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公开(公告)号：US09227278B2
公开(公告)日：2016-01-05
申请号：US12080701
申请日：2008-04-04
Applicant: Nicole Sullivan , David A. Rutz , Monika D. Kinstler , James J. Moor
Inventor： Nicole Sullivan , David A. Rutz , Monika D. Kinstler , James J. Moor
Abstract: A method of hole defect repair includes removing one or more defects at or near a desired hole in a part by removing a portion of the part proximate the desired hole in a series of chain link patterns, and welding a filler material to the part after removing the chain link pattern portion of the part.
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公开(公告)号：US08910378B2
公开(公告)日：2014-12-16
申请号：US13461283
申请日：2012-05-01
Applicant: Monika D. Kinstler
Inventor： Monika D. Kinstler
IPC: B21K25/00
CPC classification number: F23R3/002 , B23P6/002 , B23P2700/13 , F23R2900/00018 , F23R2900/00019 , Y10T29/49318 , Y10T29/4932 , Y10T29/49348
Abstract: A method for working or repairing a combustor wall panel that may be damaged is disclosed. The method comprises providing a supplemental body to a combustor float wall panel, and attaching at least one cooling pin to the supplemental body.
Abstract translation: 公开了一种用于工作或修理可能损坏的燃烧器壁板的方法。 该方法包括向燃烧器浮体壁板提供补充体，并将至少一个冷却销附接到补充体。
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公开(公告)号：US20110167634A1
公开(公告)日：2011-07-14
申请号：US12882380
申请日：2010-09-15
Applicant: Timothy A. Milleville , Monika D. Kinstler , David A. Litton , Daniel F. Paulonis
Inventor： Timothy A. Milleville , Monika D. Kinstler , David A. Litton , Daniel F. Paulonis
IPC: B23P6/00
CPC classification number: B23P6/007 , C23C10/02 , C23C10/04 , C23C10/60 , C23C28/021 , C23C28/023 , C23C28/028 , C23C30/00 , F01D5/005 , F01D5/288 , F05D2230/30 , F05D2230/90 , Y10T29/49318 , Y10T428/12493 , Y10T428/12944
Abstract: A method of repairing a component of a gas turbine engine that includes a metallic substrate, an existing aluminide coating, and a diffusion layer formed in the metallic substrate adjacent to the coating. The method includes removing at least a portion of the existing aluminide coating, removing material forming the diffusion layer, applying a new metallic layer to the metallic substrate, and applying a new aluminide coating over the new metallic layer to form a new diffusion layer in the new metallic layer. The new metallic layer is a substantially homogeneous material that is substantially similar in chemical composition to that of the metallic substrate, and the new metallic layer forms a structural layer having a thickness selected to provide a specified contour to the component.
Abstract translation: 一种修复燃气涡轮发动机的部件的方法，其包括金属基板，现有的铝化物涂层和形成在与涂层相邻的金属基板中的扩散层。 该方法包括去除现有的铝化物涂层的至少一部分，去除形成扩散层的材料，向金属基底施加新的金属层，以及在新的金属层上施加新的铝化物涂层，以形成新的扩散层 新金属层。 新的金属层是基本上均匀的材料，其化学组成基本上与金属基底相似，并且新的金属层形成具有被选择为该部件提供特定轮廓的厚度的结构层。
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公开(公告)号：US20100285330A1
公开(公告)日：2010-11-11
申请号：US11939854
申请日：2007-11-14
Applicant: Igor V. Belousov , Igor S. Malashenko , Gregory A. Serhiyenko , Anatoli N. Shelkovoi , Evgeniy A. Shelkovoy , Robert L. Memmen , David A. Rutz , Monika D. Kinstler
Inventor： Igor V. Belousov , Igor S. Malashenko , Gregory A. Serhiyenko , Anatoli N. Shelkovoi , Evgeniy A. Shelkovoy , Robert L. Memmen , David A. Rutz , Monika D. Kinstler
CPC classification number: C23C14/30 , Y10T428/12639 , Y10T428/12778 , Y10T428/12806
Abstract: A method for depositing a first material on a substrate includes providing the substrate in a deposition chamber. A molten body is formed between the substrate and a source of the first material by melting one or more second materials. A flow of the first material is passed through the molten body and from the molten body to the substrate as a vapor flow. An essentially non-expending portion of the molten body comprises an alloy having a melting temperature below a melting temperature of the first material.
