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公开(公告)号:US10940535B2
公开(公告)日:2021-03-09
申请号:US16003988
申请日:2018-06-08
Applicant: General Electric Company
Inventor: Ananda Barua , Sathyanarayanan Raghavan , Ken Salas Nobrega , Arunkumar Natarajan , Vadim Bromberg , Raymond Floyd Martell , Meghan J. Borz
Abstract: A binder jet printed article includes a part having a top portion, a bottom portion, and an overhang extending from the top portion and a support structure formed around the part that may block deformation of the part during post-printing thermal processing. The support structure includes a skid positioned adjacent to the bottom portion that may support the part, a first plurality of support features disposed along an outer perimeter of the skid, and a second plurality of support features disposed on the top portion of the printed part. The first and second plurality of support features form a lattice around the printed part such that the printed part is nested within the support structure.
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公开(公告)号:US10781721B2
公开(公告)日:2020-09-22
申请号:US15892735
申请日:2018-02-09
Applicant: General Electric Company
Inventor: Ananda Barua , Joshua Tyler Mook , Raymond Floyd Martell , Changjie Sun , Gautam Naik , Jordan Paule Tesorero , Aigbedion Akwara
IPC: F01D25/28 , F01D9/04 , B33Y80/00 , F01D9/06 , F01D25/16 , B29C64/00 , B22F5/00 , B33Y10/00 , B22F3/105
Abstract: Turbine center frames are provided. For example, a turbine center frame comprises an annular outer case and an annular hub. The hub is defined radially inward of the outer case such that the outer case circumferentially surrounds the hub. The turbine center frame further comprises an annular fairing extending between the outer case and the hub, a ligament extending from the fairing to the outer case to connect the fairing to the outer case, a plurality of struts extending from the hub to the outer case, and a boss structure defined on an outer surface of the outer case. The outer case, hub, fairing, ligament, plurality of struts, and boss structure are integrally formed as a single monolithic component. For instance, the turbine center frame is additively manufactured as an integral structure, and methods for manufacturing turbine center frames also are provided.
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公开(公告)号:US20190375006A1
公开(公告)日:2019-12-12
申请号:US16001565
申请日:2018-06-06
Applicant: General Electric Company
Inventor: Ananda Barua , Sathyanarayanan Raghavan , Ken Salas Nobrega , Vadim Bromberg , Arunkumar Natarajan
IPC: B22F3/00 , B33Y40/00 , B33Y80/00 , B33Y10/00 , B29C64/165 , B29C64/379 , B28B1/00 , C04B35/622 , C04B35/634 , C04B35/638 , C04B35/64
Abstract: A setter assembly for use in additive manufacturing a binder-jet part includes a base, a first setter component having a first setter portion and a second setter portion that may be removably coupled to the first setter portion and a plurality of protrusions disposed on and extending away from a surface of the base. The plurality of protrusions may align the base with the first setter component and enable coupling of the first setter component to the base. The setter assembly also includes a second setter component positioned between the base and the first setter component. The second setter component is disposed on the surface and the first setter component, the second setter component, and the base can be assembled onto a printed part such that at least a portion of the printed part is nested between the first setter component and the second setter component.
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公开(公告)号:US20230260687A1
公开(公告)日:2023-08-17
申请号:US17670836
申请日:2022-02-14
Applicant: General Electric Company
Inventor: Wanming Zhang , Ananda Barua , Shenyan Huang , Changjie Sun , Vandana Prabhakar Rallabandi , Anthony Joseph Vinciquerra , Min Zou
CPC classification number: H01F1/24 , C22C19/00 , H01F1/1475 , C22C2202/02
Abstract: Methods for manufacturing dual phase soft magnetic components include combining a plurality of soft ferromagnetic particles with a plurality of paramagnetic particles to form a component structure, wherein the plurality of soft ferromagnetic particles each comprise an electrically insulative coating, and, heat treating the component structure to consolidate the plurality of soft ferromagnetic particles with the plurality of paramagnetic particles.
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公开(公告)号:US11714938B2
公开(公告)日:2023-08-01
申请号:US16542860
申请日:2019-08-16
Applicant: General Electric Company
Inventor: Ananda Barua
CPC classification number: G06F30/23 , G06T17/20 , B33Y10/00 , B33Y50/02 , G06F2119/18 , G06T2219/012
Abstract: According to some embodiments, system and methods are provided comprising receiving, via a communication interface of a distortion and correction module comprising a processor, a defined geometry for one or more parts, wherein the parts are manufactured with an additive manufacturing machine; discretizing the defined geometry into a mesh including a plurality of nodes; predicting a distortion of a position of each node of the plurality of nodes; determining whether the predicted distortion position exceeds a pre-set tolerance; determining an adjusted pre-distortion position for each node of the plurality of nodes when the predicted distortion position exceeds the pre-set tolerance; predicting a distortion of the adjusted determined pre-distortion position for each node of the plurality of nodes; determining whether the distortion of the determined adjusted pre-distortion position exceeds the pre-set tolerance; and printing the part when one of the predicted distortion position and the predicted adjusted pre-distortion position is below the pre-set tolerance. Numerous other aspects are provided.
