公开(公告)号：WO2015017095A3

公开(公告)日：2015-04-09

申请号：PCT/US2014045985

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROACH JAMES T ,  KLING COLIN J ,  COOK GRANT O III ,  MCPHAIL JAMES J ,  BUGAJ SHARI L ,  O'BRIEN JAMES F ,  DEHLAVI MAJIDULLAH ,  SMITH SCOTT A ,  RADER MATTHEW R ,  TURNER MATTHEW A ,  XU JINQUAN

IPC: F01D25/00 ,  B29D22/00 ,  F01D25/24 ,  F02C7/20

CPC classification number: B64D29/00 ,  B29D22/00 ,  F01D5/02 ,  F01D25/28 ,  F02K3/04 ,  F05D2220/32 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2300/10 ,  F05D2300/43 ,  F05D2300/603 ,  Y02T50/672

Abstract: Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.

Abstract translation: 公开了用于制造轻质电镀聚合物燃气涡轮发动机部件的电镀聚合物燃气涡轮发动机部件和方法。 部件包括镀有一个或多个金属层的聚合物基底。 聚合物基材的聚合物材料可以用可包含碳，金属或玻璃的材料在结构上增强。 聚合物基材还可以包括多个层以形成复合叠层结构。

公开(公告)号：WO2015084460A3

公开(公告)日：2015-08-20

申请号：PCT/US2014056552

申请日：2014-09-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROBERTSON THOMAS J ,  MCPHAIL JAMES J

IPC: F02C7/28 ,  F01D11/00

CPC classification number: F01D11/005 ,  F01D5/02 ,  F01D11/001 ,  F02C7/04 ,  F02C7/28 ,  F05D2220/32 ,  F05D2220/36 ,  F05D2240/24 ,  F05D2240/55 ,  F16J15/04

Abstract: A recirculation seal for use within a gas turbine engine. The recirculation seal includes a first seal base, including a first seal base axis. The recirculation seal further includes a second seal base, including a second seal base axis The recirculation seal further includes a resilient bulb member coupled to the first seal base. The resilient bulb member includes an exterior bulb wall and an interior bulb wall, wherein the interior bulb wall defines an interior space.

Abstract translation: 用于燃气涡轮发动机内的再循环密封。 再循环密封件包括第一密封基座，包括第一密封基座轴线。 再循环密封件还包括第二密封基座，包括第二密封基座轴线。再循环密封件还包括联接到第一密封基座的弹性球形部件。 弹性灯泡构件包括外部灯泡壁和内部灯泡壁，其中内部灯泡壁限定内部空间。

公开(公告)号：CA2917916A1

公开(公告)日：2015-02-05

申请号：CA2917916

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROACH JAMES T ,  KLING COLIN J ,  COOK GRANT O III ,  MCPHAIL JAMES J ,  BUGAJ SHARI L ,  O'BRIEN JAMES F ,  DEHLAVI MAJIDULLAH ,  SMITH SCOTT A ,  RADER MATTHEW R ,  TURNER MATTHEW A ,  XU JINQUAN

IPC: F01D25/00 ,  B29D22/00 ,  F01D25/24 ,  F02C7/20

Abstract: Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.

公开(公告)号：EP3019711A4

公开(公告)日：2017-05-10

申请号：EP14832491

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROACH JAMES T ,  KLING COLIN J ,  COOK GRANT O III ,  MCPHAIL JAMES J ,  BUGAJ SHARI L ,  O'BRIEN JAMES F ,  DEHLAVI MAJIDULLAH ,  SMITH SCOTT A ,  RADER MATTHEW R ,  TURNER MATTHEW A ,  XU JINQUAN

IPC: F01D25/00 ,  B29D22/00 ,  F01D25/24 ,  F02C7/20

CPC classification number: B64D29/00 ,  B29D22/00 ,  F01D5/02 ,  F01D25/28 ,  F02K3/04 ,  F05D2220/32 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2300/10 ,  F05D2300/43 ,  F05D2300/603 ,  Y02T50/672

公开(公告)号：EP3052788A4

公开(公告)日：2017-06-21

申请号：EP14868665

申请日：2014-09-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROBERTSON THOMAS J ,  MCPHAIL JAMES J

IPC: F02C7/28 ,  F01D5/02 ,  F01D11/00 ,  F02C7/04 ,  F16J15/04

CPC classification number: F01D11/005 ,  F01D5/02 ,  F01D11/001 ,  F02C7/04 ,  F02C7/28 ,  F05D2220/32 ,  F05D2220/36 ,  F05D2240/24 ,  F05D2240/55 ,  F16J15/04

公开(公告)号：EP3060777A4

公开(公告)日：2017-06-21

申请号：EP14855237

申请日：2014-05-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KLING COLIN J ,  WEBB SCOT A ,  MCPHAIL JAMES J

IPC: B64C11/14 ,  F01D5/06

CPC classification number: B64C11/14 ,  F01D5/066 ,  F02C3/04 ,  F05D2220/36 ,  F05D2230/23 ,  Y02T50/672

Abstract: A fan assembly of a gas turbine engine, a method for fabricating a fan assembly for a gas turbine engine, and a gas turbine engine are disclosed. The fan assembly of the gas turbine engine may include a spinner section, a fan hub section aft of the spinner section, and a joint therebetween. The fan assembly may further include a support ring for internally supporting the spinner, the support ring including a first portion facing the fan hub and a second portion connected to the spinner at the joint, wherein the connection between the second portion and the joint is a bonded connection.

Abstract translation: 公开了一种燃气涡轮发动机的风扇组件，用于制造用于燃气涡轮发动机的风扇组件的方法以及燃气涡轮发动机。 燃气涡轮发动机的风扇组件可以包括旋转器部分，旋转器部分的尾部的风扇轮毂部分以及它们之间的接头。 所述风扇组件还可包括用于内部支撑所述旋转器的支撑环，所述支撑环包括面向所述风扇轮毂的第一部分和在所述接头处连接至所述旋转器的第二部分，其中所述第二部分与所述接头之间的连接是 绑定连接。