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公开(公告)号：US20150337672A1
公开(公告)日：2015-11-26
申请号：US14708746
申请日：2015-05-11
Applicant: United Technologies Corporation
Inventor： Michael G. McCaffrey , Alan C. Barron
CPC classification number: F01D11/08 , B25J9/1697 , B25J11/0055 , F01D9/02 , F01D9/04 , F01D11/12 , F01D11/122 , F01D25/145 , F01D25/24 , F05D2220/30 , F05D2230/90 , F05D2240/55 , Y10S901/10
Abstract: A blade outer air seal for a turbomachine includes a base portion configured to attach to a turbomachine housing, a thermal coating disposed on the base portion, and at least one groove defined in an external surface of the thermal coating. The groove can be machined. A method of manufacturing a blade outer air seal includes disposing a thermal coating on a base portion, and machining at least one groove into the thermal coating. The method can also include using an automated force sensing and vision sensing equipped robotic system.
Abstract translation: 用于涡轮机的叶片外部空气密封件包括构造成附接到涡轮机壳体的基部部分，设置在基部部分上的热涂层以及限定在热涂层的外表面中的至少一个凹槽。 凹槽可加工。 一种制造叶片外部空气密封件的方法包括将热涂层设置在基部上，并将至少一个凹槽加工到热涂层中。 该方法还可以包括使用自动力感测和视觉感测装备的机器人系统。
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22.发明申请公开(公告)号：US20140255158A1
公开(公告)日：2014-09-11
申请号：US13725229
申请日：2012-12-21
Applicant: United Technologies Corporation
Inventor： Steven W. Burd , Alan C. Barron
Abstract: A method of coating a component having a multiple of cooling holes includes removing at least a portion of a prior coating; directing a gas through at least one of the multiple of cooling holes; and applying a coat layer while directing the gas through at least one of the
Abstract translation: 涂覆具有多个冷却孔的部件的方法包括去除至少一部分现有涂层; 引导气体通过多个冷却孔中的至少一个; 并且在引导气体通过所述气体中的至少一个的同时施加涂层
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公开(公告)号：US11473433B2
公开(公告)日：2022-10-18
申请号：US16043257
申请日：2018-07-24
Applicant: United Technologies Corporation
Inventor： Anton G. Banks , Alan C. Barron
Abstract: An airfoil for a gas turbine engine includes a substrate portion extending from an airfoil leading edge to an airfoil trailing edge portion. The airfoil trailing edge portion includes a flared portion wherein a substrate portion thickness increases along a camber line of the airfoil, and a trailing edge defined as a full constant radius extending from a pressure side of the airfoil to a suction side of the airfoil. A coating portion includes a coating applied over at least a portion of the substrate portion.
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公开(公告)号：US11334051B2
公开(公告)日：2022-05-17
申请号：US16446463
申请日：2019-06-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： James Tilsley Auxier , Alan C. Barron , Norman W. Cofalka , Joel H. Wagner
IPC: G05B19/4097 , F01D5/14
Abstract: A system for automated adaptive manufacturing of airfoil castings is disclosed. The system may receive a three dimensional scan of a work piece. The system may compare the three dimensional scan to a digital model of the work piece. The system may identify an area of dimensional abnormality on the work piece based on the comparison. The system may alter the area of dimensional abnormality on the work piece.
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公开(公告)号：US11319814B2
公开(公告)日：2022-05-03
申请号：US16403208
申请日：2019-05-03
Applicant: United Technologies Corporation
Inventor： James Tilsley Auxier , Norman W. Cofalka , Alan C. Barron
IPC: B23P15/02 , B23P15/04 , B33Y10/00 , B33Y50/02 , B33Y80/00 , B22D25/02 , B23P15/00 , F01D5/14 , F02C3/04 , F02C3/14 , F02C7/36 , F02C9/18 , B23P13/02
Abstract: A method of manufacturing a casting is provided and includes establishing desired dimensions of a nominal casting, executing a casting process to produce multiple actual castings with each of the multiple actual castings having respective dimensions that differ from each other and from the desired dimensions of the nominal casting and engaging one or more tools to adaptively machine, without rigidly-programmed toolpaths, each of the multiple actual castings to reduce the respective differences between the actual dimensions of each of the multiple actual castings and the desired dimensions.
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Patent Agency Ranking
公开(公告)号：US11143030B2
公开(公告)日：2021-10-12
申请号：US13725229
申请日：2012-12-21
Applicant: United Technologies Corporation
Inventor： Steven W. Burd , Alan C. Barron
Abstract: A method of coating a component having a multiple of cooling holes includes removing at least a portion of a prior coating; directing a gas through at least one of the multiple of cooling holes; and applying a coat layer while directing the gas through at least one of the
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公开(公告)号：US11053855B2
公开(公告)日：2021-07-06
申请号：US16433896
申请日：2019-06-06
Applicant: United Technologies Corporation
Inventor： Brian T. Hazel , Alan C. Barron , Mary Catherine Gurak
IPC: C23C14/08 , C23C14/30 , C23C16/06 , C23C16/455 , F02C7/24
Abstract: A process for coating a component includes applying a bond coat on a substrate of a component; applying a thermal barrier material to the bond coat; and applying a conforming reflective layer to the thermal barrier material, the conforming reflective layer conforming to porous microstructure of the ceramic coating.
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公开(公告)号：US20200347729A1
公开(公告)日：2020-11-05
申请号：US16403208
申请日：2019-05-03
Applicant: United Technologies Corporation
Inventor： James Tilsley Auxier , Norman W. Cofalka , Alan C. Barron
Abstract: A method of manufacturing a casting is provided and includes establishing desired dimensions of a nominal casting, executing a casting process to produce multiple actual castings with each of the multiple actual castings having respective dimensions that differ from each other and from the desired dimensions of the nominal casting and engaging one or more tools to adaptively machine, without rigidly-programmed toolpaths, each of the multiple actual castings to reduce the respective differences between the actual dimensions of each of the multiple actual castings and the desired dimensions.
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公开(公告)号：US10309243B2
公开(公告)日：2019-06-04
申请号：US14708746
申请日：2015-05-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Michael G McCaffrey , Alan C. Barron
Abstract: A blade outer air seal for a turbomachine includes a base portion configured to attach to a turbomachine housing, a thermal coating disposed on the base portion, and at least one groove defined in an external surface of the thermal coating. The groove can be machined. A method of manufacturing a blade outer air seal includes disposing a thermal coating on a base portion, and machining at least one groove into the thermal coating. The method can also include using an automated force sensing and vision sensing equipped robotic system.
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公开(公告)号：US09844834B2
公开(公告)日：2017-12-19
申请号：US14518563
申请日：2014-10-20
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Richard L. Smith , Alan C. Barron
IPC: B23K26/38 , B23K26/382 , B23K26/06 , B23K26/60 , B23K101/00 , B23K101/34
CPC classification number: B23K26/389 , B23K26/0617 , B23K26/60 , B23K2101/001 , B23K2101/34
Abstract: A method for drilling holes in a part includes positioning the part relative to a laser source, applying a first stress to the part, and applying a laser from the laser source to the part to drill a hole therein, wherein the first stress which is present during the application of the laser counteracts a second stress induced by the application of the laser.
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