公开(公告)号：US20100313568A1

公开(公告)日：2010-12-16

申请号：US12485505

申请日：2009-06-16

申请人： LEWIS BERKLEY DAVIS, JR. ,  FEI HAN ,  SHIVA SRINIVASAN ,  KAPIL KUMAR SINGH ,  KWANWOO KIM ,  VENKATESWARLU NARRA

发明人： LEWIS BERKLEY DAVIS, JR. ,  FEI HAN ,  SHIVA SRINIVASAN ,  KAPIL KUMAR SINGH ,  KWANWOO KIM ,  VENKATESWARLU NARRA

IPC分类号： F02C7/24

CPC分类号： F23R3/002 ,  F23M20/005 ,  F23R2900/00013 ,  F23R2900/00014

摘要： A combustor for a gas turbine engine and related method is provided in which a plurality of combustor cans are selectively adapted with corresponding resonators. The resonators may, for example, be attached to every can in the consecutive arrangement of combustor cans, every other can, every third can or the like, and may be tuned to the same or first, second, third, etc. frequencies of operation. Such selective tuning is configured to suppress one or more of out-of-phase and in-phase dynamic interaction of streams discharged from adjacent combustor cans by changing the frequencies of pressure oscillation instabilities across the arrangement of consecutive cans.

摘要翻译： 提供了一种用于燃气涡轮发动机的燃烧器和相关方法，其中多个燃烧器罐选择性地适应于相应的谐振器。 例如，谐振器可以在燃烧器罐的连续布置中，每隔一个可以，每隔三分之一或者类似地连接到每个罐，并且可以调谐到相同或第一，第二，第三等操作频率 。 这种选择性调谐被配置为通过改变跨连续罐排列的压力振荡不稳定性的频率来抑制从相邻燃烧器罐排出的流的异相和同相动态相互作用中的一个或多个。