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公开(公告)号：US20170307216A1
公开(公告)日：2017-10-26
申请号：US15134511
申请日：2016-04-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Edward R. Bareiss
Abstract: A method of fabricating a combustor thermal shield comprising a combustor panel, a cooling feature, and an attachment feature, the combustor thermal shield to be used in a gas turbine engine combustor, includes shaping a sheet of material used to form the combustor panel. The method also includes additively manufacturing the cooling feature onto the sheet of material forming the combustor panel. The method also includes attaching the attachment feature to the sheet of material forming the combustor panel. The method also includes curving the sheet of material forming the combustor panel to achieve a curve profile according to a design of the gas turbine engine combustor.
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2.发明申请Multi-Airfoil Split and Rejoin Method to Produce Enhanced Durability Coating 审中-公开多机翼拆分和再加工方法生产增强耐久性涂层公开(公告)号：US20150352649A1
公开(公告)日：2015-12-10
申请号：US14765467
申请日：2013-12-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Edward R. Bareiss , Russell J. Bergman , Bradley T. Duelm , Michael L. Miller , Paul M. Pellet
CPC classification number: B23K1/0018 , B23H7/02 , B23H9/10 , B23K31/02 , B23P6/007 , C23C4/02 , C23C4/18 , C23C14/02 , C23C14/30 , C23C14/325 , C23C14/58 , F01D5/005 , F01D9/041 , F01D9/044 , F01D9/065 , F05D2230/236 , F05D2230/64 , F05D2240/81 , F05D2300/607 , Y02T50/676
Abstract: A method for working an airfoil cluster is disclosed. The method may include attaching a first datum to a first portion of the airfoil cluster and a second datum to a second portion of the airfoil cluster; adding material to at least one of the first portion and the second portion; and joining the first portion to the second portion, the first and second datums substantially aligned in a common plane spaced away from the first and second portions.
Abstract translation: 公开了一种用于加工翼型组的方法。 该方法可以包括将第一基准附加到翼型群的第一部分，并将第二基准附接到翼型群的第二部分; 向所述第一部分和所述第二部分中的至少一个添加材料; 并且将所述第一部分接合到所述第二部分，所述第一和第二基准基本上在与所述第一和第二部分间隔开的公共平面中对准。
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Patent Agency Ranking
公开(公告)号：US10443846B2
公开(公告)日：2019-10-15
申请号：US15134511
申请日：2016-04-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Edward R. Bareiss
Abstract: A method of fabricating a combustor thermal shield comprising a combustor panel, a cooling feature, and an attachment feature, the combustor thermal shield to be used in a gas turbine engine combustor, includes shaping a sheet of material used to form the combustor panel. The method also includes additively manufacturing the cooling feature onto the sheet of material forming the combustor panel. The method also includes attaching the attachment feature to the sheet of material forming the combustor panel. The method also includes curving the sheet of material forming the combustor panel to achieve a curve profile according to a design of the gas turbine engine combustor.
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公开(公告)号：US10239142B2
公开(公告)日：2019-03-26
申请号：US14765467
申请日：2013-12-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Edward R. Bareiss , Russell J. Bergman , Bradley T. Duelm , Michael L. Miller , Paul M. Pellet
IPC: B23K1/00 , C23C14/30 , C23C14/32 , B23K31/02 , F01D5/00 , F01D9/04 , C23C4/02 , C23C4/18 , C23C14/02 , C23C14/58 , B23P6/00 , F01D9/06 , B23H7/02 , B23H9/10
Abstract: A method for working an airfoil cluster is disclosed. The method may include attaching a first datum to a first portion of the airfoil cluster and a second datum to a second portion of the airfoil cluster; adding material to at least one of the first portion and the second portion; and joining the first portion to the second portion, the first and second datums substantially aligned in a common plane spaced away from the first and second portions.
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公开(公告)号：US10584602B2
公开(公告)日：2020-03-10
申请号：US14762630
申请日：2013-12-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Edward R. Bareiss , Russell J. Bergman , Bradley T. Duelm , Michael L. Miller , Paul M. Pellet
IPC: B23P6/00 , F01D9/04 , F01D5/00 , B23K1/00 , F01D9/06 , F01D25/12 , F01D5/18 , B23H7/02 , B23H9/10 , B23K101/00
Abstract: A method for working an airfoil cluster is disclosed. The method may include attaching a first datum to a first portion of the airfoil cluster, and joining a second portion of the airfoil cluster to the first portion, the second portion having a second datum substantially aligned with the first datum in a common plane spaced away from the first and second portions.
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公开(公告)号：US10132176B2
公开(公告)日：2018-11-20
申请号：US14766477
申请日：2014-02-17
Applicant: United Technologies Corporation
Inventor： Edward R. Bareiss , Russell J. Bergman , Bradley T. Duelm , Michael L. Miller , Paul M. Pellet
IPC: F01D9/04 , B23H9/14 , B23K1/00 , B23K26/382 , B23K28/00 , F01D25/12 , F01D5/00 , F01D9/06 , F01D5/18 , B23K101/00
Abstract: A method of fabricating airfoil cluster includes providing an airfoil cluster that has a pair of spaced-apart airfoils that extend from a common platform wall. The airfoil cluster is then divided through the common platform wall to provide separate first and second airfoil segments. At least one cooling hole is then formed in at least one of the first and second airfoil segments. The segments are then metallurgically fused together in a distinct metallurgical joint in the common platform wall.
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公开(公告)号：US20150369070A1
公开(公告)日：2015-12-24
申请号：US14762630
申请日：2013-12-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Edward R. Bareiss , Russell J. Bergman , Bradley T. Duelm , Michael L. Miller , Paul M. Pellet
Abstract: A method for working an airfoil cluster is disclosed. The method may include attaching a first datum to a first portion of the airfoil cluster, and joining a second portion of the airfoil cluster to the first portion, the second portion having a second datum substantially aligned with the first datum in a common plane spaced away from the first and second portions.
Abstract translation: 公开了一种用于加工翼型组的方法。 该方法可以包括将第一基准附接到翼型群的第一部分，以及将翼型群的第二部分连接到第一部分，第二部分具有基本上与第一基准对准的公共平面间隔开的第二基准 从第一和第二部分。
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