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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：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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公开(公告)号：US09359959B2
公开(公告)日：2016-06-07
申请号：US13956201
申请日：2013-07-31
Applicant: General Electric Company
Inventor： Jose Antonio Cuevas , Tho Nguyen , Horacio Solis
CPC classification number: F02C7/30 , F01D25/002 , F01D25/02 , Y02E20/16 , Y02E20/18
Abstract: A system includes a gas turbine system that has a turbine, a combustor, and a compressor having an air intake. The air intake is configured to supply an air flow to the compressor. The system also includes a fluid injection system that has a fluid wash system configured to inject a wash fluid into the gas turbine system via the air intake. The fluid wash system includes an injector configured to inject the wash fluid into the gas turbine system and an anti-icing system configured to inject an anti-icing fluid into the gas turbine system via the air intake. The anti-icing system is configured to inject the anti-icing fluid into the gas turbine system via the injector.
Abstract translation: 一种系统包括具有涡轮机，燃烧器和具有进气口的压缩机的燃气轮机系统。 进气口配置成向压缩机提供空气流。 该系统还包括具有流体清洗系统的流体注入系统，流体清洗系统构造成经由进气口将洗涤流体喷射到燃气涡轮机系统中。 流体洗涤系统包括配置成将洗涤流体注入到燃气涡轮机系统中的喷射器以及被配置为经由进气口将防冰流体喷射到燃气涡轮机系统中的防冰系统。 防冰系统被配置为经由喷射器将防冰流体喷射到燃气轮机系统中。
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公开(公告)号：US20150033698A1
公开(公告)日：2015-02-05
申请号：US13956201
申请日：2013-07-31
Applicant: General Electric Company
Inventor： Jose Antonio Cuevas , Tho Nguyen , Horacio Solis
IPC: F02C7/30
CPC classification number: F02C7/30 , F01D25/002 , F01D25/02 , Y02E20/16 , Y02E20/18
Abstract: A system includes a gas turbine system that has a turbine, a combustor, and a compressor having an air intake. The air intake is configured to supply an air flow to the compressor. The system also includes a fluid injection system that has a fluid wash system configured to inject a wash fluid into the gas turbine system via the air intake. The fluid wash system includes an injector configured to inject the wash fluid into the gas turbine system and an anti-icing system configured to inject an anti-icing fluid into the gas turbine system via the air intake. The anti-icing system is configured to inject the anti-icing fluid into the gas turbine system via the injector.
Abstract translation: 一种系统包括具有涡轮机，燃烧器和具有进气口的压缩机的燃气轮机系统。 进气口配置成向压缩机提供空气流。 该系统还包括具有流体清洗系统的流体注入系统，流体清洗系统构造成经由进气口将洗涤流体喷射到燃气涡轮机系统中。 流体洗涤系统包括配置成将洗涤流体注入到燃气涡轮机系统中的喷射器以及被配置为经由进气口将防冰流体喷射到燃气涡轮机系统中的防冰系统。 防冰系统被配置为经由喷射器将防冰流体喷射到燃气轮机系统中。
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