公开(公告)号：EP2923043A4

公开(公告)日：2016-03-09

申请号：EP13856375

申请日：2013-11-20

Applicant: UNITED TECHNOLOGIES CORP ,  GEORGIA INST TECHNOLOGY

Inventor： STAROSELSKY ALEXANDER ,  PIETRASZKIEWICZ EDWARD F ,  MONGILLO DOMINIC J JR ,  BARKER VINCENT ,  ADAIR BENJAMIN ,  JOHNSON W STEVEN

IPC: F01D25/00 ,  F01D5/00 ,  F01D5/12 ,  F01D21/00 ,  F01D25/28 ,  F02C7/00 ,  G01N29/04

CPC classification number: B23P6/002 ,  B23P6/045 ,  B23P9/00 ,  F01D5/005 ,  F01D25/285 ,  F05D2230/80 ,  F05D2270/11 ,  F05D2300/60 ,  Y10T29/49318 ,  Y10T29/49748

公开(公告)号：EP3036405A4

公开(公告)日：2017-05-10

申请号：EP14837927

申请日：2014-08-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： THOMEN SETH J ,  PIETRASZKIEWICZ EDWARD F

IPC: F01D5/18 ,  F01D9/04 ,  F01D9/06 ,  F01D11/08 ,  F01D11/24 ,  F01D25/12 ,  F02C7/12 ,  F02C7/18 ,  F04D29/54 ,  F04D29/58

CPC classification number: F01D25/12 ,  F01D9/041 ,  F01D9/065 ,  F01D11/08 ,  F01D11/24 ,  F02C7/12 ,  F04D29/164 ,  F04D29/542 ,  F04D29/582 ,  F04D29/584 ,  F05D2220/32 ,  F05D2240/11 ,  F05D2240/81 ,  F05D2250/11 ,  F05D2260/201 ,  F05D2260/202 ,  F05D2260/205 ,  F05D2260/22141

公开(公告)号：EP2825732A4

公开(公告)日：2016-03-30

申请号：EP13762007

申请日：2013-03-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PROPHETER-HINCKLEY TRACY A ,  PIETRASZKIEWICZ EDWARD F ,  PEREZ RAFAEL A ,  BANKS ANTON G

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F05D2240/12 ,  F05D2250/185 ,  F05D2260/205 ,  F05D2260/2212 ,  F05D2260/22141

Abstract: An airfoil for a gas turbine engine according to one exemplary embodiment includes an airfoil body that extends between a leading edge and a trailing edge. A cooling circuit can be defined within the airfoil body. The cooling circuit can include at least one trip strip disposed within a cavity of the cooling circuit between a leading edge inner wall and a first rib. The at least one trip strip can include an increasing height in a direction from the first rib toward the leading edge inner wall.

Abstract translation: 根据一个示例性实施例的用于燃气涡轮发动机的翼型件包括在前缘和后缘之间延伸的翼型件本体。 可以在翼型体内限定冷却回路。 冷却回路可以包括设置在前缘内壁和第一肋之间的冷却回路的空腔内的至少一个跳闸条。 至少一个跳闸带可以包括从第一肋朝向前缘内壁的方向上的增加的高度。

公开(公告)号：EP2971545A4

公开(公告)日：2017-02-01

申请号：EP14779667

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CORCORAN CHRISTOPHER ,  GHIGLIOTTY JAIME G ,  PEREZ RAFAEL A ,  PIETRASZKIEWICZ EDWARD F

IPC: F01D5/18 ,  F02C7/12

CPC classification number: F01D5/186 ,  F01D5/187 ,  F05D2220/32 ,  F05D2240/30 ,  F05D2260/202 ,  F05D2260/22141 ,  Y02T50/676

Abstract: A rotor blade comprises a root section, an airfoil section, a leading edge cooling cavity, an intermediate cooling cavity, and a trailing edge cooling cavity. The leading edge, intermediate, and trailing edge cooling cavities each extend spanwise through the airfoil section from a coolant inlet passage in the root section, and each terminate proximate the airfoil tip.

公开(公告)号：EP2938856A4

公开(公告)日：2016-01-27

申请号：EP13866761

申请日：2013-12-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KOONANKEIL JAMES M ,  PIETRASZKIEWICZ EDWARD F ,  MONGILLO JR DOMINIC J

IPC: F01D5/18

CPC classification number: F02C7/12 ,  F01D5/186 ,  F05D2250/141 ,  F05D2250/231 ,  F05D2250/232 ,  F05D2250/51 ,  F05D2260/202 ,  Y02T50/676

公开(公告)号：EP2815104A4

公开(公告)日：2016-01-06

申请号：EP13784491

申请日：2013-02-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEVASSEUR GLENN ,  PIETRASZKIEWICZ EDWARD F

IPC: F01D5/18 ,  F01D9/06 ,  F23R3/00 ,  F23R3/06

CPC classification number: F01D25/14 ,  F01D5/186 ,  F01D9/065 ,  F05D2240/81 ,  F05D2250/182 ,  F05D2250/183 ,  F05D2250/324 ,  F05D2260/202 ,  F23R3/002 ,  F23R2900/03042 ,  Y02T50/676 ,  Y10T29/49229 ,  Y10T29/49323

Abstract: A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface and a diffusing section in communication with the inlet and extending to the outlet. The diffusing section includes a plurality of crenellation features that encourage lateral spreading of cooling air flowing through the cooling hole.

