发明名称 |
Gas turbine combustor with angled tube section |
摘要 |
A combustor inner tube 102 or a burner 101 provided on the upstream side of a tail pipe 103 having a straight or substantially straight axis is disposed at an angle with respect to the axis of tail pipe 103, by which a secondary flow is produced in combustion gas. Thereby, low-temperature gas at the outer peripheral portion is mixed with high-temperature gas at the central portion so that the gas temperature distribution is made uniform.
|
申请公布号 |
US6006523(A) |
申请公布日期 |
1999.12.28 |
申请号 |
US19970846644 |
申请日期 |
1997.04.30 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
MANDAI, SHIGEMI;SATO, NOBUO;TANIMURA, SATOSHI;KAWABATA, HITOSHI |
分类号 |
F23R3/44;(IPC1-7):F23R3/42 |
主分类号 |
F23R3/44 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|