Abstract translation: 用于在衬底上沉积第一材料的方法包括在沉积室中提供衬底。 通过熔化一种或多种第二种材料，在基材和第一材料源之间形成熔融体。 第一材料的流动作为蒸汽流通过熔融体并从熔融体流到基底。 熔融体的基本不膨胀部分包括熔融温度低于第一材料的熔融温度的合金。
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公开(公告)号：US10669867B2
公开(公告)日：2020-06-02
申请号：US15103077
申请日：2014-12-03
Applicant: Lei Chen , Zhiwei Yang , William J. Brindley , Monika D. Kinstler , Bruce R. Saxton
Inventor： Lei Chen , Zhiwei Yang , William J. Brindley , Monika D. Kinstler , Bruce R. Saxton
IPC: F01D5/28 , C25D5/50 , C25D3/66 , C25D3/56 , C22C19/05 , C25D3/12 , C25D5/40 , C25D7/00 , F01D9/02 , F01D25/00 , C25D5/18
Abstract: A nickel-chromium (Ni—Cr) alloy and a method for electrodepositing the Ni—Cr alloy on a turbine engine component for dimensionally restoring the engine component are described. The engine component is restored by re-building wall thickness with the Ni—Cr alloy including from 2 to 50 wt % chromium balanced with nickel. The turbine component coated with the Ni—Cr alloy is heat-treated at a high temperature to homogenize composition of the alloy to mimic the base alloy and to restore materials lost during repair of the turbine component.
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Patent Agency Ranking
公开(公告)号：US08286582B2
公开(公告)日：2012-10-16
申请号：US11939854
申请日：2007-11-14
Applicant: Igor V. Belousov , Igor S. Malashenko , Gregory A. Serhiyenko , Anatoli N. Shelkovoy , Evgeniy A. Shelkovoy, legal representative , Robert L. Memmen , David A. Rutz , Monika D. Kinstler
Inventor： Igor V. Belousov , Igor S. Malashenko , Gregory A. Serhiyenko , Anatoli N. Shelkovoy , Robert L. Memmen , David A. Rutz , Monika D. Kinstler
IPC: C23C16/00
CPC classification number: C23C14/30 , Y10T428/12639 , Y10T428/12778 , Y10T428/12806
Abstract: A method for depositing a first material on a substrate includes providing the substrate in a deposition chamber. A molten body is formed between the substrate and a source of the first material by melting one or more second materials. A flow of the first material is passed through the molten body and from the molten body to the substrate as a vapor flow. An essentially non-expending portion of the molten body comprises an alloy having a melting temperature below a melting temperature of the first material.
Abstract translation: 用于在衬底上沉积第一材料的方法包括在沉积室中提供衬底。 通过熔化一种或多种第二种材料，在基材和第一材料源之间形成熔融体。 第一材料的流动作为蒸汽流通过熔融体并从熔融体流到基底。 熔融体的基本不膨胀部分包括熔融温度低于第一材料的熔融温度的合金。
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公开(公告)号：US20090320287A1
公开(公告)日：2009-12-31
申请号：US11303579
申请日：2005-12-15
Applicant: John F. Mullooly , William M. Rose , David R. Malley , Monika D. Kinstler
Inventor： John F. Mullooly , William M. Rose , David R. Malley , Monika D. Kinstler
IPC: B23P6/00
CPC classification number: B23P6/007 , C23C4/01 , C23C4/18 , C23C10/04 , F01D5/005 , F05D2230/90 , F05D2300/611 , Y10T29/49318 , Y10T29/49336 , Y10T29/49732 , Y10T29/49734 , Y10T29/49746 , Y10T29/4975
Abstract: A method for repairing a turbine engine component is provided. The method broadly comprises the steps of providing a turbine engine component having an airfoil portion, applying a coating to the airfoil portion, and restoring a tip portion, a chord, and surfaces of the airfoil portion to original dimensions in a single operation. A system for repairing the turbine engine component is also described.
