发明名称 Combustor resonator with non-uniform resonator passages
摘要 Certain embodiments of the present disclosure include a combustor resonator having a non-uniform annulus between a combustor assembly and a resonator shell. The combustor resonator may further include resonator necks or passages having non-uniform lengths and geometries.
申请公布号 US8966903(B2) 申请公布日期 2015.03.03
申请号 US201113212105 申请日期 2011.08.17
申请人 General Electric Company 发明人 Bobba Mohan Krishna;Kim Kwanwoo;Melton Patrick Benedict;Antoniono Carolyn Ashley
分类号 F02C7/24;F23R3/00 主分类号 F02C7/24
代理机构 Fletcher Yoder, P.C. 代理人 Fletcher Yoder, P.C.
主权项 1. A system, comprising: a combustor assembly comprising: a liner; anda flow sleeve disposed about the liner, wherein the flow sleeve comprises a plurality of resonator passages; and a resonator coupled to the combustor assembly, wherein the resonator comprises a resonator shell extending circumferentially about the combustor assembly to define a resonator chamber, a radial distance between the resonator shell and the combustor assembly is non-uniform, each resonator passage of the plurality of resonator passages comprising a neck extending radially from the flow sleeve toward the resonator shell and a length of the neck varies from one resonator passage to another.
地址 Schenectady NY US