发明申请
US20090191353A1 TURBINE COMPONENT OTHER THAN AIRFOIL HAVING CERAMIC CORROSION RESISTANT COATING AND METHODS FOR MAKING SAME
审中-公开
除具有陶瓷耐腐蚀涂层的空气涡轮机以外的涡轮机构及其制造方法
- 专利标题: TURBINE COMPONENT OTHER THAN AIRFOIL HAVING CERAMIC CORROSION RESISTANT COATING AND METHODS FOR MAKING SAME
- 专利标题(中): 除具有陶瓷耐腐蚀涂层的空气涡轮机以外的涡轮机构及其制造方法
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申请号: US12421190申请日: 2009-04-09
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公开(公告)号: US20090191353A1公开(公告)日: 2009-07-30
- 发明人: BANGALORE ASWATHA NAGARAJ , BRIAN THOMAS HAZEL , JEFFREY ALLAN PFAENDTNER
- 申请人: BANGALORE ASWATHA NAGARAJ , BRIAN THOMAS HAZEL , JEFFREY ALLAN PFAENDTNER
- 申请人地址: US NY Schenectady
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: US NY Schenectady
- 主分类号: C23C18/02
- IPC分类号: C23C18/02 ; C23C4/10
摘要:
An article comprising a turbine component other than an airfoil having a metal substrate and a ceramic corrosion resistant coating overlaying the metal substrate. This coating has a thickness up to about 5 mils (127 microns) and comprises a ceramic metal oxide selected from the group consisting of zirconia, hafnia and mixtures thereof. This coating can be formed by a method comprising the following steps: (a) providing a turbine component other than an airfoil comprising the metal substrate; (b) providing a gel-forming solution comprising a ceramic metal oxide precursor; (c) heating the gel-forming solution to a first preselected temperature for a first preselected time to form a gel; (d) depositing the gel on the metal substrate; and (e) firing the gel at a second preselected temperature above the first preselected temperature to form the ceramic corrosion resistant coating comprising the ceramic metal oxide. This coating can also be formed by alternative methods wherein a ceramic composition comprising the ceramic metal oxide is deposited by physical vapor deposition on the metal substrate to provide a strain-tolerant columnar structure, or is thermal sprayed on the metal substrate.