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公开(公告)号：US07735222B2
公开(公告)日：2010-06-15
申请号：US11290347
申请日：2005-11-30
Applicant: Graham David Sherlock , Paul Lawrence Kalmar
Inventor： Graham David Sherlock , Paul Lawrence Kalmar
IPC: B23P6/00
CPC classification number: B23P6/002 , F01D5/3007 , F05D2230/10 , F05D2230/80 , Y10T29/49318 , Y10T29/49336
Abstract: A tool capable of removing material is applied to a turbine wheel cooling slot. Material is removed from a selected portion of the cooling slot with the tool. And, stress concentrations are reduced within the slot through the removal of material.
Abstract translation: 能够移除材料的工具被施加到涡轮机叶轮冷却槽。 用工具从冷却槽的选定部分移除材料。 并且，通过去除材料，在槽内减少应力集中。
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公开(公告)号：US20140064954A1
公开(公告)日：2014-03-06
申请号：US13599145
申请日：2012-08-30
Applicant: Anshuman Singh , Paul Lawrence Kalmar , Graham David Sherlock , Americo Zapata
Inventor： Anshuman Singh , Paul Lawrence Kalmar , Graham David Sherlock , Americo Zapata
CPC classification number: F01D5/005 , B23P6/005 , F01D11/001 , Y10T29/49318
Abstract: A turbomachine diaphragm includes a sealing section having a first end portion that extends to a second end portion through an intermediate portion. At least one rail member includes a first end section that extends from the first end portion of the sealing section to a second end section through an intermediate section having an inner surface section and an outer surface section. The second end section includes a machined surface having a repair coupon mounting element. A repair coupon is mounted at the repair coupon mounting element and operatively connected to the at least one rail member. A method of repairing a turbomachine diaphragm is also disclosed herein.
Abstract translation: 涡轮机械振动膜包括具有通过中间部分延伸到第二端部的第一端部的密封部分。 至少一个轨道构件包括通过具有内表面部分和外表面部分的中间部分从密封部分的第一端部延伸到第二端部的第一端部部分。 第二端部分包括具有修复试样安装元件的加工表面。 修理券被安装在修理券安装元件上并且可操作地连接到至少一个轨道构件。 本文还公开了一种维修涡轮机隔膜的方法。
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公开(公告)号：US08051564B2
公开(公告)日：2011-11-08
申请号：US11621152
申请日：2007-01-09
Applicant: Graham David Sherlock , Christopher Edward Thompson
Inventor： Graham David Sherlock , Christopher Edward Thompson
IPC: B21K25/00
CPC classification number: G01B5/25 , F01D9/044 , F01D25/285 , F05D2230/64
Abstract: A method for fabricating a nozzle segment for use within a turbine nozzle assembly. The method comprises providing a nozzle segment including an outer band, an inner band, and at least one vane extending there between, wherein at least one of the inner band and the outer band is formed with a transition piece groove defined therein, positioning an inspection tool in contact with the nozzle assembly such that the inspection tool is aligned relative to the nozzle segment using at least one datum, and verifying an alignment of each transition piece groove using the inspection tool.
Abstract translation: 一种用于制造在涡轮喷嘴组件内使用的喷嘴段的方法。 该方法包括提供包括外带，内带和在其间延伸的至少一个叶片的喷嘴段，其中内带和外带中的至少一个形成有限定在其中的过渡件槽，定位检查 与喷嘴组件接触的工具，使得检查工具使用至少一个基准相对于喷嘴段对准，并使用检查工具验证每个过渡件槽的对准。
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公开(公告)号：US20080115648A1
公开(公告)日：2008-05-22
申请号：US11822790
申请日：2007-07-10
Applicant: Graham David Sherlock , Lynn Charles Gagne
Inventor： Graham David Sherlock , Lynn Charles Gagne
CPC classification number: F01D5/005 , B23C3/18 , F01D5/027 , F04D29/542 , F05D2230/10 , F05D2230/50 , F05D2260/96 , Y10T83/0605 , Y10T83/68
Abstract: An assembly is provided for cropping the trailing edge tip of a stator zero blade in-situ. The cropping assembly includes a base plate that is secured to the end of the compressor stator blade to be cropped; a removable, rotational guide block; and a drill that is mounted to the guide block and rotatable relative to the base plate to crop the trailing edge tip of a stator blade.
