公开(公告)号：WO2015006433A2

公开(公告)日：2015-01-15

申请号：PCT/US2014045928

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROACH JAMES T ,  BARNETT BARRY ,  COOK III GRANT O ,  WATSON CHARLES R ,  BUGAJ SHARI L ,  LEVASSEUR GLENN ,  TWELVES WENDELL V JR ,  HERTEL CHRISTOPHER J ,  KLING COLIN J ,  TURNER MATTHEW A ,  XU JINQUAN ,  CLARKSON STEVEN ,  CAULFIELD MICHAEL

CPC classification number: F04D19/002 ,  B32B1/00 ,  B32B1/08 ,  B32B27/281 ,  B32B27/285 ,  B32B27/34 ,  B32B27/36 ,  B32B2255/10 ,  B32B2255/205 ,  B32B2262/101 ,  B32B2262/103 ,  B32B2262/106 ,  B32B2270/00 ,  B32B2307/554 ,  F01D5/147 ,  F01D5/26 ,  F01D5/282 ,  F01D5/286 ,  F01D9/041 ,  F01D25/02 ,  F01D25/24 ,  F04D29/388 ,  F04D29/541 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2240/00 ,  F05D2240/12 ,  F05D2240/30 ,  F05D2260/96 ,  F05D2300/10 ,  F05D2300/43 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/673

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。 这些部件包括镀有一个或多个金属层的聚合物基材。 聚合物基材的聚合材料可以用可以包括碳，金属或玻璃的材料在结构上加强。 聚合物基底还可以包括多个层以形成复合铺层结构。

公开(公告)号：CA2917884A1

公开(公告)日：2015-01-15

申请号：CA2917884

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROACH JAMES T ,  BARNETT BERRY ,  COOK GRANT O III ,  WATSON CHARLES R ,  BUGAJ SHARI L ,  LEVASSEUR GLENN ,  TWELVES WENDELL V JR ,  HERTEL CHRISTOPHER J ,  KLING COLIN J ,  TURNER MATTHEW A ,  XU JINQUAN ,  CLARKSON STEVEN ,  CAULFIELD MICHAEL

IPC: F01D25/00 ,  B32B7/02 ,  B32B27/00 ,  F01D5/28 ,  F01D5/30 ,  F01D9/02 ,  F02C7/05

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：EP3019710A4

公开(公告)日：2017-05-10

申请号：EP14822947

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ROACH JAMES T ,  BARNETT BARRY ,  COOK III GRANT O ,  WATSON CHARLES R ,  BUGAJ SHARI L ,  LEVASSEUR GLENN ,  TWELVES WENDELL V JR ,  HERTEL CHRISTOPHER J ,  KLING COLIN J ,  TURNER MATTHEW A ,  XU JINQUAN ,  CLARKSON STEVEN ,  CAULFIELD MICHAEL

IPC: F01D25/00 ,  B32B7/02 ,  B32B27/00 ,  F01D5/28 ,  F01D5/30 ,  F01D9/02 ,  F02C7/05

CPC classification number: F04D19/002 ,  B32B1/00 ,  B32B1/08 ,  B32B27/281 ,  B32B27/285 ,  B32B27/34 ,  B32B27/36 ,  B32B2255/10 ,  B32B2255/205 ,  B32B2262/101 ,  B32B2262/103 ,  B32B2262/106 ,  B32B2270/00 ,  B32B2307/554 ,  F01D5/147 ,  F01D5/26 ,  F01D5/282 ,  F01D5/286 ,  F01D9/041 ,  F01D25/02 ,  F01D25/24 ,  F04D29/388 ,  F04D29/541 ,  F05D2220/32 ,  F05D2230/90 ,  F05D2240/00 ,  F05D2240/12 ,  F05D2240/30 ,  F05D2260/96 ,  F05D2300/10 ,  F05D2300/43 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/673