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Patent Agency Ranking
公开(公告)号：US08876448B1
公开(公告)日：2014-11-04
申请号：US14012503
申请日：2013-08-28
Applicant: General Electric Company
Inventor： John Raymond Hess , Netaji Haribhau Mane , Gregory Allan Crum , Jason Allen Seale , David William Hogg
CPC classification number: B60P7/06 , F01D25/28 , F01D25/285 , F05D2260/02
Abstract: A shipping fixture for a turbine lower casing includes a frame having a substantially rectangular shape including a pair of elongated, laterally-spaced side beams and a pair of transverse end beams. A first lateral support structure extends between the side beams at a first location corresponding to a first vertically-oriented joint between the turbine compressor casing section and the turbine combustor casing section; and a second lateral support structure includes support blocks mounted on the side beams at a second location corresponding to a second vertically-oriented joint between the turbine combustor casing section and the turbine stage casing section.
Abstract translation: 用于涡轮机下壳体的运输夹具包括具有基本上矩形形状的框架，该框架包括一对细长的，横向间隔开的侧梁和一对横向端梁。 第一侧向支撑结构在对应于涡轮压缩机壳体部分和涡轮机燃烧器壳体部分之间的第一垂直定向接头的第一位置处在侧梁之间延伸; 并且第二横向支撑结构包括安装在所述侧梁上的支撑块，所述支撑块在对应于所述涡轮燃烧器壳体部分和所述涡轮级壳体部分之间的第二垂直定向接头的第二位置处。
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公开(公告)号：US10184357B2
公开(公告)日：2019-01-22
申请号：US15017968
申请日：2016-02-08
Applicant: General Electric Company
Inventor： Netaji Haribhau Mane , Padmapriya Vijayakumar , Jason Allen Seale
Abstract: A partially assembled casing for a turbine including: an assembly of connected casing sections, wherein the assembly does not form a complete casing for the turbine; a gap in the assembly of connected casing sections, wherein the gap corresponds to an absent casing section which is not included in the assembly of connected casing sections, and a frame inserted in the gap and providing structural support to the assembly of connected casing sections.
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公开(公告)号：US09273569B2
公开(公告)日：2016-03-01
申请号：US13736421
申请日：2013-01-08
Applicant: General Electric Company
Inventor： Jason Allen Seale , Gregory Allan Crum , Netaji Haribhau Mane
CPC classification number: F01D25/243 , F01D25/26 , F01D25/285 , F05D2260/02
Abstract: A lifting fixture assembly adapted for shipping and/or lifting includes a lower turbine casing having two horizontal joint flanges adapted to engage mating flanges on an upper-turbine casing. The horizontal joint flanges are provided with plural bolt holes used for securing the upper turbine casing to the lower turbine casing. A plurality of cross-beams extend transversely across the lower turbine casing, removably secured to said horizontal joint flanges, using selected ones of the existing bolt holes.
Abstract translation: 适于运输和/或提升的起重工具组件包括具有两个水平接头凸缘的下涡轮机壳体，其适于接合上涡轮机壳体上的配合凸缘。 水平接头凸缘设有多个螺栓孔，用于将上涡轮机壳体固定到下涡轮机壳体。 多个横梁横向延伸穿过下涡轮机壳体，使用选定的现有螺栓孔可拆卸地固定到所述水平接头凸缘。
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公开(公告)号：US11767978B2
公开(公告)日：2023-09-26
申请号：US17382458
申请日：2021-07-22
Applicant: General Electric Company
Inventor： Dana Morgan , Lucas John Stoia , Elizabeth Leigh Exley , Mohan Krishna Bobba , Netaji Haribhau Mane , John Bryan Pourcho
CPC classification number: F23R3/343 , F02C7/24 , F05D2260/231 , F23C1/08 , F23D11/38 , F23D17/002 , F23R3/36
Abstract: A cartridge tip includes a main body having an outer annular wall and an inner core each extending between a respective upstream end and a respective downstream end. The inner core is radially spaced apart from the outer annular wall such that an annular air passage is defined at least partially between the outer annular wall and the inner core. A pilot fuel circuit extends between a pilot inlet defined in the upstream end of the inner core and a pilot outlet defined in a downstream end of the inner core. The pilot fuel circuit extends at least partially along an axial centerline of the cartridge tip. A main fuel circuit extends between a main inlet in the upstream end of the inner core and a plurality of main outlets circumferentially spaced apart from one another and disposed upstream from the from the pilot outlet.
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公开(公告)号：US20230022306A1
公开(公告)日：2023-01-26
申请号：US17382458
申请日：2021-07-22
Applicant: General Electric Company
Inventor： Dana Morgan , Lucas John Stoia , Elizabeth Leigh Exley , Mohan Krishna Bobba , Netaji Haribhau Mane , John Bryan Pourcho
Abstract: A cartridge tip includes a main body having an outer annular wall and an inner core each extending between a respective upstream end and a respective downstream end. The inner core is radially spaced apart from the outer annular wall such that an annular air passage is defined at least partially between the outer annular wall and the inner core. A pilot fuel circuit extends between a pilot inlet defined in the upstream end of the inner core and a pilot outlet defined in a downstream end of the inner core. The pilot fuel circuit extends at least partially along an axial centerline of the cartridge tip. A main fuel circuit extends between a main inlet in the upstream end of the inner core and a plurality of main outlets circumferentially spaced apart from one another and disposed upstream from the from the pilot outlet.
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