公开(公告)号：EP2815109A4

公开(公告)日：2016-03-02

申请号：EP13785031

申请日：2013-02-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEVASSEUR GLENN ,  PIETRASZKIEWICZ EDWARD F ,  ZELESKY MARK F ,  MONGILLO DOMINIC J ,  KLINEFELTER KEVIN J ,  DOLL STEPHEN D ,  FRITCH MARKUS W

IPC: B23H9/14 ,  B23H7/26 ,  B23H9/10 ,  F01D5/18 ,  F01D9/06 ,  F23R3/06

CPC classification number: B23H9/10 ,  B23H1/00 ,  B23H7/26 ,  B23H9/14 ,  F01D5/186 ,  F01D9/065 ,  F05D2240/81 ,  F05D2260/202 ,  F23R3/002 ,  F23R2900/03042 ,  Y02T50/676

Abstract: A method for forming a cooling hole extending from an inlet on a first surface of a wall to an outlet on a second surface of the wall includes forming a diffusing section of the cooling hole, and a trailing edge on the outlet by electrical discharge machining, and forming longitudinal lobes in the diffusing section. The metering section extends from the inlet on a first surface of the wall towards the second surface of the wall. The diffusing section extends from the outlet to one end of a metering section located between the inlet and the outlet. The outlet is substantially linear or convex at the trailing edge and the lobes are separated by longitudinal ridges.

公开(公告)号：EP2900963A4

公开(公告)日：2016-02-17

申请号：EP13841940

申请日：2013-09-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SLAVENS THOMAS N ,  PIETRASZKIEWICZ EDWARD F ,  MARTIN THOMAS J ,  ZELESKY MARK F ,  GAUTSCHI STEVEN B ,  DEVORE MATTHEW A ,  STAROSELSKY ALEXANDER

IPC: F02C7/12 ,  F01D5/18 ,  F01D17/16 ,  F02K3/00

CPC classification number: F01D25/12 ,  F01D5/186 ,  F01D5/187 ,  F01D5/188 ,  F01D5/189 ,  F01D9/04 ,  F01D9/06 ,  F01D9/065 ,  F01D17/162 ,  F05D2220/32 ,  F05D2240/81 ,  F05D2260/202 ,  F05D2260/232 ,  Y02T50/673 ,  Y02T50/676

Abstract: A vane structure includes a baffle (84) movably mounted within an aperture (96), the baffle (84) movable to control a cooling flow between a first cooling cavity (98) and a second cooling cavity (100).

公开(公告)号：EP2870344A4

公开(公告)日：2015-08-26

申请号：EP13855260

申请日：2013-07-02

Applicant: UNITED TECHNOLOGIES CORP

Inventor： XU JINQUAN ,  PIETRASZKIEWICZ EDWARD F ,  ZELESKY MARK F ,  LEVASSEUR GLENN ,  MONGILLO DOMINIC J

IPC: F01D5/18 ,  F01D5/28 ,  F23R3/06

CPC classification number: B24C1/045 ,  B23K26/0622 ,  B23K26/082 ,  B23K26/146 ,  B23K26/389 ,  B23K2201/001 ,  B26F3/004 ,  F01D5/186 ,  F01D5/288 ,  F01D9/041 ,  F05D2240/81 ,  F05D2250/52 ,  F05D2250/70 ,  F05D2260/202 ,  F23R3/06 ,  F23R2900/00018 ,  F23R2900/03042 ,  Y02T50/676

Abstract: A gas turbine engine component includes a wall with an inner face and an outer skin. A plurality of cooling air holes extend from the inner face to the outer skin. The cooling holes include an inlet merging into a metering section, and a diffusion section downstream of the metering section, and extend to an outlet at the outer skin. The diffusion section includes a plurality of lobes. A coating layer is formed on the outer skin, with at least a portion of the plurality of lobes formed within the thermal barrier coating. A method of forming such a component is also disclosed.

公开(公告)号：EP2971544A4

公开(公告)日：2017-02-01

申请号：EP14774119

申请日：2014-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GHIGLIOTTY JAIME G ,  PIETRASZKIEWICZ EDWARD F ,  MONGILLO DOMINIC J ,  CORCORAN CHRISTOPHER

IPC: F01D5/18 ,  B22C9/10 ,  B22D25/02 ,  F01D25/12 ,  F02C7/18

CPC classification number: F01D5/186 ,  B22C9/10 ,  B22D25/02 ,  F01D5/187 ,  F05D2220/32 ,  F05D2230/30 ,  F05D2240/304 ,  F05D2250/185 ,  F05D2260/202 ,  F05D2260/2212 ,  F05D2260/22141 ,  Y02T50/676

Abstract: A gas turbine engine component includes first and second walls spaced apart from one another to provide a cooling passage. First and second trip strips are respectively provided on the first and second walls and arranged to face one another. The first and second trip strips are arranged in an interleaved fashion with respect to one another in a direction.