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公开(公告)号：US20180194688A1
公开(公告)日：2018-07-12
申请号：US15401575
申请日：2017-01-09
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Matthew Troy HAFNER , John McConnell DELVAUX , Glenn Curtis TAXACHER , Zachary John SNIDER
CPC classification number: C04B35/806 , B32B18/00 , C04B35/573 , C04B37/005 , C04B2235/3826 , C04B2235/5224 , C04B2235/5228 , C04B2235/5236 , C04B2235/5244 , C04B2235/5248 , C04B2237/083 , C04B2237/365 , C04B2237/38 , C04B2237/61 , C04B2237/704 , F01D5/282 , F01D9/02 , F01D25/005 , F05D2300/6033
Abstract: A CMC ply assembly is disclosed including at least one matrix ply interspersed amongst a plurality of CMC plies. Each of the plurality of CMC plies includes a first matrix and a plurality of ceramic fibers. The at least one matrix ply includes a second matrix and is essentially free of ceramic fibers. The plurality of CMC plies and the at least one matrix ply are arranged in an undensified ply stack having an article conformation. A CMC article is disclosed including a plurality of densified CMC plies and at least one densified matrix ply interspersed amongst the plurality of densified CMC plies. A method for forming the CMC article is disclosed including forming, carburizing, infusing a melt infiltration agent into, and densifying the CMC ply assembly. The melt infiltration agent infuses more completely through the at least one matrix ply than through the plurality of CMC plies.
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公开(公告)号：US20170276000A1
公开(公告)日：2017-09-28
申请号：US15079346
申请日：2016-03-24
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Zachary John SNIDER , John McConnell DELVAUX , Glenn Curtis TAXACHER
CPC classification number: F01D9/02 , F01D11/005 , F01D11/10 , F01D25/246 , F05D2230/60 , F05D2240/11 , F05D2240/128 , F05D2240/30 , F05D2240/55 , F05D2300/6033 , F05D2300/614
Abstract: An apparatus is disclosed including a first article, a second article, and a third article disposed adjacent to one another, with the first article and the second article disposed between the third article and a gas path. The first article includes at least one first ceramic matrix composite ply defining a first cooperating feature. The second article includes at least one second ceramic matrix composite ply defining a second cooperating feature. The first cooperating feature and the second cooperating feature define a restricted flow path from the gas path to the third article, which includes a reduced volumetric flow rate of a gas from the gas path to the third article relative to a non-restricted flow path of a non-cooperating interface. A method for forming the apparatus includes forming and aligning the first cooperating feature and the second cooperating feature.
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公开(公告)号：US20180363509A1
公开(公告)日：2018-12-20
申请号：US15624070
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Glenn Curtis TAXACHER , John McConnell DELVAUX , Matthew Troy HAFNER
CPC classification number: F01D25/28 , F01D9/04 , F01D25/005 , F05D2240/11 , F05D2240/35 , F05D2250/184 , F05D2250/61 , F05D2260/52 , F05D2300/10 , F05D2300/6012 , F05D2300/6033 , F05D2300/611 , F23R3/007 , F23R3/60 , F23R2900/00005 , F23R2900/00017
Abstract: A turbine component assembly is disclosed, including a first component, a second component, and a circumferentially oriented flat spring. The first component is arranged to be disposed adjacent to a hot gas path, and includes a ceramic matrix composite composition. The second component is adjacent to the first component and arranged to be disposed distal from the hot gas path across the first component. The circumferentially oriented flat spring is disposed on and directly contacting the second component and directly contacting and supporting the first component as a compliant contact interface between the first component and the second component. The circumferentially oriented flat spring provides a radial spring compliance between the first component and the second component.
