发明名称 |
Can combustor for a can-annular combustor arrangement in a gas turbine |
摘要 |
The invention relates to a can-combustor for a can-annular combustor arrangement in a gas turbine, wherein the can combustor (10) at least comprising an essentially cylindrical casing (11) with an axially upstream front panel (13) and an axially downstream outlet end, a number of premixed burners (14), extending in an upstream direction from said front panel (13) and having a burner exit (17), supported by this front panel (13), for supplying a fuel/air mixture into a combustion zone (12) inside the casing (11), wherein up to four premixed burners (14) are attached to the front panel (13) in a substantially annular array, each burner (14) having a conical swirl generator (15) and a mixing tube (16) to induce a swirl flow of said fuel/air mixture. |
申请公布号 |
EP2796789(B1) |
申请公布日期 |
2017.03.01 |
申请号 |
EP20130165488 |
申请日期 |
2013.04.26 |
申请人 |
General Electric Technology GmbH |
发明人 |
Knapp, Klaus;Aluri, Naresh;Tran, Nicolas;Rathmann, Ulrich;Genin, Franklin Marie |
分类号 |
F23R3/14;F23R3/28;F23R3/34;F23R3/46 |
主分类号 |
F23R3/14 |
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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