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公开(公告)号:US20190001402A1
公开(公告)日:2019-01-03
申请号:US15636282
申请日:2017-06-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Xi YANG , Michael COLE , Michael BROWN , Gregory Terrence GARAY , Tingfan PANG , Brian David PRZESLAWSKI , Douglas Gerard KONITZER
Abstract: The present disclosure relates to a method of forming a cast component and a method of forming a casting mold. The method is performed by connecting at least one wax gate component to a ceramic core-shell mold. The ceramic core-shell mold includes at least a first core portion, a first shell portion, and a second shell portion, wherein the first shell portion is adapted to interface with at least the second shell portion to form at least one first cavity between the core portion and the first and second shell portions. The core-shell mold may be inspected and assembled prior to connection of the wax gate component. At least a portion of the ceramic core-shell mold and the wax gate component is coated with a second ceramic material. The wax gate component is then removed to form a second cavity in fluid communication with the first cavity.
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公开(公告)号:US20190001522A1
公开(公告)日:2019-01-03
申请号:US15636008
申请日:2017-06-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Xi YANG , Michael COLE , Michael BROWN , Gregory Terrence GARAY , Tingfan PANG , Brian David PRZESLAWSKI , Douglas Gerard KONITZER
CPC classification number: B28B1/001 , B22C7/02 , B22C9/04 , B22C9/08 , B22C9/10 , B28B7/28 , B28B7/346 , B33Y10/00 , C04B2235/6026 , F01D5/147 , F01D5/187 , F05D2230/211 , F05D2230/30 , F05D2250/185 , F05D2300/20
Abstract: The present disclosure generally relates to integrated core-shell investment casting molds that provide a filament structure corresponding to a cooling hole pattern in the surface of the turbine blade, stator vane, or shroud. The disclosure also relates to the forming of a ceramic coating on at least a portion of the shell of the core-shell casting mold.
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公开(公告)号:US20190001405A1
公开(公告)日:2019-01-03
申请号:US15636404
申请日:2017-06-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Xi YANG , Michael COLE , Michael BROWN , Gregory Terrence GARAY , Tingfan PANG , Brian David PRZESLAWSKI , Douglas Gerard KONITZER
CPC classification number: B22C9/10 , B22C9/04 , B22D29/002 , B28B1/001 , B28B11/045 , B33Y10/00 , B33Y80/00
Abstract: The present disclosure generally relates to integrated core-shell investment casting molds that provide a filament structure corresponding to a cooling hole pattern in the surface of the turbine blade, stator vane, or shroud. The disclosure also relates to the forming of a ceramic coating on at least a portion of the shell of the core-shell casting mold.
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4.
公开(公告)号:US20190001403A1
公开(公告)日:2019-01-03
申请号:US15636366
申请日:2017-06-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Xi YANG , Michael COLE , Michael BROWN , Gregory Terrence GARAY , Tingfan PANG , Brian David PRZESLAWSKI , Douglas Gerard KONITZER
Abstract: The present disclosure relates to a method of forming a cast component and a method of forming a casting mold. The method is performed by connecting at least one wax gate component to a ceramic core-shell mold. The ceramic core-shell mold includes at least a filter, first core portion, a first shell portion, and at least one first cavity between the core portion and the first shell portion. The core-shell mold may manufactured using an additive manufacturing process and may include an integrated ceramic filter. At least a portion of the ceramic core-shell mold and the wax gate component is coated with a second ceramic material. The wax gate component is then removed to form a second cavity in fluid communication with the first cavity.
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公开(公告)号:US20200030872A1
公开(公告)日:2020-01-30
申请号:US16531842
申请日:2019-08-05
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Xi YANG , Michael COLE , Michael BROWN , Gregory Terrence GARAY , Tingfan PANG , Brian David PRZESLAWSKI , Douglas Gerard KONITZER
Abstract: The present disclosure generally relates to integrated core-shell investment casting molds that provide a filament structure corresponding to a cooling hole pattern in the surface of the turbine blade, stator vane, or shroud. The disclosure also relates to the forming of a ceramic coating on at least a portion of the shell of the core-shell casting mold.
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6.
公开(公告)号:US20190240726A1
公开(公告)日:2019-08-08
申请号:US15887601
申请日:2018-02-02
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Gregory Terrence GARAY , Meredith DUBELMAN , Xi YANG , Tingfan PANG , Michael Scott COLE , Brian David PRZESLAWSKI , Douglas Gerard KONITZER , Nicole BARBA , Kirk GALLIER , Brian KEITH
CPC classification number: B22C9/22 , B22D29/002 , B28B1/001 , B33Y10/00 , B33Y80/00 , C30B29/02 , F01D5/18 , F01D9/02 , F05D2220/32 , F05D2300/10
Abstract: The present disclosure generally relates to integrated core-shell investment casting molds that provide tongue or groove structures corresponding, respectively, to groove or tongue structures in the surface of the turbine blade or stator vane, including in locations that are otherwise inaccessible. The groove and tongue structures also provide a pathway to restrict cooling flow between turbine blades to the flowpath.
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7.
公开(公告)号:US20190001404A1
公开(公告)日:2019-01-03
申请号:US15636389
申请日:2017-06-28
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Xi YANG , Michael COLE , Michael BROWN , Gregory Terrence GARAY , Tingfan PANG , Brian David PRZESLAWSKI , Douglas Gerard KONITZER
Abstract: The present disclosure relates to a method of forming a cast component and a method of forming a casting mold. The method is performed by connecting at least one wax gate component to a ceramic core-shell mold. The ceramic core-shell mold includes at least a filter, first core portion, a first shell portion, and at least one first cavity between the core portion and the first shell portion. The core-shell mold may manufactured using an additive manufacturing process and may include an integrated ceramic filter. At least a portion of the ceramic core-shell mold and the wax gate component is coated with a second ceramic material. The wax gate component is then removed to form a second cavity in fluid communication with the first cavity.
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