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公开(公告)号：US20180266323A1
公开(公告)日：2018-09-20
申请号：US15463902
申请日：2017-03-20
发明人： Hua ZHANG , Naveen Ghattadhahalli PARMESHWAR , Christopher Conrad FRESE , Valery Ivanovich PONYAVIN , Bradly Aaron KIPPEL
CPC分类号： F02C7/057 , F02C7/055 , F05D2260/207 , F05D2260/80 , F05D2270/303 , F05D2270/311 , F28C3/08 , F28D2021/0026 , F28F25/087 , F28F27/00
摘要： The present application provides a method of evaluating media effectiveness in a gas turbine engine. The method may include the steps of receiving a baseline media effectiveness rating, receiving a media replacement cost, receiving a number of operating parameters from a number of sensors, based at least in part on the operating parameters and the baseline media effectiveness rating, determining a media effectiveness model, based at least in part of the media effectiveness model, determining a loss in evaporative benefit cost over time, determining a time t when the loss in evaporative benefit cost exceeds the media replacement cost, and scheduling media replacement at time t.
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公开(公告)号：US20180266319A1
公开(公告)日：2018-09-20
申请号：US15463624
申请日：2017-03-20
发明人： Valery Ivanovich PONYAVIN , Naveen Ghattadhahalli Parmeshwar , Christopher Conard Frese , Hua Zhang , Bradly Aaron Kippel
CPC分类号： F02C7/055
摘要： The present application provides a gas turbine engine. The gas turbine engine may include a compressor, an inlet filter house positioned upstream of the compressor, and one or more inlet water separator pads positioned within the inlet filter house. The one or more inlet water separator pads may include a synthetic liquid-gas separator media.
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公开(公告)号：US20170292456A1
公开(公告)日：2017-10-12
申请号：US15096922
申请日：2016-04-12
发明人： Laxmikant MERCHANT , Hua ZHANG , Dinesh VENUGOPAL SETTY , Valery Ivanovich PONYAVIN , James den Outer
CPC分类号： F02C9/18 , F01D9/02 , F02C7/045 , F02C7/047 , F05D2220/32 , F05D2260/96 , F05D2270/101
摘要： An inlet system for a gas turbine includes an integrated inlet bleed heat system, wherein the inlet bleed design is integrated in, e.g., a silencer or inlet.
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公开(公告)号：US20180266321A1
公开(公告)日：2018-09-20
申请号：US15463885
申请日：2017-03-20
发明人： Christopher Conrad FRESE , Naveen Ghattadhahalli PARMESHWAR , Hua ZHANG , Valery Ivanovich PONYAVIN , Bradly Aaron KIPPEL
CPC分类号： F02C7/1435 , F02C7/04 , F02C7/05 , F02C7/143 , F04D29/5826 , F05D2220/32 , F05D2250/61 , F05D2260/232 , F05D2300/614
摘要： The present application provides an inlet air system for cooling an inlet air flow to a compressor of a gas turbine engine. The inlet air system may include a wetted media pad and a drift eliminator positioned downstream of the wetted media pad with an air gap therebetween. The drift eliminator may include a fibrous media pad.
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公开(公告)号：US20170276386A1
公开(公告)日：2017-09-28
申请号：US15082825
申请日：2016-03-28
CPC分类号： F24F6/04 , F02C7/1435 , F24F5/0035 , F24F13/20
摘要： Synthetic media pads configured to be arranged in a stack of an evaporative cooler for a gas turbine, wherein the synthetic media pads include high density synthetic media pads and low density synthetic media pads. The sides of the pads may have surface patterns, such as grooves and ridges, to provide support for the pads.
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6.发明申请INLET BLEED HEAT SYSTEM AND RELATED METHOD FOR A COMPACT GAS TURBINE INLET 有权进气排气系统及相关方法用于紧凑型气体涡轮进口公开(公告)号：US20150068217A1
公开(公告)日：2015-03-12
申请号：US14019791
申请日：2013-09-06
摘要： An inlet system for a gas turbine includes an inlet air duct; a silencer disposed in the inlet air duct, the silencer including a plurality of panels with spaces between the panels; and a conduit with orifices disposed to inject inlet bleed heat into each of the spaces. A method of conditioning inlet air for a gas turbine includes flowing air through spaces between panels of a silencer in an inlet air duct of the gas turbine, and injecting inlet bleed heat through orifices and into each of the spaces.
摘要翻译： 用于燃气轮机的入口系统包括入口空气管道; 设置在所述入口空气管道中的消音器，所述消声器包括在所述面板之间具有空间的多个面板; 以及设置有用于将入口放气热量注入每个空间的孔口的导管。 调节用于燃气轮机的入口空气的方法包括使空气通过燃气轮机的入口空气管道中的消声器的面板之间的空间，以及通过孔口将入口排出热量并进入每个空间。
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