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公开(公告)号：US20130174869A1
公开(公告)日：2013-07-11
申请号：US13813919
申请日：2011-08-03
申请人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
发明人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
IPC分类号： B24C1/00
CPC分类号： B24C1/003 , B08B7/0021 , B08B9/00 , B24C1/086 , B24C3/325 , F01D25/002
摘要： The invention relates to a method for cleaning a turbo-machine stage (100) consisting of at least one of the following steps: a cleaning nozzle (1) is introduced into an opening of a turbo-machine, in particular into an inspection opening (220); and the blade (100) of the stage is acted upon by solid particles, said particles subliming at the blade temperature, in particular into dry ice particles.
摘要翻译： 本发明涉及一种用于清洁由以下至少一个步骤组成的涡轮机台（100）的方法：将清洁喷嘴（1）引入涡轮机的开口中，特别是引入到检查开口 220）; 并且所述台的叶片（100）由固体颗粒作用，所述颗粒在叶片温度下升华，特别是干冰颗粒。
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公开(公告)号：US09492906B2
公开(公告)日：2016-11-15
申请号：US13813919
申请日：2011-08-03
申请人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
发明人： Jürgen Rösing , Frank Seidel , Lutz Winkler , Bernd Kriegl , Thomas Uihlein , Martin Dürr , Fabian Moritz
CPC分类号： B24C1/003 , B08B7/0021 , B08B9/00 , B24C1/086 , B24C3/325 , F01D25/002
摘要： The invention relates to a method for cleaning a turbo-machine stage (100) consisting of at least one of the following steps: a cleaning nozzle (1) is introduced into an opening of a turbo-machine, in particular into an inspection opening (220); and the blade (100) of the stage is acted upon by solid particles, said particles subliming at the blade temperature, in particular into dry ice particles.
摘要翻译： 本发明涉及一种用于清洁由以下至少一个步骤组成的涡轮机台（100）的方法：将清洁喷嘴（1）引入涡轮机的开口中，特别是引入到检查开口 220）; 并且所述台的叶片（100）由固体颗粒作用，所述颗粒在叶片温度下升华，特别是干冰颗粒。
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公开(公告)号：US20060272152A1
公开(公告)日：2006-12-07
申请号：US10554471
申请日：2004-03-29
IPC分类号： B23P6/00
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/60 , F05D2230/70 , F05D2230/80 , Y10T29/49318 , Y10T29/4932 , Y10T29/4973 , Y10T29/49829 , Y10T29/5137 , Y10T29/534
摘要： A method for the maintenance of gas turbines is provided. According to method, a gas turbine is dismantled and modules, structural components, or component parts of the aeroplane mechanism are subsequently inspected and/or repaired. Then, an aeroplane mechanism consisting of inspected and/or repaired or new modules, structural components or component parts is mounted. Dismantling and/or mounting is divided into at least two work steps. A work station is provided for each work step and the aeroplane mechanism, modules, structural components or component parts of the aeroplane mechanism are displaced by the work station provided for carrying out one work step.
摘要翻译： 提供了维护燃气轮机的方法。 根据方法，拆卸燃气轮机，随后对飞机机构的模块，结构部件或部件进行检查和/或修理。 然后，安装由检查和/或修理或新模块，结构部件或部件组成的飞机机构。 拆卸和/或安装分为至少两个工作步骤。 为每个工作步骤提供工作站，并且飞机机构的飞机机构，模块，结构部件或组件部分被设置用于执行一个工作步骤的工作站移动。
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公开(公告)号：US07827686B2
公开(公告)日：2010-11-09
申请号：US10554471
申请日：2004-03-29
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/60 , F05D2230/70 , F05D2230/80 , Y10T29/49318 , Y10T29/4932 , Y10T29/4973 , Y10T29/49829 , Y10T29/5137 , Y10T29/534
摘要： A method for the maintenance of gas turbines is provided. According to the method, a gas turbine is dismantled and modules, structural components, or component parts of the aeroplane mechanism are subsequently inspected and/or repaired. Then, an aeroplane mechanism consisting of inspected and/or repaired or new modules, structural components or component parts is mounted. Dismantling and/or mounting is divided into at least two work steps. A work station is provided for each work step and the aeroplane mechanism, modules, structural components or component parts of the aeroplane mechanism are displaced by the work station provided for carrying out one work step.
摘要翻译： 提供了维护燃气轮机的方法。 根据该方法，拆除燃气轮机，随后对飞机机构的模块，结构部件或部件进行检查和/或修理。 然后，安装由检查和/或修理或新模块，结构部件或部件组成的飞机机构。 拆卸和/或安装分为至少两个工作步骤。 为每个工作步骤提供工作站，并且飞机机构的飞机机构，模块，结构部件或组件部分被设置用于执行一个工作步骤的工作站移动。
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