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    • 1. 发明授权
    • Modular drop-in combustor assembly for industrial gas turbine and method for installation
    • 用于工业燃气轮机的模块式落地式燃烧器组件及其安装方法
    • US09127593B2
    • 2015-09-08
    • US13670741
    • 2012-11-07
    • Glenn E. SancewichJose L. AlonsoDaniel E. Ford
    • Glenn E. SancewichJose L. AlonsoDaniel E. Ford
    • B23P19/00F01D25/28F02C7/00F23R3/28F23R3/60
    • F02C7/00B23P19/00F01D25/285F05D2230/60F05D2230/68F23R3/283F23R3/60F23R2900/00017Y10T29/49323
    • A preassembled modular drop-in combustor having internal components in conformity with assembly and function specifications prior to and after insertion into an industrial gas turbine access port and internal combustor transition. The combustor assembly maintains conformity with those specifications after insertion into the combustor case if it does not inadvertently impact other turbine components during its installation. Inadvertent impact is avoided by having a combustor service zone proximal the combustor case, enabling slidable insertion of each combustor assembly into its corresponding access port and transition along its corresponding insertion path without contacting other turbine system components. A multi-axis motion combustor handling tool in the combustor service zone, preferably under automatic control, is coupled to each combustor and facilitates precise alignment along the insertion path. Automatic control facilitates consistent repetitive combustor installation and removal by executing a sequence of stored pre-determined manipulation steps.
    • 一种预组装的模块式落入式燃烧器,其在插入工业燃气涡轮机进气口和内部燃烧器转换之前和之后具有符合组装和功能规格的内部部件。 如果燃烧器组件在其安装过程中不会无意中撞击其他涡轮机部件,则在插入燃烧器壳体之后,保持与这些规格的一致性。 通过在燃烧器壳体附近具有燃烧器使用区域,可以避免无意中的冲击,使得每个燃烧器组件能够滑入其相应的进入口并沿其对应的插入路径过渡而不接触其它涡轮机系统部件。 燃烧器使用区域中的多轴运动燃烧器处理工具优选地在自动控制下被联接到每个燃烧器,并且有助于沿着插入路径的精确对准。 自动控制通过执行存储的预定操作步骤的顺序来促进连续重复的燃烧器安装和移除。
    • 2. 发明授权
    • Modular drop-in transition assembly for industrial gas turbine and method for installation
    • 用于工业燃气轮机的模块化落地过渡组件及其安装方法
    • US09255522B2
    • 2016-02-09
    • US13672878
    • 2012-11-09
    • Glenn E. SancewichJose L. AlonsoDaniel E. Ford
    • Glenn E. SancewichJose L. AlonsoDaniel E. Ford
    • F02C7/00F01D9/02F01D25/28
    • F02C7/00F01D9/026F01D25/285F05D2230/60F05D2230/68F05D2230/70F05D2230/80F23R2900/00017
    • A preassembled modular drop-in transition having internal components in conformity with assembly and function specifications prior to and after insertion into an industrial gas turbine access port. The transition assembly maintains conformity with those specifications after insertion into the combustor case if it does not inadvertently impact other turbine components during its installation. Inadvertent impact is avoided by having a combustor service zone proximal the combustor case, enabling slidable insertion of each transition and/or combustor assembly into its corresponding access port along its corresponding insertion path without contacting other turbine system components. A multi-axis motion transition handling tool (THT) in the combustor service zone, preferably under automatic control, is coupled to a transition and facilitates precise alignment along the insertion path. Automatic control facilitates consistent repetitive transition installation and removal by executing a sequence of stored pre-determined manipulation steps.
