发明名称 Gas Turbine Combustor
摘要 A gas turbine combustor includes a pilot burner, a plurality of main burners disposed around the main burners on the radially outer side. Each of the main burners ( 2 ) includes an extension tube disposed at the downstream end. The outlet of the extension tube is shaped to have a radial edge which is parallel to the radial direction. In this manner, occurrence of flashback is effectively prevented.
申请公布号 US2008184708(A1) 申请公布日期 2008.08.07
申请号 US20050574203 申请日期 2005.09.01
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 MORIWAKI ATSUSHI;OHTA MASATAKA;SAITOH KEIJIRO;TANIMURA SATOSHI;AKAMATSU SHINJI;NAGAI NORIHIKO
分类号 F02C1/00 主分类号 F02C1/00
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