发明名称 Sound attenuating chimney element for a turbomachine system
摘要 A sound attenuating chimney element for a turbomachine system includes a high density outer body having an external surface and an internal surface, and one or more acoustic attenuation layers provided on the external surface of the outer body. The one or more acoustic attenuation layers include an outer surface portion and an inner surface portion. A structural layer is provided on the outer surface portion of the one or more acoustic attenuation layers. The structural layer includes an external surface that defines a duct configured and disposed to pass gases from the turbomachine system.
申请公布号 US9039352(B2) 申请公布日期 2015.05.26
申请号 US201213668855 申请日期 2012.11.05
申请人 GENERAL ELECTRIC COMPANY 发明人 Watson Eric Tracy;Harris Joseph Gabriel;Nguyen Quoc Hoai;Zou Yunyi
分类号 F04D29/66;F01D25/30;F02C7/24;G10K11/168 主分类号 F04D29/66
代理机构 Cantor Colburn LLP 代理人 Cantor Colburn LLP
主权项 1. A sound attenuating chimney element for a turbomachine system comprising: a high density outer body including an external surface and an internal surface; one or more acoustic attenuation layers provided on the internal surface of the high density outer body, the one or more acoustic attenuation layers including an outer surface portion and an inner surface portion; and a structural layer comprising concrete provided on the inner surface portion of the one or more acoustic attenuation layers, the structural layer including an internal surface section that defines a duct configured and disposed to pass exhaust gases from the turbomachine system.
地址 Schenectady NY US