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1.发明申请公开(公告)号：US20180236615A1
公开(公告)日：2018-08-23
申请号：US15439451
申请日：2017-02-22
摘要： Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.
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2.发明申请公开(公告)号：US20180236556A1
公开(公告)日：2018-08-23
申请号：US15439529
申请日：2017-02-22
IPC分类号： B22F5/04 , B22F3/105 , B22F7/08 , B22F7/06 , B22D29/00 , B22D25/02 , B33Y10/00 , B33Y80/00 , F01D5/12
CPC分类号： B22F5/04 , B22D25/02 , B22D29/002 , B22F3/1055 , B22F7/062 , B22F7/08 , B22F2005/103 , B22F2007/068 , B33Y10/00 , B33Y80/00 , F01D5/20 , F05D2230/14 , F05D2230/211 , F05D2230/31 , F05D2240/307 , F05D2300/175 , F05D2300/607
摘要： Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.
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公开(公告)号：US20190143444A1
公开(公告)日：2019-05-16
申请号：US15811293
申请日：2017-11-13
IPC分类号： B23K15/00 , B33Y10/00 , B33Y30/00 , B33Y70/00 , B23K15/08 , B23K26/082 , B23K26/342 , B23K35/02
摘要： The present disclosure generally relates to methods and apparatuses for additive manufacturing using foil-based build materials. Such methods and apparatuses eliminate several drawbacks of conventional powder-based methods, including powder handling, recoater jams, and health risks. In addition, the present disclosure provides methods and apparatuses for compensation of in-process warping of build plates and foil-based build materials.
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公开(公告)号：US20180238173A1
公开(公告)日：2018-08-23
申请号：US15439584
申请日：2017-02-22
IPC分类号： F01D5/14 , B22F3/105 , B22F5/04 , B22F7/08 , B22F7/06 , B22D25/02 , B22D29/00 , B33Y10/00 , B33Y80/00 , F01D9/04 , F01D5/28
CPC分类号： F01D5/147 , B22D25/02 , B22D29/002 , B22F3/1055 , B22F5/04 , B22F7/08 , B22F2007/068 , B33Y10/00 , B33Y80/00 , F01D5/005 , F01D5/284 , F05D2230/10 , F05D2230/21 , F05D2230/22 , F05D2230/31 , F05D2240/12 , F05D2240/125 , F05D2240/307
摘要： Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.
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公开(公告)号：US20180236616A1
公开(公告)日：2018-08-23
申请号：US15439643
申请日：2017-02-22
摘要： Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.
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公开(公告)号：US20170056975A1
公开(公告)日：2017-03-02
申请号：US14837059
申请日：2015-08-27
发明人： William Thomas CARTER , Mark Kevin MEYER , Andrew David DEAL , Mark Allen CHEVERTON , Samar Jyoti KALITA , Michael Francis Xavier GIGLIOTTI
CPC分类号： B33Y80/00 , B22F3/1055 , B22F5/04 , B22F7/062 , B22F2003/1056 , B22F2999/00 , B33Y10/00 , B33Y30/00 , B33Y50/02 , C21D1/42 , Y02P10/253 , Y02P10/295 , B22F2203/03 , B22F2203/11
摘要： The disclosure relates to an apparatus for manufacturing a metallic component, and corresponding methods. The apparatus may include a build plate with a build surface and an aperture. The apparatus may also include an actuator operable to translate a metallic component such that an end portion of the metallic component is positioned within the aperture of the build plate and below the build surface. The apparatus may further include a seal coupled within the aperture of the build plate and configured to engage the end portion of the metallic component. The aperture of the build plate, the seal, and the end portion of the metallic component may cooperate to form a powder bed to hold metallic powder therein. The apparatus may also include an external heat control mechanism operable to form a predetermined temperature profile of the end portion of the component to prevent cracking of the component.
摘要翻译： 本公开涉及一种用于制造金属部件的装置以及相应的方法。 该装置可以包括具有构建表面和孔的构建板。 该装置还可以包括可操作以平移金属部件的致动器，使得金属部件的端部位于构建板的孔内并在构建表面下方。 该设备还可以包括联接在构建板的孔内并被配置为接合金属部件的端部的密封件。 构建板，密封件和金属部件的端部的孔可以协作以形成粉末床以将金属粉末保持在其中。 该装置还可以包括外部热控制机构，其可操作以形成部件的端部的预定温度分布，以防止部件的开裂。
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7.发明申请公开(公告)号：US20190143587A1
公开(公告)日：2019-05-16
申请号：US15811196
申请日：2017-11-13
IPC分类号： B29C64/223 , B29C64/268 , B29C64/147
摘要： The present disclosure generally relates to methods and apparatuses for additive manufacturing using foil-based build materials. Such methods and apparatuses eliminate several drawbacks of conventional powder-based methods, including powder handling, recoater jams, and health risks. In addition, the present disclosure provides methods and apparatuses for compensation of in-process warping of build plates and foil-based build materials, in-process monitoring, and closed loop control.
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公开(公告)号：US20190143443A1
公开(公告)日：2019-05-16
申请号：US15811283
申请日：2017-11-13
IPC分类号： B23K15/00 , B33Y10/00 , B33Y30/00 , B33Y70/00 , B23K15/08 , B23K26/082 , B23K26/14 , B23K26/342
摘要： The present disclosure generally relates to methods and apparatuses for additive manufacturing using foil-based build materials. Such methods and apparatuses eliminate several drawbacks of conventional powder-based methods, including powder handling, recoater jams, and health risks. In addition, the present disclosure provides methods and apparatuses for compensation of in-process warping of build plates and foil-based build materials, in-process monitoring, and closed loop control.
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公开(公告)号：US20180236558A1
公开(公告)日：2018-08-23
申请号：US15439592
申请日：2017-02-22
IPC分类号： B22F5/04 , B22F3/105 , B22F7/06 , B22F7/08 , B22D29/00 , B22D25/02 , B33Y10/00 , B33Y80/00 , F01D5/00 , F01D9/04
CPC分类号： B22F5/04 , B22D25/02 , B22D29/002 , B22F3/1055 , B22F7/062 , B22F7/08 , B22F2007/068 , B33Y10/00 , B33Y80/00 , F01D5/005 , F05D2230/21 , F05D2230/22 , F05D2230/80 , F05D2240/125 , F05D2240/307
摘要： Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.
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公开(公告)号：US20180236557A1
公开(公告)日：2018-08-23
申请号：US15439548
申请日：2017-02-22
IPC分类号： B22F5/04 , B22F3/105 , B22F7/08 , B22F7/06 , B22D25/02 , B22D29/00 , B33Y10/00 , B33Y80/00 , F01D9/04 , F01D5/14 , F01D5/28
摘要： Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.
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