发明名称 GAS TURBINE COMBUSTOR
摘要 A gas turbine combustor in which a part or all of the wall of the combustor disposed within an intake chamber is formed as an acoustic energy absorbing member that can absorb the acoustic energy of a combustion variation generated within the combustor. The acoustic energy absorbing member is constructed of a thin corrugated plate in a circumferential direction, a high-temperature-proof perforated material, or a back plate disposed at the outside of a perforated plate in a radial direction with a distance from the perforated plate. It is also possible to provide a covering member at the outside of the acoustic energy absorbing member in a radial direction, for covering the acoustic energy absorbing member with a distance from the acoustic energy absorbing member. It is preferable that the acoustic energy-absorbing member and/or the covering member are reinforced with a frame that extends in a circumferential direction and/or a longitudinal direction.
申请公布号 CA2366704(C) 申请公布日期 2008.11.04
申请号 CA20022366704 申请日期 2002.01.03
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 IKEDA, KAZUFUMI;OHNISHI, KEIZO;ONO, MASAKI;NISHIMURA, MASAHARU;TANAKA, KATSUNORI
分类号 F23R3/42;F23M99/00;F23R3/00 主分类号 F23R3/42
代理机构 代理人
主权项
地址