发明授权
US09353948B2 Gas turbine combustor including a coating having reflective characteristics for radiation heat and method for improved combustor temperature uniformity
有权
包括具有用于辐射热的反射特性的涂层的燃气轮机燃烧器和用于改善燃烧器温度均匀性的方法
- 专利标题： Gas turbine combustor including a coating having reflective characteristics for radiation heat and method for improved combustor temperature uniformity
- 专利标题（中）： 包括具有用于辐射热的反射特性的涂层的燃气轮机燃烧器和用于改善燃烧器温度均匀性的方法
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申请号： US13334173申请日： 2011-12-22
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公开(公告)号： US09353948B2公开(公告)日： 2016-05-31
- 发明人: Hendrik Pieter Jacobus de Bock , Mark Allan Hadley , Joel Meier Haynes , Brian Gene Brzek
- 申请人： Hendrik Pieter Jacobus de Bock , Mark Allan Hadley , Joel Meier Haynes , Brian Gene Brzek
- 申请人地址： US NY Niskayuna
- 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 Niskayuna
- 代理商 Pabrita K. Chakrabarti
- 主分类号： F23R3/00
- IPC分类号： F23R3/00 ; F01D5/28
摘要：
A combustor and a method for reducing a temperature gradient of a combustor component are provided. The combustor includes a coating applied to at least a portion thereof with the coating serving to alter the emissivity of the at least a portion to which it is applied. The method includes applying a coating on at least one of a combustor liner and a flow sleeve, wherein the coating alters the emissivity exhibited where applied.
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