Abstract translation: 提供了用于在现场裁剪定子零叶片的后缘尖端的组件。 裁剪组件包括固定到待裁剪的压缩机定子叶片的端部的基板; 可移动的旋转引导块; 以及钻头，其安装到引导块并且可相对于基板旋转以裁剪定子叶片的后缘尖端。
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公开(公告)号：US09303515B2
公开(公告)日：2016-04-05
申请号：US13599145
申请日：2012-08-30
Applicant: Anshuman Singh , Paul Lawrence Kalmar , Graham David Sherlock , Americo Zapata
Inventor： Anshuman Singh , Paul Lawrence Kalmar , Graham David Sherlock , Americo Zapata
CPC classification number: F01D5/005 , B23P6/005 , F01D11/001 , Y10T29/49318
Abstract: A turbomachine diaphragm includes a sealing section having a first end portion that extends to a second end portion through an intermediate portion. At least one rail member includes a first end section that extends from the first end portion of the sealing section to a second end section through an intermediate section having an inner surface section and an outer surface section. The second end section includes a machined surface having a repair coupon mounting element. A repair coupon is mounted at the repair coupon mounting element and operatively connected to the at least one rail member. A method of repairing a turbomachine diaphragm is also disclosed herein.
Abstract translation: 涡轮机械振动膜包括具有通过中间部分延伸到第二端部的第一端部的密封部分。 至少一个轨道构件包括通过具有内表面部分和外表面部分的中间部分从密封部分的第一端部延伸到第二端部的第一端部部分。 第二端部分包括具有修复试样安装元件的加工表面。 修理券被安装在修理券安装元件上并且可操作地连接到至少一个轨道构件。 本文还公开了一种维修涡轮机隔膜的方法。
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Patent Agency Ranking
公开(公告)号：US20120023746A1
公开(公告)日：2012-02-02
申请号：US13270521
申请日：2011-10-11
Applicant: Graham David Sherlock , Christopher Edward Thompson
Inventor： Graham David Sherlock , Christopher Edward Thompson
CPC classification number: G01B5/25 , F01D9/044 , F01D25/285 , F05D2230/64
Abstract: A method for fabricating a nozzle segment for use within a turbine nozzle assembly. The method comprises providing a nozzle segment including an outer band, an inner band, and at least one vane extending there between, wherein at least one of the inner band and the outer band is formed with a transition piece groove defined therein, positioning an inspection tool in contact with the nozzle assembly such that the inspection tool is aligned relative to the nozzle segment using at least one datum, and verifying an alignment of each transition piece groove using the inspection tool.
Abstract translation: 一种用于制造在涡轮喷嘴组件内使用的喷嘴段的方法。 该方法包括提供包括外带，内带和在其间延伸的至少一个叶片的喷嘴段，其中内带和外带中的至少一个形成有限定在其中的过渡件槽，定位检查 与喷嘴组件接触的工具，使得检查工具使用至少一个基准相对于喷嘴段对准，并使用检查工具验证每个过渡件槽的对准。
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公开(公告)号：US07806655B2
公开(公告)日：2010-10-05
申请号：US11679468
申请日：2007-02-27
Applicant: Lynn Charles Gagne , Graham David Sherlock , Kelvin Aaron , Thomas Robbins Tipton
Inventor： Lynn Charles Gagne , Graham David Sherlock , Kelvin Aaron , Thomas Robbins Tipton
IPC: F01D9/04
CPC classification number: F01D9/042 , F05D2250/191
Abstract: A method for assembling a stator assembly for a turbine engine is provided. The method includes providing a blade with a base including an end wall having at least one hole defined therein and providing a shim having at least one aperture extending therethrough. The shim aperture is aligned with the end wall hole, and the shim is secured to the blade base end wall using a fastener. The fastener is inserted through the shim aperture in an interference fit within the end wall hole. The blade and the shim are coupled to a turbine casing.
