公开(公告)号：WO2014105256A3

公开(公告)日：2014-07-31

申请号：PCT/US2013064490

申请日：2013-10-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KAUFMAN ELEANOR D ,  DEVORE MATTHEW A

IPC: F02C7/12 ,  F01D5/14 ,  F01D25/12

CPC classification number: F01D5/145 ,  F01D5/187 ,  F01D9/041 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/81 ,  F05D2260/2212

Abstract: A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform having an outer surface and an inner surface that axially extend between a leading edge portion and a trailing edge portion. At least one augmentation feature is disposed on at least one of the leading edge portion and the trailing edge portion of the outer surface of the platform.

Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括具有在前缘部分和后缘部分之间轴向延伸的外表面和内表面的平台。 至少一个增强特征设置在平台的外表面的前缘部分和后缘部分中的至少一个上。

公开(公告)号：SG11201403864WA

公开(公告)日：2014-10-30

申请号：SG11201403864W

申请日：2013-02-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZELESKY MARK F ,  KAUFMAN ELEANOR D

IPC: F02C7/12 ,  F01D5/18 ,  F01D25/12

Abstract: A turbine engine airfoil includes a first surface to be cooled by a flow of cooling air. The first surface includes a pedestal array and a first row of contour bumps. The pedestal array includes first and second rows of pedestals extending from the first surface. The second row of pedestals runs in a direction generally parallel to the first row of pedestals. The first row of contour bumps extends from the first surface between the first row of pedestals and the second row of pedestals and runs parallel to the first row of pedestals. The first row of contour bumps is aligned such that at least one of the contour bumps of the first row of contour bumps is positioned at least one of immediately downstream of a pedestal of the first row of pedestals and immediately upstream of a pedestal of the second row of pedestals.

公开(公告)号：SG10201607494TA

公开(公告)日：2016-10-28

申请号：SG10201607494T

申请日：2013-02-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZELESKY MARK F ,  KAUFMAN ELEANOR D

Abstract: A turbine engine airfoil includes a first surface to be cooled by a flow of cooling air. The first surface includes a pedestal array and a first row of contour bumps. The pedestal array includes first and second rows of pedestals extending from the first surface. The second row of pedestals runs in a direction generally parallel to the first row of pedestals. The first row of contour bumps extends from the first surface between the first row of pedestals and the second row of pedestals and runs parallel to the first row of pedestals. The first row of contour bumps is aligned such that at least one of the contour bumps of the first row of contour bumps is positioned at least one of immediately downstream of a pedestal of the first row of pedestals and immediately upstream of a pedestal of the second row of pedestals.

公开(公告)号：EP2909459A4

公开(公告)日：2016-07-27

申请号：EP13867802

申请日：2013-10-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KAUFMAN ELEANOR D ,  DEVORE MATTHEW A

IPC: F02C7/12 ,  F01D5/14 ,  F01D25/12

CPC classification number: F01D5/145 ,  F01D5/187 ,  F01D9/041 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/81 ,  F05D2260/2212

公开(公告)号：EP2825748A4

公开(公告)日：2016-01-20

申请号：EP13760940

申请日：2013-02-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZELESKY MARK F ,  KAUFMAN ELEANOR D

IPC: F02C7/12 ,  F01D5/14 ,  F01D5/18 ,  F01D11/08 ,  F01D25/12

CPC classification number: F01D5/187 ,  F01D5/141 ,  F01D9/041 ,  F01D11/08 ,  F01D25/12 ,  F02C3/10 ,  F05D2220/32 ,  F05D2240/127 ,  F05D2240/81 ,  F05D2260/202 ,  F05D2260/22141

Abstract: A turbine engine component includes a first surface to be cooled by a flow of cooling air. The first surface includes a pedestal array and a first row of contour bumps. The pedestal array includes first and second rows of pedestals extending from the first surface. The second row of pedestals runs in a direction generally parallel to the first row of pedestals. The first row of contour bumps extends from the first surface between the first row of pedestals and the second row of pedestals and runs parallel to the first row of pedestals. The first row of contour bumps is aligned such that at least one of the contour bumps of the first row of contour bumps is positioned at least one of immediately downstream of a pedestal of the first row of pedestals and immediately upstream of a pedestal of the second row of pedestals.

公开(公告)号：EP3099901A4

公开(公告)日：2017-02-01

申请号：EP14881024

申请日：2014-12-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DOWNEY JAMES B JR ,  ZHANG BRENDA ,  LEMIEUX STEVEN G ,  KAUFMAN ELEANOR D ,  FUKUDA TAKAO ,  NADEAU DANIEL C

IPC: F01D5/18 ,  F02C7/18

CPC classification number: F01D5/18 ,  F01D5/187 ,  F01D9/02 ,  F01D25/12 ,  F05D2220/32 ,  F05D2240/304 ,  F05D2260/221 ,  F05D2260/2212 ,  F05D2260/2214 ,  Y02T50/676

Abstract: An airfoil for a gas turbine engine includes pressure and suction surfaces that are provided by pressure and suction walls extending in a radial direction and joined at a leading edge and a trailing edge. A cooling passage is arranged between the pressure and suction walls and extending to the trailing edge. The cooling passage terminates in a trailing edge exit that is arranged in the trailing edge. Multiple rows of pedestals include a first row of pedestals that join the pressure and suction walls. The first row of pedestals is arranged closest to the trailing edge but interiorly from the trailing edge thereby leaving the trailing edge exit unobstructed.