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31.发明公开IMPROVED OPERABILITY GEARED TURBOFAN ENGINE INCLUDING COMPRESSOR SECTION VARIABLE GUIDE VANES 审中-公开牛皮癣菌MIT VERBESSERTER BEDIENBARKEIT MITVERÄNDERLICHENVERDICHTERABSCHNITTLEITSCHAUFELN
公开(公告)号：EP2909460A4
公开(公告)日：2016-07-20
申请号：EP13845694
申请日：2013-10-03
Applicant: UNITED TECHNOLOGIES CORP
Inventor： LEVASSEUR GLENN , SUCIU GABRIEL L , STETSON GARY M
CPC classification number: F01D17/162 , F02C7/36 , F02C9/20 , F05D2260/4031
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公开(公告)号：EP3019723A4
公开(公告)日：2017-05-10
申请号：EP14823763
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ROACH JAMES T , WATSON CHARLES R , COOK GRANT O , BARNETT BARRY , BUGAJ SHARI J , LEVASSEUR GLENN
IPC: F02C7/00 , B05D1/00 , C25D1/02 , C25D5/56 , F01D5/12 , F01D5/28 , F01D25/24 , F02C7/30 , F04D29/38 , F04D29/40
CPC classification number: F04D29/023 , B64D33/06 , B64D2033/0206 , C23C18/1605 , C23C18/1641 , C23C18/1651 , C23C18/1653 , C25D5/022 , C25D5/10 , C25D5/12 , C25D5/16 , C25D5/56 , F01D5/282 , F01D5/288 , F01D5/3092 , F01D5/34 , F01D25/005 , F01D25/02 , F04D29/322 , F04D29/324 , F04D29/522 , F04D29/542 , F05D2220/36 , F05D2250/181 , F05D2250/182 , F05D2250/61 , F05D2300/10 , F05D2300/43 , F05D2300/512 , F05D2300/611 , Y02T50/672 , Y02T50/673
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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
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
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公开(公告)号：EP2815104A4
公开(公告)日：2016-01-06
申请号：EP13784491
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor： LEVASSEUR GLENN , PIETRASZKIEWICZ EDWARD F
CPC classification number: F01D25/14 , F01D5/186 , F01D9/065 , F05D2240/81 , F05D2250/182 , F05D2250/183 , F05D2250/324 , F05D2260/202 , F23R3/002 , F23R2900/03042 , Y02T50/676 , Y10T29/49229 , Y10T29/49323
Abstract: A gas turbine engine component includes a wall having first and second wall surfaces and a cooling hole extending through the wall. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface and a diffusing section in communication with the inlet and extending to the outlet. The diffusing section includes a plurality of crenellation features that encourage lateral spreading of cooling air flowing through the cooling hole.
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35.发明公开
公开(公告)号：EP2815113A4
公开(公告)日：2015-12-30
申请号：EP13785247
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor： XU JINQUAN , LEVASSEUR GLENN
CPC classification number: F01D5/186 , F01D9/065 , F05D2240/81 , F05D2260/202 , F23R2900/03042 , Y02T50/676
Abstract: A gas turbine engine component includes a wall having first and second wall surfaces, a cooling hole extending through the wall and a convexity. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section and a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section. The convexity is located near the outlet.
