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公开(公告)号:US20160160869A1
公开(公告)日:2016-06-09
申请号:US14904001
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: James T. Roach , Charles R. Watson , Grant O. Cook , Barry Barnett , Shari J. Bugaj , Glenn LeVasseur
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:US20150315922A1
公开(公告)日:2015-11-05
申请号:US14592942
申请日:2015-01-09
Applicant: United Technologies Corporation
Inventor: James T. Roach , Grant O. Cook, III , Colin J. Kling , James F. O'Brien , Shari L. Bugaj
CPC classification number: F01D9/02 , B64C11/14 , F01D5/02 , F01D5/12 , F02C7/04 , F05D2220/32 , F05D2300/10 , F05D2300/603 , F05D2300/6034 , Y02T50/672
Abstract: A spinner for a gas turbine engine comprises an outer shell for defining an airflow path when mounted in a gas turbine engine. An inner surface is provided with a plurality of webs. A gas turbine engine and a fan section for a gas turbine engine are also disclosed.
Abstract translation: 用于燃气涡轮发动机的旋转器包括用于在安装在燃气涡轮发动机中时限定气流路径的外壳。 内表面设置有多个腹板。 还公开了一种燃气涡轮发动机和用于燃气涡轮发动机的风扇部分。
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公开(公告)号:US20200023452A1
公开(公告)日:2020-01-23
申请号:US16126427
申请日:2018-09-10
Applicant: United Technologies Corporation
Inventor: Grant O. Cook, III , James T. Roach
Abstract: Methods of bonding first structures to second structures are disclosed wherein the first and second structures are fabricated materials having different physical characteristics. For example, the first structure may be a composite fan blade and the second structure may be a composite or metallic rotor, both for use in gas turbine engines. The method includes providing the first and second structures and plating or otherwise coating a portion of the first structure with a metal to provide a metal-coated portion. The method includes applying at least one intermediate material onto the metal-coated portion of the first structure. The method further includes bonding the metal-coated portion of the first structure and the intermediate material to the second structure. The bonding is carried out using a relatively low-temperature process, such as liquid phase bonding, including TLP and PTLP bonding. Brazing is also a suitable technique, depending on the materials chosen for the first and second structures.
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公开(公告)号:US20160369419A1
公开(公告)日:2016-12-22
申请号:US14903866
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Michael S. Miarecki , Charles R. Watson , James T. Roach
CPC classification number: C25D5/56 , B05D5/00 , B05D7/02 , B22C7/023 , B22C9/043 , B22C9/10 , B22F1/004 , B28B1/24 , B28B7/342 , B28B11/04 , B28B11/243 , B32B3/263 , B32B7/12 , B32B15/04 , B32B15/08 , B32B15/20 , B32B37/12 , B32B37/1284 , B32B37/14 , B32B2255/10 , B32B2307/202 , B32B2307/554 , B32B2603/00 , B33Y10/00 , B33Y80/00 , B62D35/00 , C04B35/76 , C04B35/806 , C09D5/26 , C23C14/20 , C23C16/06 , C23C18/1633 , C23C18/165 , C23C18/2013 , C23C18/22 , C23C18/31 , C23C26/00 , C23C28/02 , C25D3/02 , C25D3/38 , C25D3/46 , C25D5/48 , C25D9/04 , C25D11/20 , F01D5/00 , F01D5/147 , F01D5/187 , F01D5/284 , F01D5/288 , F01D9/02 , F01D9/041 , F01D11/08 , F01D25/005 , F04D29/023 , F04D29/324 , F04D29/542 , F05D2220/32 , F05D2230/10 , F05D2230/22 , F05D2230/30 , F05D2230/312 , F05D2230/314 , F05D2240/122 , F05D2240/304 , F05D2300/10 , F05D2300/11 , F05D2300/121 , F05D2300/132 , F05D2300/133 , F05D2300/1616 , F05D2300/171 , F05D2300/177 , F05D2300/20 , F05D2300/30 , F05D2300/44 , F05D2300/501 , F05D2300/603 , F05D2300/611 , F05D2300/614 , F42B10/02
Abstract: A plated polymer component is disclosed. The plated polymer component may comprise a polymer substrate having an outer surface, and a metal plating deposited on the outer surface of the polymer substrate. The plated polymer component may further comprise an adhesion promoter at an interface between the polymer substrate and the metal plating.