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公开(公告)号：US20180363504A1
公开(公告)日：2018-12-20
申请号：US15623938
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Glenn Curtis TAXACHER , John McConnell DELVAUX , Matthew Troy HAFNER
Abstract: An anti-rotation shroud dampening pin is disclosed including a shaft, an anti-rotation dampening tip at a first end of the shaft, and a cap at a second end of the shaft. The anti-rotation dampening tip includes a pin non-circular cross-section. A turbine shroud assembly is disclosed, including an inner shroud, an outer shroud, the anti-rotation shroud dampening pin, and a biasing apparatus. The inner shroud includes an anti-rotation depression having a depression non-circular cross-section. The outer shroud includes a channel extending from an aperture adjacent to the inner shroud. The anti-rotation shroud dampening pin is disposed within the channel and in contact with the inner shroud, and extends through the aperture into the anti-rotation depression. The biasing apparatus contacts the cap and provides a biasing force to the inner shroud through the anti-rotation dampening tip. The pin non-circular cross-section mates non-rotatably into the depression non-circular cross-section.
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公开(公告)号：US20180363503A1
公开(公告)日：2018-12-20
申请号：US15623899
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Glenn Curtis TAXACHER , Herbert Chidsey ROBERTS, III , Randall GILL
Abstract: A shroud dampening pin is disclosed including a shaft, a dampening portion at a first end of the shaft, and a cap at a second end of the shaft. The dampening portion includes a bevel having a bevel angle and a contact surface. A turbine shroud assembly is disclosed, including an inner shroud, an outer shroud, the shroud dampening pin, and a biasing apparatus. The outer shroud includes a channel extending from an aperture adjacent to the inner shroud at a channel angle from the aperture. The shroud dampening pin is disposed within the channel. The dampening portion extends through the aperture with the contact surface contacting the inner shroud. The biasing apparatus contacts the cap and provides a biasing force to the inner shroud through the contact surface. The bevel angle is about the same as the channel angle, and the contact surface is about parallel to the aperture.
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Patent Agency Ranking
公开(公告)号：US20180363510A1
公开(公告)日：2018-12-20
申请号：US15624142
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Glenn Curtis TAXACHER , John McConnell DELVAUX , Matthew Troy HAFNER
CPC classification number: F01D25/28 , F01D9/04 , F01D9/042 , F01D11/08 , F05D2240/35 , F05D2260/38 , F05D2260/52 , F05D2300/10 , F05D2300/6033 , F05D2300/611 , F23R3/007 , F23R3/60 , F23R2900/00005 , F23R2900/00017
Abstract: A turbine component assembly is disclosed, including a first component, a second component, and a cantilever spring. The first component is arranged to be disposed adjacent to a hot gas path, and includes a ceramic matrix composite composition. The second component is adjacent to the first component and arranged to be disposed distal from the hot gas path across the first component. The cantilever spring is attached directly to the second component as a compliant contact interface between the first component and the second component. The cantilever spring provides a radial spring compliance between the first component and the second component. During operation, the cantilever spring directly contacts and supports the first component.
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公开(公告)号：US20180363498A1
公开(公告)日：2018-12-20
申请号：US15623990
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Glenn Curtis TAXACHER , John McConnell DELVAUX , Matthew Troy HAFNER
CPC classification number: F01D25/04 , F01D9/04 , F01D11/08 , F01D25/246 , F05D2220/32 , F05D2240/11 , F05D2260/30 , F05D2260/42 , F05D2300/175 , F05D2300/6033
Abstract: A turbine shroud assembly is disclosed including an inner shroud, an outer shroud, a shroud dampening pin, and a biasing apparatus. The inner shroud is adjacent to a hot gas path. The outer shroud is adjacent to the inner shroud and distal from the hot gas path, and includes a channel extending from an aperture adjacent to the inner shroud. The shroud dampening pin is within the channel and contacts the inner shroud, and includes a shaft, a contact surface, and a cap. The shaft is within the channel. The contact surface extends through the aperture in contact with the inner shroud. The cap is distal across the shaft from the contact surface. The biasing apparatus contacts the cap, is driven by a pressurized fluid, and provides a biasing force away from the outer shroud along the shroud dampening pin to the inner shroud through the contact surface.
