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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
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。
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公开(公告)号:WO2015006397A1
公开(公告)日:2015-01-15
申请号:PCT/US2014045866
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: GALOS CAMELIA , COOK GRANT O III , ROACH JAMES T , LEVASSEUR GLENN , BU GAJ SHARI L
IPC: C23C26/00
CPC classification number: C23C18/165 , B63G8/001 , B63G2008/002 , B64G1/10 , C23C18/1603 , C23C18/2073 , C23C18/31 , C25D5/02 , C25D5/022 , C25D5/48 , C25D5/56 , C25D7/00 , F24F13/00 , F25D23/00 , G21F5/06 , Y02E10/721 , Y02E10/726
Abstract: An industrial product comprising a polymer substrate formed in a shape of the industrial product, and a metallic plating layer plated on at least one surface of the industrial product is described. The industrial product may be nuclear waste equipment, industrial equipment exposed to saline, a satellite or satellite component, or heating, ventilation, air-conditioning and refrigeration (HVACR) equipment.
Abstract translation: 描述了包括形成为工业产品形状的聚合物基材和电镀在工业产品的至少一个表面上的金属镀层的工业产品。 工业产品可能是核废料设备,暴露于盐水的工业设备,卫星或卫星部件,或加热,通风,空调和制冷(HVACR)设备。
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公开(公告)号:CA2917872A1
公开(公告)日:2015-01-15
申请号:CA2917872
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: LEVASSEUR GLENN , ROACH JAMES T , COOK GRANT O III , KERSEY RAYMOND K
Abstract: A plated polymer test specimen for measuring strain imparted to the plated polymer test specimen includes a polymeric substrate including a top, a bottom, a pair of opposing edges and a pair of opposing end edges, the top and bottom being plated with top and bottom metal layers respectively, the side edges and the end edges being at least substantially free of plating. The substrate includes two spaced-apart holes that extend through the top metal layer, substrate and the bottom metal layer. Alternatively, the substrate may comprise a composite layup structure. A method for testing the strain imparted to a plated polymer test specimen is also disclosed.
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公开(公告)号:WO2015006400A8
公开(公告)日:2015-08-20
申请号:PCT/US2014045871
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: COOK GRANT O , ROACH JAMES T
IPC: F03D11/00 , B05D1/00 , C25D1/02 , C25D3/12 , C25D3/22 , C25D3/38 , C25D3/46 , C25D3/48 , C25D5/56 , F03D1/06
CPC classification number: C23C18/165 , B63G8/001 , B63G2008/002 , B64G1/10 , C23C18/1603 , C23C18/2073 , C23C18/31 , C25D5/02 , C25D5/022 , C25D5/48 , C25D5/56 , C25D7/00 , F24F13/00 , F25D23/00 , G21F5/06 , Y02E10/721 , Y02E10/726
Abstract: A wind turbine component is disclosed. The wind turbine component may comprise a polymer substrate and a metal plating layer plated on a surface of the polymer substrate. The wind turbine component may be a nacelle or a wind turbine blade.
Abstract translation: 公开了一种风力涡轮机部件。 风力涡轮机部件可以包括聚合物基板和镀在聚合物基板的表面上的金属镀层。 风力涡轮机部件可以是机舱或风力涡轮机叶片。
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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。
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公开(公告)号:WO2014120123A2
公开(公告)日:2014-08-07
申请号:PCT/US2013023635
申请日:2013-01-29
Applicant: UNITED TECHNOLOGIES CORP
Inventor: ROACH JAMES T
IPC: F02C7/20
CPC classification number: F01D9/04 , F01D1/02 , F01D5/02 , F01D5/12 , F02C7/04 , F05D2220/30 , F05D2300/10 , F05D2300/40 , F05D2300/43
Abstract: A nosecone for a turbine engine includes a nosecone body and a nosecone mount. The nosecone body extends along an axis between a tip end and a base end. The nosecone body is configured from or otherwise includes thermoplastic material. The nosecone body includes a shell and an arrangement of ribs, which structurally support at least a portion of the shell. A thickness of the arrangement of ribs is greater than or substantially equal to approximately one half of a thickness of the shell. The nosecone mount is adapted to connect the nosecone body to a component of the turbine engine.
Abstract translation: 用于涡轮发动机的鼻锥包括鼻锥体和鼻锥座。 鼻锥体沿着尖端和基端之间的轴线延伸。 鼻锥体由热塑性材料构成或以其他方式包括热塑性材料。 鼻锥体包括壳体和肋的布置,其在结构上支撑壳体的至少一部分。 肋的布置的厚度大于或基本上等于壳的厚度的大约一半。 鼻锥安装座适于将鼻锥体与涡轮发动机的部件连接。
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公开(公告)号:CA2917931A1
公开(公告)日:2015-01-15
申请号:CA2917931
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: DACUNHA NELSON , BARNETT BERRY , LOMASNEY GARY M , PARKOS JOSEPH , ROACH JAMES T , LEVASSEUR GLENN , WATSON CHARLES R , XU JINQUAN , COOK GRANT O III , KERSEY RAYMOND K , TWELVES WENDELL V , BUGAJ SHARI L
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.
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公开(公告)号:CA2917880A1
公开(公告)日:2015-01-15
申请号:CA2917880
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: ROACH JAMES T , COOK GRANT , BUGAJ SHARI L , DEHLAVI MAJIDULLAH , SCHLICHTING KEVIN W , PARKOS JOSEPH , LEVASSEUR GLENN
IPC: C23C26/00
Abstract: Aviation components comprising a polymeric substrate having an outer surface wherein a metal is plated onto the outer surface to form a plated layer are disclosed. A method to make aviation components comprising a polymeric substrate having an outer surface and where a metal is plated onto the outer surface is disclosed. An over-plated heating element for shedding ice from an aircraft component having a polymeric substrate with a pocket to receive a heating element, a metal deposited onto the substrate, a heating element positioned within the pocket and a covering layer deposited onto the heating element and the plated layer is disclosed.
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公开(公告)号:CA2917888A1
公开(公告)日:2015-01-15
申请号:CA2917888
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KLING COLIN J , ROACH JAMES T , BUGAJ SHARI L
Abstract: Plated polymeric articles having a composite layup structure and method of making the same are disclosed. A plated polymeric article comprises a composite layup having first and second polymer layers. The plated polymeric article further comprises a first metal plated onto the polymer. Additionally, methods for fabricating a plated polymeric article are disclosed. A composite layup is provided and compression molded into a desired shape having an outer surface. The outer surface of the article is prepared to receive a catalyst and then is activated with the catalyst. A first metallic layer is then plated onto the outer surface.
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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
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.
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