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1.发明申请ADDITIVE MANUFACTURING OF CERAMIC TURBINE COMPONENTS BY PARTIAL TRANSIENT LIQUID PHASE BONDING USING METAL BINDERS 审中-公开用金属结合剂部分瞬间液相结合陶瓷涡轮机零部件的添加剂制造
公开(公告)号：WO2015030879A3
公开(公告)日：2015-05-07
申请号：PCT/US2014034943
申请日：2014-04-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MIRONETS SERGEY , COOK III GRANT O
IPC: C04B35/10 , C04B35/28 , C04B35/46 , C04B35/622
CPC classification number: C04B35/653 , B22F3/1055 , B22F5/009 , B28B1/001 , B33Y10/00 , C04B35/10 , C04B35/565 , C04B35/584 , C22C29/065 , C22C29/12 , C22C29/16 , F05D2230/30 , Y02P10/295
Abstract: A ceramic turbine component is formed by a process including mixing a ceramic powder with a metal binder powder mixture. The powder mixture is then formed into a turbine component that is subsequently densified by partial transient liquid phase sintering. In an embodiment, the turbine component may be formed by an additive manufacturing process such as selective laser sintering.
Abstract translation: 陶瓷涡轮机部件通过包括将陶瓷粉末与金属粘合剂粉末混合物混合的过程形成。 然后将粉末混合物形成涡轮机部件，随后通过部分瞬时液相烧结致密化。 在一个实施例中，涡轮机部件可以通过诸如选择性激光烧结的增材制造工艺形成。
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公开(公告)号：WO2015053832A3
公开(公告)日：2015-06-18
申请号：PCT/US2014045929
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： TWELVES WENDELL V , COOK III GRANT O
CPC classification number: C25D5/56 , B05D5/00 , B05D7/02 , B22C7/023 , B22C9/043 , B22C9/10 , B22F5/04 , B22F7/08 , 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 , B64C39/024 , B64C39/028 , B64C2201/10 , 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: An airfoil is disclosed. The airfoil may comprise a leading edge, a body portion and a trailing edge formed from a high-modulus plating. The body portion of the airfoil may be formed from a material having a lower elastic modulus than the high-modulus plating. The high-modulus plating may improve the stiffness of the trailing edge, allowing for thinner trailing edges with improved fatigue life to be formed.
Abstract translation: 公开了翼型。 翼型可以包括由高模量电镀形成的前缘，主体部分和后缘。 翼型的主体部分可以由具有比高模量镀层更低的弹性模量的材料形成。 高模量电镀可以改善后缘的刚性，允许形成更薄的后缘，并且具有改善的疲劳寿命。
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3.发明申请ADDITIVE MANUFACTURING OF CERAMIC TURBINE COMPONENTS BY TRANSIENT LIQUID PHASE BONDING USING METAL OR CERAMIC BINDERS 审中-公开用金属或陶瓷粘合剂瞬时液相结合陶瓷涡轮部件的添加剂制造
公开(公告)号：WO2015012911A2
公开(公告)日：2015-01-29
申请号：PCT/US2014034939
申请日：2014-04-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MIRONETS SERGEY , COOK III GRANT O
CPC classification number: C04B35/65 , B33Y10/00 , B33Y70/00 , C04B35/117 , C04B35/44 , C04B35/46 , C04B35/48 , C04B35/486 , C04B35/565 , C04B35/584 , C04B35/6303 , C04B35/6316 , C04B2235/3217 , C04B2235/3225 , C04B2235/3244 , C04B2235/3281 , C04B2235/3298 , C04B2235/3409 , C04B2235/3418 , C04B2235/386 , C04B2235/3865 , C04B2235/40 , C04B2235/402 , C04B2235/6026 , C04B2235/665 , C04B2235/764 , C04B2235/9653
Abstract: A ceramic turbine component is formed by a process including mixing a ceramic powder with an inorganic binder powder. The powder mixture is then formed into a turbine component that is subsequently densified by transient liquid phase sintering. In an embodiment, the turbine component may be formed by an additive manufacturing process such as selective laser sintering.
