-
1.发明公开SYSTEM AND METHOD FOR REJUVENATING COATED COMPONENTS OF GAS TURBINE ENGINES 审中-公开用于再燃燃气涡轮发动机的涂覆组件的系统和方法
公开(公告)号：EP3231989A2
公开(公告)日：2017-10-18
申请号：EP17156241.6
申请日：2017-02-15
CPC分类号： F01D5/005 , C23C10/04 , C23C18/1619 , C23C18/1633 , C23C30/00 , F01D5/288 , F01D9/02 , F01D25/24 , F04D29/324 , F04D29/388 , F04D29/522 , F04D29/542 , F04D29/545 , F05D2220/32 , F05D2230/60 , F05D2230/70 , F05D2230/80 , F05D2230/90 , F05D2300/121 , F05D2300/132 , F05D2300/1431 , F05D2300/222
摘要： The present disclosure is directed to a method for rejuvenating a damaged coated component of a gas turbine engine (10). The method includes uninstalling the damaged coated component from the gas turbine engine (10). The method also includes isolating a first coated portion (105) of the component of the gas turbine engine (10) from a second coated portion (108) of the component. In addition, the method includes simultaneously depositing a first coating material (112) on the first coated portion (105) of the component and a different, second coating material (114) on the second coated portion (108) of the component. The method also includes reinstalling the rejuvenated coated component into the gas turbine engine (10).
摘要翻译： 本公开涉及一种用于使燃气涡轮发动机（10）的损坏的涂覆部件再生的方法。 该方法包括从燃气涡轮发动机（10）卸载损坏的涂覆部件。 该方法还包括将燃气涡轮发动机（10）的部件的第一涂覆部分（105）与部件的第二涂覆部分（108）隔离。 此外，该方法包括在部件的第一涂覆部分（105）上同时沉积第一涂层材料（112），并且在部件的第二涂覆部分（108）上同时沉积不同的第二涂层材料（114）。 该方法还包括将再生的涂覆部件重新安装到燃气涡轮发动机（10）中。
-
2.发明公开
公开(公告)号：EP3341503A1
公开(公告)日：2018-07-04
申请号：EP16757524.0
申请日：2016-08-23
发明人： TANG, Zhihong , GARING, Kevin, E. , KNAPP, James, K. , FEUERSTEIN, Albert , LEWIS, Thomas, F., III
CPC分类号： C23C22/73 , C09D5/103 , C09D101/284 , C23C10/58 , C23C22/82 , C23C28/321 , C23C28/3455 , C23C30/00 , F01D5/288 , F01D9/02 , F01D25/007 , F05D2220/32 , F05D2230/23 , F05D2230/30 , F05D2230/40 , F05D2230/90 , F05D2300/1431 , F05D2300/1434 , F05D2300/1435 , F05D2300/182 , F05D2300/20
摘要： Novel slurry formulations and processes for forming improved protective coatings used in the hot section components of gas turbine engines are provided. The process includes a unique two-step deposition methodology whereby the required concentration of reactive element within an improved reactive element doped aluminide coating can be consistently produced in a reproducible manner.
-
公开(公告)号：EP3231989A3
公开(公告)日：2017-11-15
申请号：EP17156241.6
申请日：2017-02-15
CPC分类号： F01D5/005 , C23C10/04 , C23C18/1619 , C23C18/1633 , C23C30/00 , F01D5/288 , F01D9/02 , F01D25/24 , F04D29/324 , F04D29/388 , F04D29/522 , F04D29/542 , F04D29/545 , F05D2220/32 , F05D2230/60 , F05D2230/70 , F05D2230/80 , F05D2230/90 , F05D2300/121 , F05D2300/132 , F05D2300/1431 , F05D2300/222
摘要： The present disclosure is directed to a method for rejuvenating a damaged coated component of a gas turbine engine (10). The method includes uninstalling the damaged coated component from the gas turbine engine (10). The method also includes isolating a first coated portion (105) of the component of the gas turbine engine (10) from a second coated portion (108) of the component. In addition, the method includes simultaneously depositing a first coating material (112) on the first coated portion (105) of the component and a different, second coating material (114) on the second coated portion (108) of the component. The method also includes reinstalling the rejuvenated coated component into the gas turbine engine (10).
-
4.发明公开
公开(公告)号：EP2886684A1
公开(公告)日：2015-06-24
申请号：EP14199522.5
申请日：2014-12-20
申请人： Howmet Corporation
CPC分类号： F01D5/286 , C25D3/50 , C25D5/022 , C25D5/08 , C25D5/48 , C25D7/00 , C25D7/04 , C25D17/004 , C25D17/10 , C25D17/12 , F01D5/186 , F01D9/02 , F05D2230/31 , F05D2300/143 , F05D2300/1431 , F05D2300/175 , F05D2300/177
摘要： Method and apparatus are provided for electroplating a surface area of an internal wall defining a cooling cavity present in a gas turbine engine component.
摘要翻译： 提供了用于电镀限定燃气涡轮发动机部件中存在的冷却腔的内壁的表面区域的方法和装置。
-
-
-
搜索结果
4 条记录 (耗时 0.007 秒)
