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1.发明申请公开(公告)号：US20200024998A1
公开(公告)日：2020-01-23
申请号：US16362878
申请日：2019-03-25
Applicant: United Technologies Corporation
Inventor： Jorge I. Farah , Jonathan P. Burt , Dana P. Stewart
Abstract: A turbine engine vane arrangement and a method for manufacturing a turbine engine vane arrangement are provided. The vane arrangement includes a plurality of vane arrangement segments arranged circumferentially around an axial centerline. Each of the vane arrangement segments includes an airfoil that extends radially between a first platform segment and a second platform segment. The first platform segment extends circumferentially between a first mate face and a second mate face. The first mate face of a first of the vane arrangement segments is bonded to the second mate face of a second of the vane arrangement segments.
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2.发明授权公开(公告)号：US10240468B2
公开(公告)日：2019-03-26
申请号：US14432432
申请日：2013-01-09
Applicant: United Technologies Corporation
Inventor： Jorge I. Farah , Jonathan P. Burt , Dana P. Stewart
Abstract: A turbine engine vane arrangement and a method for manufacturing a turbine engine vane arrangement are provided. The vane arrangement includes a plurality of vane arrangement segments arranged circumferentially around an axial centerline. Each of the vane arrangement segments includes an airfoil that extends radially between a first platform segment and a second platform segment. The first platform segment extends circumferentially between a first mate face and a second mate face. The first mate face of a first of the vane arrangement segments is bonded to the second mate face of a second of the vane arrangement segments.
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Patent Agency Ranking
公开(公告)号：US20160053622A1
公开(公告)日：2016-02-25
申请号：US14779846
申请日：2014-04-01
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Jorge I. Farah , Conway Chuong , Dana P. Stewart
CPC classification number: F01D9/042 , F01D25/005 , F01D25/162 , F05D2240/12
Abstract: A stator vane arrangement for a turbine engine includes a first vane platform, a second vane platform and a plurality of stator vanes extending radially between the first and the second vane platforms. The first and the second vane platforms extend circumferentially around an axis, and the first vane platform includes an aperture. The stator vanes are arranged circumferentially around the axis, and include a first stator vane that extends radially into the aperture and is fastened to the first vane platform.
Abstract translation: 用于涡轮发动机的定子叶片装置包括第一叶片平台，第二叶片平台和在第一和第二叶片平台之间径向延伸的多个定子叶片。 第一和第二叶片平台围绕轴线周向延伸，并且第一叶片平台包括孔。 定子叶片围绕轴线周向地布置，并且包括第一定子叶片，该第一定子叶片径向延伸到孔中并且紧固到第一叶片平台。
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4.发明申请TURBINE ENGINE VANE ARRANGEMENT HAVING A PLURALITY OF INTERCONNECTED VANE ARRANGEMENT SEGMENTS 审中-公开涡轮发动机叶片布置具有多个互连的叶片布置部分公开(公告)号：US20150292343A1
公开(公告)日：2015-10-15
申请号：US14432432
申请日：2013-01-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Jorge I. Farah , Jonathan P. Burt , Dana P. Stewart
CPC classification number: F01D9/042 , B23P15/04 , F01D9/044 , F04D29/544
Abstract: A turbine engine vane arrangement and a method for manufacturing a turbine engine vane arrangement are provided. The vane arrangement includes a plurality of vane arrangement segments arranged circumferentially around an axial centerline. Each of the vane arrangement segments includes an airfoil that extends radially between a first platform segment and a second platform segment. The first platform segment extends circumferentially between a first mate face and a second mate face. The first mate face of a first of the vane arrangement segments is bonded to the second mate face of a second of the vane arrangement segments.
Abstract translation: 提供了一种涡轮发动机叶片装置和用于制造涡轮发动机叶片装置的方法。 叶片装置包括沿轴向中心线周向布置的多个叶片装置段。 每个叶片装置段包括在第一平台段和第二平台段之间径向延伸的翼型件。 第一平台段在第一配合面和第二配合面之间周向延伸。 第一叶片装置段的第一配合面接合到第二叶片装置段的第二配合面。
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公开(公告)号：US10344606B2
公开(公告)日：2019-07-09
申请号：US14779846
申请日：2014-04-01
Applicant: United Technologies Corporation
Inventor： Jorge I. Farah , Conway Chuong , Dana P. Stewart
Abstract: A stator vane arrangement for a turbine engine includes a first vane platform, a second vane platform and a plurality of stator vanes extending radially between the first and the second vane platforms. The first and the second vane platforms extend circumferentially around an axis, and the first vane platform includes an aperture. The stator vanes are arranged circumferentially around the axis, and include a first stator vane that extends radially into the aperture and is fastened to the first vane platform.
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公开(公告)号：US09925623B2
公开(公告)日：2018-03-27
申请号：US13631321
申请日：2012-09-28
Applicant: United Technologies Corporation
Inventor： Dana P. Stewart , Edward R. Szela , John H. Finn
CPC classification number: B23K31/02 , B23K1/0018 , B23K1/008 , B23K9/007 , B23K37/0443 , B23K2101/001 , F01D9/04 , F01D25/24 , F05D2230/237 , Y10T29/49771 , Y10T29/49968
Abstract: A case assembly includes a plurality of segments, at least one braze joint, and one or more welds. The braze joint connects the plurality of segments together and the one or more welds extend across adjacent segments.
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公开(公告)号：US20140093372A1
公开(公告)日：2014-04-03
申请号：US13631321
申请日：2012-09-28
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Dana P. Stewart , Edward R. Szela , John H. Finn
CPC classification number: B23K31/02 , B23K1/0018 , B23K1/008 , B23K9/007 , B23K37/0443 , B23K2101/001 , F01D9/04 , F01D25/24 , F05D2230/237 , Y10T29/49771 , Y10T29/49968
Abstract: A case assembly includes a plurality of segments, at least one braze joint, and one or more welds. The braze joint connects the plurality of segments together and the one or more welds extend across adjacent segments.
Abstract translation: 壳体组件包括多个段，至少一个钎焊接头和一个或多个焊缝。 钎焊接头将多个段连接在一起，并且一个或多个焊缝在相邻的段之间延伸。
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