Abstract translation: 陶瓷涡轮机部件通过包括将陶瓷粉末与无机粘合剂粉末混合的工艺形成。 然后将粉末混合物成形为涡轮机部件，随后通过瞬时液相烧结使其变得致密。 在一个实施例中，涡轮机部件可以通过诸如选择性激光烧结的增材制造工艺形成。
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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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5.发明公开ADDITIVE MANUFACTURING OF CERAMIC TURBINE COMPONENTS BY TRANSIENT LIQUID PHASE BONDING USING METAL OR CERAMIC BINDERS 审中-公开添加剂制造陶瓷涡轮部件BY临时液体相结合物使用金属或陶瓷关系
公开(公告)号：EP2989064A4
公开(公告)日：2017-01-11
申请号：EP14829417
申请日：2014-04-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MIRONETS SERGEY , COOK III GRANT O
CPC classification number: C04B35/65 , B33Y10/00 , B33Y70/00 , C04B35/117 , C04B35/44 , C04B35/46 , C04B35/48 , C04B35/486 , C04B35/565 , C04B35/584 , C04B35/6303 , C04B35/6316 , C04B2235/3217 , C04B2235/3225 , C04B2235/3244 , C04B2235/3281 , C04B2235/3298 , C04B2235/3409 , C04B2235/3418 , C04B2235/386 , C04B2235/3865 , C04B2235/40 , C04B2235/402 , C04B2235/6026 , C04B2235/665 , C04B2235/764 , C04B2235/9653
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Patent Agency Ranking6.发明公开BONDED MULTI-PIECE GAS TURBINE ENGINE COMPONENT 审中-公开GEBONDETE MEHRTEILIGE GASTURBINENMOTORKOMPONENTE
公开(公告)号：EP3080401A4
公开(公告)日：2017-08-30
申请号：EP14859735
申请日：2014-11-05
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MCCAFFREY MICHAEL G , ALVANOS IOANNIS , ABBOTT MICHAEL G , COOK III GRANT O
CPC classification number: F01D5/147 , F01D5/18 , F01D5/282 , F01D5/284 , F01D5/326 , F02C3/04 , F02C7/12 , F05D2220/32 , F05D2230/236 , F05D2230/51 , F05D2240/11 , F05D2240/12 , F05D2300/6033 , Y02T50/672
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公开(公告)号：EP2923054A4
公开(公告)日：2015-12-02
申请号：EP13857341
申请日：2013-10-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor： COOK III GRANT O
IPC: F02C7/14 , B29C70/06 , B32B1/08 , B32B15/08 , B32B27/28 , C23C18/16 , C25D1/02 , C25D5/56 , C25D7/04 , F02K3/00 , F16L9/12
CPC classification number: F02C7/04 , B32B15/08 , B32B27/281 , B32B27/288 , B32B2255/06 , B32B2255/26 , B32B2307/306 , B32B2307/54 , B32B2307/558 , B32B2307/714 , C23C18/1605 , C23C18/1616 , C23C18/165 , C25D1/02 , C25D5/022 , C25D5/56 , C25D7/04 , F02C7/14 , F05D2230/90 , F16L9/12 , Y10T428/24967 , Y10T428/26
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8.发明公开PLATED POLYMER COMPONENTS FOR A GAS TURBINE ENGINE 审中-公开PLATTIERTE POLYMERKOMPONENTENFÜREINEN GASTURBINENMOTOR
公开(公告)号：EP3019722A4
公开(公告)日：2017-05-10
申请号：EP14823557
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： DACUNHA NELSON , BARNETT BARRY , LOMASNEY GARY M , PARKOS JOSEPH , ROACH JAMES T , LEVASSEUR GLENN , WATSON CHARLES R , XU JINQUAN , COOK III GRANT O , KERSEY RAYMOND K , TWELVES WENDELL V , BUGAJ SHARI L
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。 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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9.发明公开ADDITIVE MANUFACTURING OF CERAMIC TURBINE COMPONENTS BY PARTIAL TRANSIENT LIQUID PHASE BONDING USING METAL BINDERS 审中-公开部分瞬间液相管陶瓷涡轮机部件的添加制造绑定应该使用金属领带
公开(公告)号：EP2989065A4
公开(公告)日：2016-07-20
申请号：EP14840617
申请日：2014-04-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MIRONETS SERGEY , COOK III GRANT O
CPC classification number: C04B35/653 , B22F3/1055 , B22F5/009 , B28B1/001 , B33Y10/00 , C04B35/10 , C04B35/565 , C04B35/584 , C22C29/065 , C22C29/12 , C22C29/16 , F05D2230/30 , Y02P10/295
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10.发明公开BONDED MULTI-PIECE GAS TURBINE ENGINE COMPONENT 审中-公开GEBONDETE MEHRTEILIGE GASTURBINENMOTORKOMPONENTE
公开(公告)号：EP3049627A4
公开(公告)日：2017-06-14
申请号：EP14847036
申请日：2014-09-08
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ROBERGE GARY , COOK III GRANT O
IPC: F01D5/14 , B23K1/00 , B23K20/00 , B23K20/02 , B23K101/00 , B23K103/00 , B23K103/08 , B23K103/18 , B32B37/12 , F01D5/18 , F01D5/28 , F01D25/00 , F02C7/00 , F16B11/00
CPC classification number: F01D5/147 , B23K1/0018 , B23K20/02 , B23K2201/001 , B23K2203/08 , B23K2203/18 , B23K2203/26 , B23K2203/52 , B32B37/12 , B32B2311/00 , B32B2315/02 , F01D5/14 , F01D5/186 , F01D5/187 , F01D5/189 , F01D5/28 , F01D5/284 , F05D2220/32 , F05D2230/236 , F05D2230/60 , F05D2260/202 , F05D2300/131 , F05D2300/222 , F05D2300/228 , F05D2300/608 , Y02T50/672 , Y02T50/673 , Y02T50/676
Abstract: A component includes a component body that is configured for use in a gas turbine engine. The component body includes first and second structural segments that are bonded to each other in at least one diffusion joint. The first and second structural segments are formed of, respectively, first and second materials. The first and second materials are different base-metal alloys, a metallic alloy and a ceramic-based material, or ceramic-based materials that differ by at least one of composition and microstructure.
Abstract translation: 部件包括配置用于燃气涡轮发动机的部件主体。 部件主体包括在至少一个扩散接头中彼此接合的第一和第二结构段。 第一和第二结构段分别由第一和第二材料形成。 第一和第二材料是不同的基础金属合金，金属合金和陶瓷基材料，或者陶瓷基材料，其组成和微结构中的至少一个不同。
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