公开(公告)号：US20140126997A1

公开(公告)日：2014-05-08

申请号：US13668855

申请日：2012-11-05

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Eric Tracy Watson ,  Joseph Gabriel Harris ,  Quoc Hoai Nguyen ,  Yunyi Zou

IPC: F04D29/66 ,  F01N1/24

CPC classification number: F01D25/30 ,  F02C7/24 ,  F05D2260/96 ,  G10K11/168

Abstract: 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.

Abstract translation: 用于涡轮机系统的声音衰减烟囱元件包括具有外表面和内表面的高密度外体体，以及设置在外体外表面上的一个或多个声衰减层。 一个或多个声衰减层包括外表面部分和内表面部分。 在一个或多个声衰减层的外表面部分上提供结构层。 结构层包括外表面，该外表面限定了构造和设置成使来自涡轮机系统的气体的管道。

公开(公告)号：US09039352B2

公开(公告)日：2015-05-26

申请号：US13668855

申请日：2012-11-05

Applicant: General Electric Company

Inventor： Eric Tracy Watson ,  Joseph Gabriel Harris ,  Quoc Hoai Nguyen ,  Yunyi Zou

IPC: F04D29/66 ,  F01D25/30 ,  F02C7/24 ,  G10K11/168

CPC classification number: F01D25/30 ,  F02C7/24 ,  F05D2260/96 ,  G10K11/168

Abstract: 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.

Abstract translation: 用于涡轮机系统的声音衰减烟囱元件包括具有外表面和内表面的高密度外体体，以及设置在外体外表面上的一个或多个声衰减层。 一个或多个声衰减层包括外表面部分和内表面部分。 在一个或多个声衰减层的外表面部分上提供结构层。 结构层包括外表面，该外表面限定了构造和设置成使来自涡轮机系统的气体的管道。