发明名称 Combustor of gas turbine
摘要 Manifolds are shaped cross star having curved surfaces inside thereof, and holes are bored in four corners of the manifolds. In mounting a combustor to a casing, oil in the manifolds is transmitted to the holes by way of the curved surfaces. As a result of this, oil is prevented from staying, and coking is prevented from occurring, inside the manifolds.
申请公布号 US2004237531(A1) 申请公布日期 2004.12.02
申请号 US20040490386 申请日期 2004.04.02
申请人 HIRASAKI TAKEO 发明人 HIRASAKI TAKEO
分类号 F23R3/28;F02C7/232;F23D11/36;F23R3/34;(IPC1-7):F23R3/28 主分类号 F23R3/28
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