发明授权
- 专利标题: Process for producing a ceramic thermal barrier layer for gas turbine engine component
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申请号: US10187504申请日: 2002-07-01
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公开(公告)号: US06602553B2公开(公告)日: 2003-08-05
- 发明人: Beate Heimberg , Wolfram Beele , Karl Kempter , Ulrich Bast , Thomas Haubold , Michael Hoffmann , Axel Endriss , Peter Greil , Chu-Wan Hong , Fritz Aldinger , Hans J. Seifert
- 申请人: Beate Heimberg , Wolfram Beele , Karl Kempter , Ulrich Bast , Thomas Haubold , Michael Hoffmann , Axel Endriss , Peter Greil , Chu-Wan Hong , Fritz Aldinger , Hans J. Seifert
- 优先权: DE19748508 19971103
- 主分类号: B05D102
- IPC分类号: B05D102
摘要:
An article that is particularly well suited for use as a gas turbine engine component has a metallic substrate and a ceramic thermal barrier layer including a mixed metal oxide system comprising a compound selected from the group consisting of (i) a lanthanum aluminate and (ii) a calcium zirconate, the calcium in which is partially replaced by at least one calcium-substitute element, such as strontium (Sr) or barium (Ba). In addition, the lanthanum in the lanthanum aluminate can be partially replaced by a lanthanum-substitute element from the lanthanide group, particularly gadolinium (Gd). A process for producing such an article comprises providing a pre-reacted mixed metal oxide system as described above and applying it to the substrate by plasma spraying or an evaporation coating process.