Abstract translation: 燃气涡轮发动机部件包括具有第一和第二壁表面的壁，延伸穿过壁的冷却孔和凸起。 冷却孔包括位于第一壁表面处的入口，位于第二壁表面处的出口，从入口下游延伸的计量部分和从计量部分延伸到出口的扩散部分。 扩散部分包括从计量部分纵向和横向分叉的第一凸角和邻近第一凸角并从计量部分纵向和横向发散的第二凸角。 凸起位于出口附近。
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Patent Agency Ranking
公开(公告)号：EP3019727A4
公开(公告)日：2017-05-10
申请号：EP14823873
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ROACH JAMES T , BARNETT BARRY , COOK GRANT O III , WATSON CHARLES R , BUGAJ SHARI L , LEVASSEUR GLENN , WALL SARAH M , HERTEL CHRISTOPHER J , ZIMMITTI JONATHAN F , BETTAGERE LAKSHMINARAYAN , DEHLAVI MAJIDULLAH , WALTER BRIAN D , ALARCON ANDREW G , MARTIN OCTAVIO , ROBERTSON THOMAS J JR , BEAUDRY AARON , SCALIA JEFFREY J , OTT JOE , WASSEL JOSEPH J
IPC: F02C7/30 , C23C18/16 , C23C26/00 , C25D1/00 , C25D7/00 , F01D5/28 , F01D9/00 , F01D25/00 , F01D25/24
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
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37.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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公开(公告)号：EP2861847A4
公开(公告)日：2016-07-27
申请号：EP13804715
申请日：2013-06-14
Applicant: UNITED TECHNOLOGIES CORP , GKN AEROSPACE SWEDEN AB
Inventor： MOUNTZ DARYL B , KAPUSTKA THEODORE W , LEVASSEUR GLENN , BORG MARCUS , BERGLUND JOAKIM , SVAHN ANDERS , OCKBORN JOHAN , PETTERSSON BENGT
CPC classification number: F01D25/005 , F01D21/045 , F01D25/162 , F01D25/24 , F01D25/30 , F02C9/18 , F02K1/386 , F05D2220/32 , F05D2230/21 , F05D2230/232 , F05D2230/25 , F05D2230/54 , F05D2260/941 , F05D2300/175 , F05D2300/176 , F05D2300/177 , F05D2300/502
Abstract: A turbine exhaust case has an outer housing to be secured within a gas turbine engine and a central hub. Struts extend between the outer housing and the central hub. The struts are formed at least in part of a first material. The central hub is formed at least in part of a second material.
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公开(公告)号：EP2815109A4
公开(公告)日：2016-03-02
申请号：EP13785031
申请日：2013-02-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor： LEVASSEUR GLENN , PIETRASZKIEWICZ EDWARD F , ZELESKY MARK F , MONGILLO DOMINIC J , KLINEFELTER KEVIN J , DOLL STEPHEN D , FRITCH MARKUS W
CPC classification number: B23H9/10 , B23H1/00 , B23H7/26 , B23H9/14 , F01D5/186 , F01D9/065 , F05D2240/81 , F05D2260/202 , F23R3/002 , F23R2900/03042 , Y02T50/676
Abstract: A method for forming a cooling hole extending from an inlet on a first surface of a wall to an outlet on a second surface of the wall includes forming a diffusing section of the cooling hole, and a trailing edge on the outlet by electrical discharge machining, and forming longitudinal lobes in the diffusing section. The metering section extends from the inlet on a first surface of the wall towards the second surface of the wall. The diffusing section extends from the outlet to one end of a metering section located between the inlet and the outlet. The outlet is substantially linear or convex at the trailing edge and the lobes are separated by longitudinal ridges.
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40.发明公开MULTI-LOBED COOLING HOLES IN GAS TURBINE ENGINE COMPONENTS HAVING THERMAL BARRIER COATINGS 审中-公开燃气涡轮发动机组件中带有隔热层的多层冷却孔
公开(公告)号：EP2870344A4
公开(公告)日：2015-08-26
申请号：EP13855260
申请日：2013-07-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor： XU JINQUAN , PIETRASZKIEWICZ EDWARD F , ZELESKY MARK F , LEVASSEUR GLENN , MONGILLO DOMINIC J
CPC classification number: B24C1/045 , B23K26/0622 , B23K26/082 , B23K26/146 , B23K26/389 , B23K2201/001 , B26F3/004 , F01D5/186 , F01D5/288 , F01D9/041 , F05D2240/81 , F05D2250/52 , F05D2250/70 , F05D2260/202 , F23R3/06 , F23R2900/00018 , F23R2900/03042 , Y02T50/676
Abstract: A gas turbine engine component includes a wall with an inner face and an outer skin. A plurality of cooling air holes extend from the inner face to the outer skin. The cooling holes include an inlet merging into a metering section, and a diffusion section downstream of the metering section, and extend to an outlet at the outer skin. The diffusion section includes a plurality of lobes. A coating layer is formed on the outer skin, with at least a portion of the plurality of lobes formed within the thermal barrier coating. A method of forming such a component is also disclosed.
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