公开(公告)号：WO2015088623A2

公开(公告)日：2015-06-18

申请号：PCT/US2014057456

申请日：2014-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HIMES JASON D

IPC: F01D5/02 ,  F01D5/10 ,  F01D25/06 ,  F02C7/00

CPC classification number: F01D5/027 ,  F01D5/3015 ,  F01D25/06 ,  F02C3/04 ,  F02C7/06 ,  F02C7/36 ,  F04D29/662 ,  F05D2220/32 ,  F05D2230/22 ,  F05D2230/31 ,  Y02T50/671

Abstract: A rotating component for a turbine engine includes a rotor portion protruding radially outward, at least one overweight region is located in the rotor portion, and at least one additively manufactured counterweight region is positioned relative to the at least one overweight region such that the rotating component is circumferentially balanced.

Abstract translation: 用于涡轮发动机的旋转部件包括径向向外突出的转子部分，至少一个超重区域位于转子部分中，并且至少一个相加制造的配重区域相对于至少一个超重区域定位，使得旋转部件 周向平衡。

公开(公告)号：WO2015020931A3

公开(公告)日：2015-04-09

申请号：PCT/US2014049538

申请日：2014-08-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HIMES JASON D

IPC: F01D5/00 ,  F01D25/24

CPC classification number: F01D11/006 ,  F01D5/02 ,  F01D5/12 ,  F01D5/3015 ,  F01D11/001 ,  F04D29/083 ,  F04D29/322 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2240/80 ,  F05D2260/30

Abstract: A cover plate assembly according to an exemplary aspect of the present disclosure includes, among other things, a first cover plate and a second cover plate in contact with a portion of the first cover plate to at least axially retain the first cover plate.

Abstract translation: 根据本公开的示例性方面的盖板组件尤其包括与第一盖板的一部分接触以便​​至少轴向保持第一盖板的第一盖板和第二盖板。

公开(公告)号：WO2015088620A3

公开(公告)日：2015-08-27

申请号：PCT/US2014057346

申请日：2014-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HIMES JASON D ,  KARNER PETER JOSEF

IPC: F01D5/02 ,  F01D5/10 ,  F01D25/04 ,  F02C7/00

CPC classification number: F01D5/027 ,  F02C3/04 ,  F04D29/321 ,  F04D29/644 ,  F04D29/662 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/60 ,  F16F15/322 ,  F16F15/34

Abstract: A balance ring for a gas turbine engine has a ring shaped body with a first radial thickness, an anti-rotation tab extending outward from the body and at least one millable balancing feature connected to the body.

Abstract translation: 用于燃气涡轮发动机的平衡环具有第一径向厚度的环形主体，从主体向外延伸的防旋转翼片以及连接到主体的至少一个可磨平衡平衡特征。

公开(公告)号：WO2015073112A3

公开(公告)日：2015-08-20

申请号：PCT/US2014056023

申请日：2014-09-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BEATTIE JEFFREY S ,  HIMES JASON D ,  HOUGH MATTHEW ANDREW ,  CORCORAN CHRISTOPHER

IPC: F01D5/08 ,  F01D5/18

CPC classification number: F01D5/081 ,  F01D5/082 ,  F01D5/085 ,  F01D5/12 ,  F01D5/187 ,  F01D5/3007 ,  F01D5/3015 ,  F05D2220/32 ,  F05D2240/81 ,  F05D2260/20

Abstract: An assembly according to an exemplary aspect of the present disclosure includes, among other things, a disk, a cover plate providing a cavity at a first axial side of the disk, a passageway including an inlet provided by a notch in at least one of the disk and the cover plate in fluid communication with the cavity, and the passageway extending from the inlet to an exit provided at a second axial side of the disk opposite the first axial side, the exit in fluid communication with the inlet, and the passageway configured to provide fluid flow from the cavity to the exit.

Abstract translation: 根据本公开的示例性方面的组件包括盘，在盘的第一轴向侧提供空腔的盖板，包括由至少一个中的至少一个中的凹口提供的入口的通道 盘和盖板与空腔流体连通，并且从入口延伸到设置在与第一轴向侧相对的盘的第二轴向侧处的出口的通道，与入口流体连通的出口和配置的通道 以提供从空腔到出口的流体流动。

公开(公告)号：EP3049624A4

公开(公告)日：2017-05-24

申请号：EP14869043

申请日：2014-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HIMES JASON D ,  KARNER PETER JOSEF

IPC: F01D5/02 ,  F01D5/10 ,  F01D25/04 ,  F02C7/00

CPC classification number: F01D5/027 ,  F02C3/04 ,  F04D29/321 ,  F04D29/644 ,  F04D29/662 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/60 ,  F16F15/322 ,  F16F15/34

Abstract: A balance ring for a gas turbine engine has a ring shaped body with a first radial thickness, an anti-rotation tab extending outward from the body and at least one millable balancing feature connected to the body.

Abstract translation: 用于燃气涡轮发动机的平衡环具有第一径向厚度的环形主体，从主体向外延伸的防旋转翼片以及连接到主体的至少一个可磨平衡平衡特征。

公开(公告)号：EP3052762A4

公开(公告)日：2017-10-04

申请号：EP14861286

申请日：2014-09-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BEATTIE JEFFREY S ,  HIMES JASON D ,  HOUGH MATTHEW ANDREW ,  CORCORAN CHRISTOPHER

IPC: F01D5/08 ,  F01D5/18 ,  F01D5/30

CPC classification number: F01D5/081 ,  F01D5/082 ,  F01D5/085 ,  F01D5/12 ,  F01D5/187 ,  F01D5/3007 ,  F01D5/3015 ,  F05D2220/32 ,  F05D2240/81 ,  F05D2260/20

公开(公告)号：EP3058175A4

公开(公告)日：2017-08-09

申请号：EP14869635

申请日：2014-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HIMES JASON D

IPC: F01D5/02 ,  F01D5/10 ,  F01D25/06 ,  F02C7/00

CPC classification number: F01D5/027 ,  F01D5/3015 ,  F01D25/06 ,  F02C3/04 ,  F02C7/06 ,  F02C7/36 ,  F04D29/662 ,  F05D2220/32 ,  F05D2230/22 ,  F05D2230/31 ,  Y02T50/671

Abstract: A rotating component for a turbine engine includes a rotor portion protruding radially outward, at least one overweight region is located in the rotor portion, and at least one additively manufactured counterweight region is positioned relative to the at least one overweight region such that the rotating component is circumferentially balanced.

Abstract translation: 用于涡轮发动机的旋转部件包括径向向外突出的转子部分，至少一个超重区域位于转子部分中，并且至少一个增量式制造的配重区域相对于至少一个超重区域定位，使得旋转部件 是圆周平衡的。