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公开(公告)号：US10577940B2
公开(公告)日：2020-03-03
申请号：US15420457
申请日：2017-01-31
Applicant: General Electric Company
Inventor： Robert Frank Hoskin , Robert Alan Brittingham , Brian Denver Potter , Daniel Jason Erno , John McConnell Delvaux
Abstract: A rotor blade for a turbomachine includes an airfoil having a leading edge, a trailing edge, a root, and a tip. The airfoil defines a chord extending from the leading edge to the trailing edge and a span extending from the root to the tip. A first particle-filled damper is positioned within the airfoil between fifty percent of the chord and one hundred percent of the chord.
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公开(公告)号：US10526921B2
公开(公告)日：2020-01-07
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：USD871468S1
公开(公告)日：2019-12-31
申请号：US29598691
申请日：2017-03-28
Applicant: General Electric Company
Designer： John McConnell Delvaux , Matthew Troy Hafner , Glenn Curtis Taxacher
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公开(公告)号：US10519790B2
公开(公告)日：2019-12-31
申请号：US15623696
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Matthew Troy Hafner , John McConnell Delvaux , Glenn Curtis Taxacher
Abstract: A turbine component includes an outer shroud arranged within a turbine and further including opposed extending portions. The component further provides an inner shroud shielding the outer shroud from a gas path within the turbine during operation of the turbine and including opposed arcuate portions extending around and in direct contact with a corresponding extending portion of the outer shroud for supporting the inner shroud from the outer shroud. The component further provides a load path forming region at least partially extending between facing surfaces of each arcuate portion and corresponding extending portion. During operation of the turbine, load path forming regions extend into direct contact between at least a portion of the facing surfaces of each arcuate portion and corresponding extending portion, resulting in formation of a loading arrangement having generally evenly distributed radial load forces at the load path forming regions.
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公开(公告)号：US10215036B2
公开(公告)日：2019-02-26
申请号：US15086539
申请日：2016-03-31
Applicant: General Electric Company
Abstract: An assembly and method for affixing a turbomachine rotor blade to a rotor wheel are disclosed. In an embodiment, an adaptor member is provided disposed between the blade and the rotor wheel, the adaptor member including an adaptor attachment slot that is complementary to the blade attachment member, and an adaptor attachment member that is complementary to the rotor wheel attachment slot. A coverplate is provided, having a coverplate attachment member that is complementary to the rotor wheel attachment slot, and a hook for engaging the adaptor member. When assembled, the coverplate member matingly engages with the adaptor member, and retains the blade in the adaptor member, and the assembly in the rotor wheel.
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Patent Agency Ranking
公开(公告)号：US10087519B1
公开(公告)日：2018-10-02
申请号：US15629532
申请日：2017-06-21
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jason Robert Parolini , John McConnell Delvaux , Srikanth Chandrudu Kottilingam , James Joseph Murray , Canan Uslu Hardwicke , Matthew Troy Hafner
Abstract: A method of making a preform and preform formed by the method. The method includes providing a first pre-preg ply including at least a first fiber and a first resin. The method also includes providing a second pre-preg ply including at least a second fiber and a second resin over at least a portion of the first pre-preg ply. Heat or electromagnetic radiation is used to at least partially cure the first and second resins to form a cured preform. Heat is applied to pyrolyze at least a portion of the resin of the cured preform to form a pyrolyzed preform. A mechanical stimulus including at least one of controlled drying, local explosions, or ultrasonic energy is applied to the pyrolyzed preform. The mechanically treated pyrolyzed preform is subsequently densified by melt infiltration to form a densified preform.
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公开(公告)号：US20180272568A1
公开(公告)日：2018-09-27
申请号：US15465726
申请日：2017-03-22
Applicant: General Electric Company
Inventor： Jason Robert Parolini , Matthew Troy Hafner , James Joseph Murray , Srikanth Chandrudu Kottilingam , Canan Uslu Hardwicke , John McConnell Delvaux
IPC: B29C35/02 , B29C33/38 , C04B35/80 , C04B35/626 , C04B35/628 , C04B35/657
CPC classification number: B29C35/02 , B29C33/38 , B29L2031/7504 , B32B18/00 , C04B35/62645 , C04B35/62844 , C04B35/62876 , C04B35/657 , C04B35/803 , C04B35/806 , C04B2235/3217 , C04B2235/3826 , C04B2235/3873 , C04B2235/5224 , C04B2235/524 , C04B2235/5244 , C04B2235/5248 , C04B2235/6026 , C04B2235/6028 , C04B2235/616 , C04B2235/945 , C04B2237/38 , C04B2237/62 , C04B2237/64 , F01D5/282 , F01D5/284 , F05D2260/204 , F05D2300/6033
Abstract: The present disclosure is directed to a method for forming a passage in a composite component. The method includes forming a cavity in a fiber preform. The cavity forms a portion of the passage. The method also includes inserting a core into the cavity and placing one or more fiber plies onto the fiber preform to form a fiber preform assembly. The method further includes thermally processing the fiber preform assembly and densifying the fiber preform assembly to form the composite component. The method also includes removing the core from the composite component.
