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1. 发明申请

US20100169048A1 MAINTENANCE PLANNING METHOD 审中-公开
标题翻译：维护规划方法
公开(公告)号：US20100169048A1
公开(公告)日：2010-07-01
申请号：US12441303
申请日：2007-09-07
申请人： Klaus Hanreich , Rolf Burmeister , Torsten Petrick , Ferdinand Exler
发明人： Klaus Hanreich , Rolf Burmeister , Torsten Petrick , Ferdinand Exler
IPC分类号： G06F15/00
CPC分类号： F01D5/005 , F05D2230/80 , G06Q10/00
摘要： A maintenance planning method for turbomachines, especially for gas turbine aircraft engines, is disclosed. In an embodiment, the method includes: a) data obtained from the previous maintenance of turbomachines is stored in a database in a structured manner, where the data especially correlates maintenance work carried out with operating loads of a serviced turbomachine; b) in order to pre-plan the maintenance of a turbomachine undergoing further maintenance, the maintenance work to be carried out is planned in terms of type and sequence on the basis of the database; and c) the turbomachine undergoing further maintenance is inspected for the final planning of the maintenance, and the type and/or sequence of the maintenance work to be carried out, which was specified during the pre-planning of the maintenance, is adapted and/or supplemented on the basis of the inspection.
摘要翻译：公开了一种用于涡轮机的维护计划方法，特别是用于燃气涡轮机的发动机。在一个实施例中，该方法包括：a）从先前维护涡轮机获得的数据以结构化的方式存储在数据库中，其中数据特别地与维修工作与维修的涡轮机的运行负载相关联; b）为了预先维护正在进行进一步维护的涡轮机，要按数据库的类型和顺序计划进行的维护工作; 并且c）对进行进一步维护的涡轮机进行维护的最终计划的检查，并且在维护的预先规划期间指定的要执行的维护工作的类型和/或顺序被适配和/ 或在检查的基础上进行补充。

2. 发明申请

US20060272152A1 Method for the maintenance of gas turbines 有权
标题翻译：燃气轮机维修方法
公开(公告)号：US20060272152A1
公开(公告)日：2006-12-07
申请号：US10554471
申请日：2004-03-29
申请人： Rolf Burmeister , Ferdinand Exler , Torsten Petrick , Heinz-Juergen Siedow , Lutz Winkler
发明人： Rolf Burmeister , Ferdinand Exler , Torsten Petrick , Heinz-Juergen Siedow , Lutz Winkler
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。

3. 发明授权

US07827686B2 Method for the maintenance of gas turbines 有权
标题翻译：燃气轮机维修方法
公开(公告)号：US07827686B2
公开(公告)日：2010-11-09
申请号：US10554471
申请日：2004-03-29
申请人： Rolf Burmeister , Ferdinand Exler , Torsten Petrick , Heinz-Juergen Siedow , Lutz Winkler
发明人： Rolf Burmeister , Ferdinand Exler , Torsten Petrick , Heinz-Juergen Siedow , Lutz Winkler
IPC分类号： B21D39/03 , B21K25/00 , B23P6/00 , B23P19/00 , B23P19/04 , B23P23/00
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 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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