Abstract translation: 提供一种用于组装用于涡轮发动机的定子组件的方法。 该方法包括提供具有底座的刀片，底座包括具有限定在其中的至少一个孔的端壁，并提供具有延伸穿过其中的至少一个孔的垫片。 垫片孔与端壁孔对齐，并且垫片使用紧固件固定到刀片底端壁上。 紧固件通过垫片孔以过盈配合插入端壁孔内。 叶片和垫片联接到涡轮机壳体。
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公开(公告)号：US07766726B2
公开(公告)日：2010-08-03
申请号：US11822790
申请日：2007-07-10
Applicant: Graham David Sherlock , Lynn Charles Gagne
Inventor： Graham David Sherlock , Lynn Charles Gagne
IPC: B24B23/08
CPC classification number: F01D5/005 , B23C3/18 , F01D5/027 , F04D29/542 , F05D2230/10 , F05D2230/50 , F05D2260/96 , Y10T83/0605 , Y10T83/68
Abstract: An assembly is provided for cropping the trailing edge tip of a stator zero blade in-situ. The cropping assembly includes a base plate that is secured to the end of the compressor stator blade to be cropped; a removable, rotational guide block; and a drill that is mounted to the guide block and rotatable relative to the base plate to crop the trailing edge tip of a stator blade.
Abstract translation: 提供了用于在现场裁剪定子零叶片的后缘尖端的组件。 裁剪组件包括固定到待裁剪的压缩机定子叶片的端部的基板; 可移动的旋转引导块; 以及钻头，其安装到引导块并且可相对于基板旋转以裁剪定子叶片的后缘尖端。
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公开(公告)号：US07735238B2
公开(公告)日：2010-06-15
申请号：US12183434
申请日：2008-07-31
Applicant: Graham David Sherlock , Paul Lawrence Kalmar
Inventor： Graham David Sherlock , Paul Lawrence Kalmar
IPC: G01B5/02
CPC classification number: G01B3/20
Abstract: A measuring tool measures a trailing edge position of gas turbine nozzle. The tool includes a frame member attachable to at least one predefined reference point on the nozzle. At least one sliding member is slidable relative to the frame member and includes a measuring point engageable with the trailing edge. A position of the sliding member relative to the frame member is determinative of the trailing edge position.
Abstract translation: 测量工具测量燃气轮机喷嘴的后缘位置。 该工具包括可附接到喷嘴上的至少一个预定参考点的框架构件。 至少一个滑动构件可相对于框架构件滑动并且包括可与后缘接合的测量点。 滑动构件相对于框架构件的位置决定于后缘位置。
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公开(公告)号：US20100024238A1
公开(公告)日：2010-02-04
申请号：US12183434
申请日：2008-07-31
Applicant: Graham David Sherlock , Paul Lawrence Kalmar
Inventor： Graham David Sherlock , Paul Lawrence Kalmar
IPC: G01B5/02
CPC classification number: G01B3/20
Abstract: A measuring tool measures a trailing edge position of gas turbine nozzle. The tool includes a frame member attachable to at least one predefined reference point on the nozzle. At least one sliding member is slidable relative to the frame member and includes a measuring point engageable with the trailing edge. A position of the sliding member relative to the frame member is determinative of the trailing edge position.
Abstract translation: 测量工具测量燃气轮机喷嘴的后缘位置。 该工具包括可附接到喷嘴上的至少一个预定参考点的框架构件。 至少一个滑动构件可相对于框架构件滑动并且包括可与后缘接合的测量点。 滑动构件相对于框架构件的位置决定于后缘位置。
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