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公开(公告)号:US20110203294A1
公开(公告)日:2011-08-25
申请号:US13031880
申请日:2011-02-22
CPC分类号: F23R3/283 , F23R2900/03045 , Y02T50/675
摘要: A fuel injection system for an annular combustion chamber of a turbomachine, the system comprising support means for supporting and centering a fuel injector head, and a bowl arranged downstream from the support means and including at its downstream end an annular collar that extends radially outwards and that is cooled by air impacting against its upstream radial surface, and including on said surface means for disturbing the flow of cooling air and for increasing the heat exchange area between the air and the collar.
摘要翻译: 一种用于涡轮机的环形燃烧室的燃料喷射系统,该系统包括用于支撑和定心燃料喷射头的支撑装置,以及设置在支撑装置下游的碗,并且在其下游端包括径向向外延伸的环形套环, 其被空气冲击其上游径向表面而被冷却,并且包括在所述表面上用于干扰冷却空气的流动并增加空气和轴环之间的热交换面积的装置。