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公开(公告)号：US10436072B2
公开(公告)日：2019-10-08
申请号：US15435465
申请日：2017-02-17
Applicant: General Electric Company
Inventor： Quoc Hoai Nguyen , Ashish Agrawal , Horacio Solis , Yunyi Zou , Tho V. Nguyen
Abstract: This application provides elastomeric shock absorbers for turbine transportation. Example engine mounts may include a first plate, a second plate, and an elastomeric bearing positioned between the first plate and the second plate. The engine mount may be configured to absorb or dampen vibration along an X-axis, a Y-axis, and a Z-axis of a turbine during transportation.
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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
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。
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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。
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公开(公告)号：US20180238195A1
公开(公告)日：2018-08-23
申请号：US15435465
申请日：2017-02-17
Applicant: General Electric Company
Inventor： Quoc Hoai Nguyen , Ashish Agrawal , Horacio Solis , Yunyi Zou , Tho V. Nguyen
CPC classification number: F01D25/285 , B60P7/16 , F02C7/20 , F05D2260/02 , F16M7/00
Abstract: This application provides elastomeric shock absorbers for turbine transportation. Example engine mounts may include a first plate, a second plate, and an elastomeric bearing positioned between the first plate and the second plate. The engine mount may be configured to absorb or dampen vibration along an X-axis, a Y-axis, and a Z-axis of a turbine during transportation.
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