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公开(公告)号：US09718735B2
公开(公告)日：2017-08-01
申请号：US14612806
申请日：2015-02-03
Applicant: GENERAL ELECTRIC COMPANY
Inventor： John McConnell Delvaux , Andres Jose Garcia-Crespo , Victor John Morgan , Jacob John Kittleson
IPC: B32B3/24 , F01D25/12 , F01D25/24 , C04B35/00 , C04B35/44 , C04B35/52 , C04B35/565 , B29C70/54 , F01D5/18 , B29C71/04 , F01D25/14 , F01D5/28 , F01D11/08 , F02C6/06 , F02C6/08 , B29L31/00 , B32B3/26 , F01D11/24
CPC classification number: C04B35/565 , B29C70/545 , B29C71/04 , B29L2031/7504 , B32B3/266 , C04B35/44 , C04B35/52 , F01D5/186 , F01D5/282 , F01D5/284 , F01D5/288 , F01D11/08 , F01D11/24 , F01D25/12 , F01D25/14 , F02C6/06 , F02C6/08 , F05D2230/90 , F05D2240/11 , F05D2260/202 , F05D2260/232 , F05D2270/09 , F05D2270/11 , F05D2270/112 , F05D2300/2261 , F05D2300/6033
Abstract: Components are disclosed which include a CMC substrate having a first surface and a second surface. The first surface is in fluid communication with a compressed, dry fluid, and the second surface is in fluid communication with a wet fluid stream and includes a hermetic coating. The components further include at least one opening extending from the first surface through a portion of the CMC substrate, wherein, upon removal of a fragment of one or both of the hermetic coating and the CMC substrate, the at least one opening selectively permits a flow of the compressed, dry fluid to the second surface. In one embodiment, the component is a gas turbine component, the wet fluid stream is a hot combustion stream, the hermetic coating is an environmental barrier coating, and the flow reduces or eliminates volatilization of the CMC substrate. Methods for forming the components are also disclosed.
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59.发明授权Apparatus and method to reduce wear and friction between CMC-to-metal attachment and interface 有权降低CMC与金属附件和界面之间磨损和摩擦的装置和方法公开(公告)号：US09500083B2
公开(公告)日：2016-11-22
申请号：US13685230
申请日：2012-11-26
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Ronald Ralph Cairo , Jason Robert Parolini , John McConnell Delvaux
IPC: F01D5/14 , C04B35/117 , C04B35/185 , C04B35/565 , C04B35/80 , C04B35/83 , C04B37/02 , F01D5/30 , F23R3/00 , F23R3/60
CPC classification number: F01D5/14 , C04B35/117 , C04B35/185 , C04B35/565 , C04B35/803 , C04B35/806 , C04B35/83 , C04B37/026 , C04B2235/5224 , C04B2235/5228 , C04B2235/5244 , C04B2235/5248 , C04B2235/963 , C04B2237/123 , C04B2237/365 , C04B2237/38 , C04B2237/405 , C04B2237/592 , C04B2237/64 , C04B2237/66 , C04B2237/708 , C04B2237/76 , C04B2237/84 , F01D5/3084 , F01D5/3092 , F05D2300/6033 , F23R3/007 , F23R3/60 , F23R2900/00017 , Y10T29/49336
Abstract: An apparatus to reduce wear and friction between CMC-to-metal attachment and interface, including a metal layer configured for insertion between a surface interface between a CMC component and a metal component. The surface interface of the metal layer is compliant relative to asperities of the surface interface of the CMC component. A coefficient of friction between the surface interface of the CMC component and the metal component is about 1.0 or less at an operating temperature between about 300° C. to about 325° C. and a limiting temperature of the metal component.
Abstract translation: 一种降低CMC与金属附件和界面之间的磨损和摩擦的装置，包括配置成插入在CMC组件和金属部件之间的表面界面之间的金属层。 金属层的表面界面相对于CMC部件的表面界面的粗糙度是顺从的。 在约300℃至约325℃的操作温度和金属组分的极限温度之间，CMC组分的表面界面与金属组分之间的摩擦系数约为1.0或更小。
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60.发明授权Apparatus having engineered surface feature and method to reduce wear and friction between CMC-to-metal attachment and interface 有权具有设计的表面特征和方法的装置，以减少CMC与金属附件和界面之间的磨损和摩擦公开(公告)号：US09453421B2
公开(公告)日：2016-09-27
申请号：US15048537
申请日：2016-02-19
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Ronald Ralph Cairo , Jason Robert Parolini , John McConnell Delvaux
CPC classification number: F01D5/282 , F01D5/02 , F01D5/147 , F01D5/284 , F01D5/3007 , F01D5/3084 , F01D5/3092 , F05D2220/32 , F05D2240/24 , F05D2250/711 , F05D2250/712 , F05D2300/6033 , Y02T50/672
Abstract: An apparatus having reduced wear and friction between CMC-to-metal attachment and interface of the apparatus, including a CMC component having a surface. The CMC component surface is configured for sliding contact with a surface of a metal component, the sliding contact resulting in formation of debris along the contacting surfaces. The surface of the CMC component has an engineered surface feature formed therein to substantially prevent an accumulation of debris along the contacting surfaces.
Abstract translation: 一种具有降低CMC与金属附件和设备界面之间的磨损和摩擦的装置，包括具有表面的CMC组件。 CMC部件表面构造成与金属部件的表面滑动接触，滑动接触导致沿着接触表面形成碎屑。 CMC组件的表面具有形成在其中的工程化表面特征，以基本上防止沿着接触表面积聚碎屑。
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