翼具有主体，其包括邻接压力侧和吸力侧的前缘和后缘，以提供外部翼型表面。 冷却通道在径向方向上从根部延伸到尖端。 后缘冷却通道将冷却通道与后缘相互连接。 后缘冷却通道包括不同尺寸的第一和第二基座，其相对于具有相同尺寸的基座并且相对于不同尺寸的基座以重复图案布置。

公开(公告)号：WO2013180792A2

公开(公告)日：2013-12-05

申请号：PCT/US2013/030332

申请日：2013-03-12

Applicant: UNITED TECHNOLOGIES CORPORATION ,  LEVINE, Jeffrey, R. ,  BEATTIE, Jeffrey, S. ,  STADDON, Malcolm, C.

Inventor： LEVINE, Jeffrey, R. ,  BEATTIE, Jeffrey, S. ,  STADDON, Malcolm, C.

IPC: F01D5/18 ,  F02C7/18 ,  F02C7/00

CPC classification number: F01D5/188 ,  B22C9/103 ,  B22C9/108 ,  F01D5/187 ,  F05D2200/33 ,  F05D2230/211 ,  F05D2260/22141 ,  F05D2260/607 ,  F05D2300/13 ,  Y02E10/721

Abstract: An airfoil has a body that includes leading and trailing edges that adjoin pressure and suction sides to provide an exterior airfoil surface. A cooling passage extends in a radial direction from a root to a tip. A trailing edge cooling passage interconnects the cooling passage to the trailing edge. The trailing edge cooling passage includes first and second pedestals of different sizes that are arranged in a repeating pattern with respect to pedestals of the same size and with respect to pedestals of different sizes.

Abstract translation: 机翼具有主体，其包括邻接压力侧和吸力侧的前缘和后缘，以提供外部翼型表面。 冷却通道在径向方向上从根部延伸到尖端。 后缘冷却通道将冷却通道与后缘相互连接。 后缘冷却通道包括不同尺寸的第一和第二基座，其相对于具有相同尺寸的基座并且相对于不同尺寸的基座以重复图案布置。