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公开(公告)号:US20230073194A1
公开(公告)日:2023-03-09
申请号:US17889852
申请日:2022-08-17
Applicant: General Electric Company
Inventor: Mary Kathryn Thompson , Arunkumar Natarajan , Kwok Pong Chan , Vadim Bromberg , Xi Yang , Ananda Barua , William C. Alberts
IPC: B29C64/165 , B29C64/209 , B29C64/336 , B33Y10/00
Abstract: Various embodiments provide a method of additively manufacturing a part including depositing a layer of a powder on a working surface, depositing a binder solution on the layer of the powder at first locations, and depositing a sintering aid solution on the layer of the powder at second locations. The sintering aid solution comprises a sintering aid in a solvent. In various embodiments, the sintering aid enables an increased brown strength as compared to parts containing unbound powder. The method enables binders that provide high green strength to be used at the edges of the part, while also balancing a shortened debind time with an increased brown strength. Embodiments in which binder solution is deposited according to a predetermined pattern at second locations are also described.
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公开(公告)号:US11308249B2
公开(公告)日:2022-04-19
申请号:US16457147
申请日:2019-06-28
Applicant: General Electric Company
Inventor: Sathyanarayanan Raghavan , Ananda Barua , Evan Dozier , Joseph Block , Brendon Leary , Prabhjot Singh , Arvind Rangarajan , Changjie Sun , Dean Robinson
IPC: G06F30/20 , B29C64/393 , B29C64/40 , B33Y40/00 , B33Y50/02 , G06F119/08 , G06F119/18
Abstract: A method, medium, and system to receive a specification defining a model of a part to be produced by an additive manufacturing (AM) process; execute an AM simulation on the model of the part to determine a prediction of thermal distortions to the part; execute a topology optimization (TO) to create TO supports that counteract the predicted thermal distortions; generate at least one rule-based support based on a geometry of the part to interface with the part at one or more regions other than the TO supports; combining the TO supports and the at least one rule-based support to generate a set of hybrid supports; save a record of the set of hybrid supports; and transmit the record of the set of hybrid supports to an AM controller to control an AM system to generate a support structure for an AM production of the part.
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公开(公告)号:US11182520B2
公开(公告)日:2021-11-23
申请号:US16456333
申请日:2019-06-28
Applicant: General Electric Company
Inventor: Sathyanarayanan Raghavan , Ananda Barua , Prabhjot Singh , Arvind Rangarajan , Changjie Sun , Dean Robinson
IPC: G06F30/20 , B29C64/393 , B29C64/40 , B33Y40/00 , B33Y50/02 , G06F119/08 , G06F119/18
Abstract: A method, medium, and system to execute an additive manufacturing (AM) simulation on a model of a part; determine, based on the AM simulation, a prediction of a temperature and displacement distribution in the part at a particular time in the AM process; apply the predicted temperature and displacement distributions in the part as a boundary conditions on a support design space to determine a temperature distribution throughout the support design space; and execute a thermal-structural topology optimization based on the determined temperature and displacement distributions throughout the support design space to determine a distribution of material in the design space for a thermal support structure to interface with the part that optimally reduces a thermal gradient in the part with a minimum of material and results in the generation of an optimized AM support structure.
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公开(公告)号:US10661552B2
公开(公告)日:2020-05-26
申请号:US15663220
申请日:2017-07-28
Applicant: General Electric Company
Inventor: Ananda Barua , Arun Karthi Subramaniyan , Daniel Jason Erno , Darren Lee Hallman
IPC: B33Y50/02 , B33Y10/00 , B29C64/153 , B33Y30/00 , B22F3/105 , B33Y50/00 , G05B19/4099 , G05B19/04 , B29C64/20 , B29C64/386
Abstract: A controller for use in an additive manufacturing system including a consolidation device configured to consolidate material is provided. The controller is configured to receive a build file for a component including a plurality of build layers, wherein each build layer includes a component outer perimeter, at least one build layer generating function, at least one generating function variable, and at least one generating function constant. The controller is configured to generate at least one control signal to control a power output throughout at least one scan path of the consolidation device across the material for each build layer of the plurality of build layers, the at least one scan path generated based at least partially on the component outer perimeter, the at least one generating function, the at least one generating function variable, and the at least one generating function constant for each build layer.
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公开(公告)号:US10415579B2
公开(公告)日:2019-09-17
申请号:US15278860
申请日:2016-09-28
Applicant: General Electric Company
Inventor: Neelesh Nandkumar Sarawate , Larry Steven Rosenzweig , Sathyanarayanan Raghavan , Changjie Sun , Ananda Barua , Jinjie Shi
Abstract: Coating systems for components of a gas turbine engine, such as a compressor blade tip, are provided. The coating system can include a ceramic material disposed along the compressor blade tip and may be used with a bare compressor casing. The ceramic coating is harder than the bare compressor casing and can reduce the rub ratio thereby increasing the lifetime of the compressor blades. Methods are also provided for applying the coating system onto a compressor blade.
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