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8.发明申请公开(公告)号：US20180229451A1
公开(公告)日：2018-08-16
申请号：US15433548
申请日：2017-02-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jason Robert PAROLINI , John McConnell DELVAUX , Canan Uslu HARDWICKE , Glenn Curtis TAXACHER , James Joseph MURRAY
CPC classification number: B29C70/44 , B29C70/025 , B29D99/0028 , B32B18/00 , C04B35/806 , C04B37/001 , C04B2235/94 , C04B2235/95 , C04B2237/38 , F01D25/005 , F05D2260/202 , F05D2300/6033
Abstract: A method of forming a pre-form ceramic matrix composite mold for a ceramic matrix composite (CMC) component including providing pieces of CMC remnant scrap material and randomly arranging the pieces of CMC remnant scrap material relative to one another. The method further includes debulking the pieces of CMC remnant scrap material into a rigidized shape, the rigidized shape having gaps between adjacent pieces of CMC remnant scrap material of about 10 microns and about 10 mm and a gap spacing between about 50 microns and about 50 mm, and forming the rigidized shape into a mold.
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9.发明申请公开(公告)号：US20150345388A1
公开(公告)日：2015-12-03
申请号：US14292969
申请日：2014-06-02
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Paul Stephen DIMASCIO , Victor John MORGAN , Jason Robert PAROLINI , Glenn Curtis TAXACHER , Frederic Woodrow ROBERTS, JR. , Jacob John KITTLESON , John McConnell DELVAUX
IPC: F02C7/00 , B23K1/00 , B23P6/00 , C04B41/91 , B24B33/00 , C04B41/00 , C04B41/53 , C04B41/50 , C04B41/45 , C23C16/24 , C04B41/85
CPC classification number: F02C7/00 , B23K1/0018 , B23P6/002 , B23P6/007 , B24B33/00 , C04B41/009 , C04B41/4531 , C04B41/5025 , C04B41/5096 , C04B41/5144 , C04B41/53 , C04B41/85 , C04B41/87 , C04B41/88 , C04B41/91 , C23C16/24 , F05D2230/30 , F05D2230/90 , F05D2300/6033 , Y10T156/10 , Y10T428/24355 , C04B35/00 , C04B35/80 , C04B41/4529 , C04B41/4539 , C04B41/5133 , C04B41/0072
Abstract: A process of producing a ceramic matrix composite gas turbine component and a ceramic matrix composite gas turbine component are provided. The process includes modifying a surface of the ceramic matrix composite gas turbine component to produce a modified surface with a surface roughness of less than 6 micrometers. The modifying is selected from the group of techniques consisting of applying unreinforced matrix plies to the surface, vapor depositing silicon on the surface, honing the surface, applying braze paste to the surface, and combinations thereof. The component includes a modified surface including a surface roughness of less than 6 micrometers. The modified surface being selected from the group consisting of unreinforced matrix plies applied to a surface of the ceramic matrix composite gas turbine component, silicon vapor deposited on the surface, a honed surface, a braze paste applied to the surface, and combinations thereof.
Abstract translation: 提供了陶瓷基复合燃气轮机部件和陶瓷基复合燃气轮机部件的制造方法。 该方法包括改变陶瓷基复合燃气轮机部件的表面以产生表面粗糙度小于6微米的改性表面。 修饰选自由将未增强的基质层施加到表面，在表面上蒸镀硅，珩磨表面，将钎焊膏施加到表面上的技术组合，以及它们的组合。 该组件包括包括小于6微米的表面粗糙度的改性表面。 所述改性表面选自施加到陶瓷基复合燃气轮机部件的表面的未增强基体层，沉积在表面上的硅蒸汽表面，珩磨表面，施加到表面上的钎焊膏及其组合。
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公开(公告)号：US20180363508A1
公开(公告)日：2018-12-20
申请号：US15623715
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
CPC classification number: F01D25/26 , F01D25/005 , F05D2260/30 , F05D2300/175 , F05D2300/603
Abstract: A turbine component including an outer shroud arranged within a turbine and including opposed extending portions. An inner shroud shields the outer shroud from a gas flowing along a gas path within the turbine during its operation and including opposed first and second arcuate portions extending around and in direct contact with a corresponding extending portion of the outer shroud. A first pin and second pin have a respective first end and second end. The first arcuate portion having a first engagement region for engaging the first end, and second arcuate portion having a second engagement region for engaging the second end. In response to engagement of the first engagement region and the first end of the first pin, and engagement of the second engagement region and the second end of the second pin, the inner shroud is prevented from twisting relative to the outer shroud.
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