Abstract translation: 公开了镀覆的聚合物组分。 镀覆的聚合物组分可以包括具有外表面的聚合物基材和沉积在聚合物基材的外表面上的金属电镀。 镀覆的聚合物组分还可以在聚合物基底和金属电镀之间的界面处包含粘合促进剂。
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公开(公告)号:US20160169012A1
公开(公告)日:2016-06-16
申请号:US14904007
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Nelson DaCunha , Barry Barnett , Gary M. Lomasney , Joseph Parkos , James T. Roach , Glenn Levasseur , Charles R. Watson , Jinquan Xu , Grant O. Cook , Raymond K. Kersey , Wendell V. Twelves , Shari L. Bugaj
CPC classification number: F01D5/3092 , C23C18/1641 , C23C18/1651 , C23C18/1657 , C23C18/31 , C25D1/00 , C25D5/022 , C25D5/10 , C25D7/00 , C25D7/04 , C25D7/0607 , F02C7/04 , F02K1/54 , F05D2230/90 , F05D2260/96 , F05D2300/43 , 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:US20160167791A1
公开(公告)日:2016-06-16
申请号:US14903566
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: James T. Roach , Grant Cook , Shari L. Bugaj , Majidullah Dehlavi , Kevin W. Schlichting , Joseph Parkos , Glenn Levasseur
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.
Abstract translation: 公开了包括具有外表面的聚合物基材的航空部件,其中将金属镀在外表面上以形成镀层。 公开了一种使包括具有外表面的聚合物基材和其中金属被镀在外表面上的航空部件的方法。 一种用于从具有带有凹穴的聚合物基底的飞机部件脱落冰以接收加热元件的过镀层加热元件,沉积在基底上的金属,位于该凹槽内的加热元件和沉积在加热元件上的覆盖层, 公开了镀层。
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公开(公告)号:US20160159488A1
公开(公告)日:2016-06-09
申请号:US14903987
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: James T. Roach , Colin J. Kling , Grant O. Cook , James J. McPhail , Shari L. Bugaj , James F. O'Brien , Majidullah Dehlavi , Scott A. Smith , Matthew R. Rader , Matthew A. Turner , JinQuan Xu
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。 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:US20160153287A1
公开(公告)日:2016-06-02
申请号:US14904003
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: James T. Roach , Grant O. Cook , Lakshminarayan S. Bettagere , Jonathan F. Zimmitti , Majidullah Dehlavi , Shari L. Bugaj , Charles R. Watson , Brian D. Walter , Andrew G. Alarcon , Sarah M. Wall , Christopher J. Hertel , Octavio Martin , Thomas J. Robertson , Aaron Beaudry , Jeffrey J. Scalia , Joseph J. Wassel , Joe Ott , Barry Barnett , Glenn Levasseur
CPC classification number: F01D25/005 , B64D29/00 , B64D2045/009 , C23C18/1641 , C23C18/31 , C25D1/00 , C25D5/56 , C25D7/00 , F01D5/282 , F01D5/3092 , F01D9/041 , F01D25/24 , F01D25/30 , F02C7/04 , F02K1/54 , F04D29/023 , F04D29/321 , F04D29/322 , F04D29/522 , F04D29/542 , F05D2220/32 , F05D2230/31 , F05D2230/90 , F05D2240/00 , F05D2240/12 , F05D2240/30 , F05D2240/60 , F05D2250/283 , F05D2260/96 , F05D2300/10 , F05D2300/40 , F05D2300/43 , F05D2300/603 , F16C3/02 , 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:US20160152320A1
公开(公告)日:2016-06-02
申请号:US14930760
申请日:2015-11-03
Applicant: United Technologies Corporation
Inventor: Colin J. Kling , Shari L. Bugaj , James T. Roach
CPC classification number: B64C11/14 , B29C70/14 , B29C70/46 , B29K2101/10 , B29K2105/128 , B29K2307/04 , B29L2031/7504 , B29L2031/7724 , F02C7/04 , F05D2300/603 , Y02T50/672
Abstract: A spinner for a gas turbine engine is disclosed. The spinner may include a body extending between a first and second end comprised of a cured chopped unidirectional fiber pre-impregnated material. The body may have a generally conical shape and may further be plated with a metal or metal alloy.
Abstract translation: 公开了一种用于燃气涡轮发动机的旋转器。 旋转器可以包括在由固化的切断的单向纤维预浸渍材料组成的第一和第二端之间延伸的主体。 主体可以具有大致圆锥形的形状,并且还可以镀金属或金属合金。
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公开(公告)号:US10968758B2
公开(公告)日:2021-04-06
申请号:US16126427
申请日:2018-09-10
Applicant: United Technologies Corporation
Inventor: Grant O. Cook, III , James T. Roach
Abstract: A rotor assembly for a gas turbine engine is disclosed. The assembly includes: a composite fan blade, the fan blade including a root; a metallic rotor including a slot for receiving the root; the root being at least partially coated with a metal to form a metal-coated portion; the metal-coated portion of the root being at least partially covered with an intermediate material; and the root, metal-coated portion and intermediate material being received in the slot and bonded to the rotor.
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