    • 一个预组装的模块式下降过渡,在插入工业燃气轮机进出口之前和之后,内部组件符合组装和功能规范。 如果在安装过程中不会意外地撞击其他涡轮机部件,则过渡组件在插入燃烧器壳体后会保持与这些规格的一致性。 通过在燃烧器壳体附近具有燃烧器使用区域,可以避免无意中的冲击,从而使得每个过渡和/或燃烧器组件能够沿其相应的插入路径可滑动地插入到其相应的进入端口中,而不会接触其他涡轮机系统部件。 优选在自动控制下的燃烧器维修区域中的多轴运动过渡处理工具(THT)被耦合到过渡并有助于沿插入路径的精确对准。 自动控制通过执行存储的预定操作步骤的顺序来促进一致的重复过渡安装和移除。
    • 3. 发明申请
    • MODULAR DROP-IN COMBUSTOR ASSEMBLY FOR INDUSTIAL GAS TURBINE AND METHOD FOR INSTALLATION
    • 用于污染气体涡轮的模块式卸载式组合装置及其安装方法
    • US20140123680A1
    • 2014-05-08
    • US13670741
    • 2012-11-07
    • GLENN E. SANCEWICHJOSE L. ALONSODANIEL E. FORD
    • GLENN E. SANCEWICHJOSE L. ALONSODANIEL E. FORD
    • F02C7/00B23P19/00
    • F02C7/00B23P19/00F01D25/285F05D2230/60F05D2230/68F23R3/283F23R3/60F23R2900/00017Y10T29/49323
    • A preassembled modular drop-in combustor having internal components in conformity with assembly and function specifications prior to and after insertion into an industrial gas turbine access port and internal combustor transition. The combustor assembly maintains conformity with those specifications after insertion into the combustor case if it does not inadvertently impact other turbine components during its installation. Inadvertent impact is avoided by having a combustor service zone proximal the combustor case, enabling slidable insertion of each combustor assembly into its corresponding access port and transition along its corresponding insertion path without contacting other turbine system components. A multi-axis motion combustor handling tool in the combustor service zone, preferably under automatic control, is coupled to each combustor and facilitates precise alignment along the insertion path. Automatic control facilitates consistent repetitive combustor installation and removal by executing a sequence of stored pre-determined manipulation steps.
    • 一种预组装的模块式落入式燃烧器,其在插入工业燃气涡轮机进气口和内部燃烧器转换之前和之后具有符合组装和功能规格的内部部件。 如果燃烧器组件在其安装过程中不会无意中撞击其他涡轮机部件,则在插入燃烧器壳体之后,保持与这些规格的一致性。 通过在燃烧器壳体附近具有燃烧器使用区域,可以避免无意中的冲击,使得每个燃烧器组件能够滑入其相应的进入口并沿其对应的插入路径过渡而不接触其它涡轮机系统部件。 燃烧器使用区域中的多轴运动燃烧器处理工具优选地在自动控制下被联接到每个燃烧器,并且有助于沿着插入路径的精确对准。 自动控制通过执行存储的预定操作步骤的顺序来促进连续重复的燃烧器安装和移除。
    • 5. 发明申请
    • MODULAR DROP-IN TRANSITION ASSEMBLY FOR INDUSTRIAL GAS TURBINE AND METHOD FOR INSTALLATION
    • 用于工业气体涡轮机的模块式倾倒式组装及其安装方法
    • US20140123656A1
    • 2014-05-08
    • US13672878
    • 2012-11-09
    • GLENN E. SANCEWICHJOSE L. ALONSODANIEL E. FORD
    • GLENN E. SANCEWICHJOSE L. ALONSODANIEL E. FORD
    • F02C7/00
    • F02C7/00F01D9/026F01D25/285F05D2230/60F05D2230/68F05D2230/70F05D2230/80F23R2900/00017
    • A preassembled modular drop-in transition having internal components in conformity with assembly and function specifications prior to and after insertion into an industrial gas turbine access port. The transition assembly maintains conformity with those specifications after insertion into the combustor case if it does not inadvertently impact other turbine components during its installation. Inadvertent impact is avoided by having a combustor service zone proximal the combustor case, enabling slidable insertion of each transition and/or combustor assembly into its corresponding access port along its corresponding insertion path without contacting other turbine system components. A multi-axis motion transition handling tool (THT) in the combustor service zone, preferably under automatic control, is coupled to a transition and facilitates precise alignment along the insertion path. Automatic control facilitates consistent repetitive transition installation and removal by executing a sequence of stored pre-determined manipulation steps.
    • 一个预组装的模块式下降过渡,在插入工业燃气轮机进出口之前和之后,内部组件符合组装和功能规范。 如果在安装过程中不会意外地撞击其他涡轮机部件,则过渡组件在插入燃烧器壳体后会保持与这些规格的一致性。 通过在燃烧器壳体附近具有燃烧器使用区域,可以避免无意中的冲击,从而使得每个过渡和/或燃烧器组件能够沿其相应的插入路径可滑动地插入到其相应的进入端口中,而不会接触其他涡轮机系统部件。 优选在自动控制下的燃烧器维修区域中的多轴运动过渡处理工具(THT)被耦合到过渡并有助于沿插入路径的精确对准。 自动控制通过执行存储的预定操作步骤的顺序来促进一致的重复过渡安装和移除。