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1.
公开(公告)号:WO2015006479A1
公开(公告)日:2015-01-15
申请号:PCT/US2014/045998
申请日:2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
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。 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:WO2014182519A3
公开(公告)日:2014-11-13
申请号:PCT/US2014/036087
申请日:2014-04-30
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: WOLFF, Eric L. , SHERRILL, Brent L. , AJAMI, Andre M. , WINSTON, Kenneth W. , PASCU, Victor , VESSA, Phillip , DACUNHA, Nelson
Abstract: A gas turbine engine inlet door control system includes an actuator, an engine controller and a door controller. The actuator opens and closes an inlet door of a gas turbine engine. The engine controller determines an intermediate door position based upon one or more engine start factors. The door controller operates the actuator to open the inlet door to the intermediate door position based on the one or more engine start factors.
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公开(公告)号:EP3016862B1
公开(公告)日:2019-01-02
申请号:EP14794190.0
申请日:2014-04-30
Applicant: United Technologies Corporation
Inventor: WOLFF, Eric L. , SHERRILL, Brent L. , AJAMI, Andre M. , WINSTON, Kenneth W. , PASCU, Victor , VESSA, Phillip , DACUNHA, Nelson
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公开(公告)号:EP3019722B1
公开(公告)日:2018-11-21
申请号:EP14823557.5
申请日:2014-07-09
Applicant: United Technologies Corporation
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.
IPC: F02C7/00 , F02C7/30 , C25D5/56 , C25D1/00 , C25D7/00 , C23C18/16 , C23C18/31 , F01D5/28 , F01D5/30 , F01D9/04 , F01D25/00 , F01D25/30 , F01D25/24 , F02C7/04 , C25D5/02 , C25D5/10 , C25D7/04 , C25D7/06
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.
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5.
公开(公告)号:EP3019722A1
公开(公告)日:2016-05-18
申请号:EP14823557.5
申请日:2014-07-09
Applicant: United Technologies Corporation
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.
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6.
公开(公告)号:EP3016862A2
公开(公告)日:2016-05-11
申请号:EP14794190.0
申请日:2014-04-30
Applicant: United Technologies Corporation
Inventor: WOLFF, Eric L. , SHERRILL, Brent L. , AJAMI, Andre M. , WINSTON, Kenneth W. , PASCU, Victor , VESSA, Phillip , DACUNHA, Nelson
CPC classification number: F02C7/268 , B64D41/00 , B64D2033/0213 , F01D19/00 , F02C7/04 , F05D2220/50 , F05D2260/85
Abstract: A gas turbine engine inlet door control system includes an actuator, an engine controller and a door controller. The actuator opens and closes an inlet door of a gas turbine engine. The engine controller determines an intermediate door position based upon one or more engine start factors. The door controller operates the actuator to open the inlet door to the intermediate door position based on the one or more engine start factors.
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