发明名称 |
タービン部品の減衰構造 |
摘要 |
Disclosed is a coating for gas turbine components including at least one material having vibration-damping properties. Further disclosed is an airfoil of a gas turbine having damped vibrational characteristics including an airfoil substrate and a coating applied to the airfoil substrate including at least one material having vibration-damping properties. A method of damping vibration of a gas turbine component includes applying a coating including at least one material having damping properties to the turbine component. |
申请公布号 |
JP5932201(B2) |
申请公布日期 |
2016.06.08 |
申请号 |
JP20080212402 |
申请日期 |
2008.08.21 |
申请人 |
ゼネラル・エレクトリック・カンパニイ |
发明人 |
カナン・ウスルー・ハーウィック;ジョン・マックコネル・デルヴォー;ブラッドリー・タイラー・ボイヤー;ジェームズ・ウィリアム・ヴェアー |
分类号 |
F01D25/04;C23C4/04;C23C14/14;F01D5/26;F01D5/28;F01D25/00;F02C7/00 |
主分类号 |
F01D25/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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