Abstract translation: 提供了一种用于修理涡轮发动机部件的方法。 该方法广泛地包括以下步骤：提供具有翼型部分的涡轮发动机部件，在翼型部分上施加涂层，以及在一次操作中将翼尖部分，弦杆和翼型部分的表面恢复到原始尺寸。 还描述了用于修理涡轮发动机部件的系统。
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公开(公告)号：US20080292903A1
公开(公告)日：2008-11-27
申请号：US11805960
申请日：2007-05-25
Applicant: Timothy A. Milleville , Monika D. Kinstler , David A. Litton , Daniel F. Paulonis
Inventor： Timothy A. Milleville , Monika D. Kinstler , David A. Litton , Daniel F. Paulonis
CPC classification number: B23P6/007 , C23C10/02 , C23C10/04 , C23C10/60 , C23C28/021 , C23C28/023 , C23C28/028 , C23C30/00 , F01D5/005 , F01D5/288 , F05D2230/30 , F05D2230/90 , Y10T29/49318 , Y10T428/12493 , Y10T428/12944
Abstract: A method of repairing a component of a gas turbine engine that includes a metallic substrate, an existing coating, and a diffusion layer formed in the metallic substrate adjacent to the coating. The method includes removing at least a portion of the existing aluminide coating, removing material forming the diffusion layer, applying a new metallic layer to the metallic substrate, and applying a new aluminide coating over the new metallic layer to form a new diffusion layer in the new metallic layer. The new metallic layer is a substantially homogeneous material that is substantially similar in chemical composition to that of the metallic substrate, and the new metallic layer forms a structural layer having a thickness selected to provide a specified contour to the component.
Abstract translation: 一种修复燃气涡轮发动机的部件的方法，其包括金属基板，现有涂层和形成在与涂层相邻的金属基板中的扩散层。 该方法包括去除现有的铝化物涂层的至少一部分，去除形成扩散层的材料，向金属基底施加新的金属层，以及在新的金属层上施加新的铝化物涂层，以形成新的扩散层 新金属层。 新的金属层是基本上均匀的材料，其化学组成基本上与金属基底相似，并且新的金属层形成具有被选择为该部件提供特定轮廓的厚度的结构层。
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公开(公告)号：US07377417B2
公开(公告)日：2008-05-27
申请号：US11292505
申请日：2005-12-02
Applicant: Monika D. Kinstler
Inventor： Monika D. Kinstler
CPC classification number: B23P6/007 , B23K35/0244 , B23K35/025 , B23K35/304 , B23K2101/001 , B23P6/045 , Y10T29/49318
Abstract: In accordance with the present invention, a process for repairing metal workpieces, such as turbine engine components, is provided. The process comprises the steps of forming a braze paste containing a first nickel base alloy material containing boron and chromium and a second nickel base alloy material containing chromium and cobalt, applying the brazing paste to an area of the metal workpiece containing at least one crack, and subjecting the workpiece and the brazing paste to a brazing cycle by heating the brazing paste and the workpiece, preferably to a temperature in the range of from 2000 to 2200 degrees Fahrenheit. During the brazing cycle, the brazing paste flows into and fills the at least one crack and thus repairs the metal workpiece.
Abstract translation: 根据本发明，提供了一种用于修理诸如涡轮发动机部件的金属工件的工艺。 该方法包括以下步骤：形成含有含有硼和铬的第一镍基合金材料和含有铬和钴的第二镍基合金材料的钎焊膏，将钎焊膏施加到包含至少一个裂纹的金属工件的区域中， 并且通过将钎焊膏和工件加热而使工件和钎焊膏经受钎焊循环，优选为2000-2200华氏度的温度。 在钎焊循环期间，钎焊膏流入并填充至少一个裂纹，从而修复金属工件。
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公开(公告)号：US08122600B2
公开(公告)日：2012-02-28
申请号：US10377954
申请日：2003-03-03
Applicant: Monika D. Kinstler , David A. Rutz , Robert L. Memmen
Inventor： Monika D. Kinstler , David A. Rutz , Robert L. Memmen
IPC: B23P6/00
CPC classification number: B23P6/007 , C23C14/028 , C23C14/04 , F01D5/005 , F01D5/30 , F05D2230/30 , F05D2230/80 , Y10T29/49318 , Y10T29/49336 , Y10T29/49723 , Y10T29/49728 , Y10T29/49737 , Y10T29/49982 , Y10T29/49989
Abstract: A method for restoring blade dovetails to their original shape comprising the steps of removing damaged material from a blade dovetail at a damage site, physically depositing a metal at the damage site in an amount sufficient to replace the removed damaged material, and machining the blade dovetail to the original shape.
Abstract translation: 一种用于将叶片燕尾榫恢复到其原始形状的方法，包括以下步骤：在损坏位置从叶片燕尾of移除损坏的材料，在损伤部位物理沉积金属，其量足以替换去除的损坏材料，并且加工叶片燕尾榫 到原来的形状。
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