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公开(公告)号：US08397484B2
公开(公告)日：2013-03-19
申请号：US13028498
申请日：2011-02-16
Applicant: Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
Inventor： Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
CPC classification number: F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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2.发明授权Method for adjusting the operation of a turbomachine receiving a recirculated exhaust gas 有权用于调节接收再循环废气的涡轮机的操作的方法公开(公告)号：US09410479B2
公开(公告)日：2016-08-09
申请号：US11959975
申请日：2007-12-19
Applicant: James A. West , Rex A. Morgan , Lewis B. Davis, Jr. , Sam D. Draper , Amit Toprani
Inventor： James A. West , Rex A. Morgan , Lewis B. Davis, Jr. , Sam D. Draper , Amit Toprani
CPC classification number: F02C3/34 , F01K23/101 , F02C9/16 , F05D2270/303 , Y02E20/16
Abstract: A method for adjusting the operation of a turbomachine integrated with an exhaust gas recirculation (EGR) system is provided. The method may utilize the composition of an inlet fluid entering the turbomachine. The method may also utilize a variety of turbomachine operating data.
Abstract translation: 提供了一种用于调节与废气再循环（EGR）系统集成的涡轮机的操作的方法。 该方法可以利用进入涡轮机的入口流体的组成。 该方法还可以利用各种涡轮机操作数据。
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公开(公告)号：US08443584B2
公开(公告)日：2013-05-21
申请号：US13028526
申请日：2011-02-16
Applicant: Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
Inventor： Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
CPC classification number: F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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4.发明申请公开(公告)号：US20090150056A1
公开(公告)日：2009-06-11
申请号：US11953556
申请日：2007-12-10
Applicant: Joell R. Hibshman, II , Sam D. Draper
Inventor： Joell R. Hibshman, II , Sam D. Draper
Abstract: A method and system for controlling an exhaust gas recirculation (EGR) system is provided. The EGR system recirculates a portion of an exhaust through an inlet portion of the turbomachine. The EGR system reduces the level of harmful constituents within the exhaust before the recirculation occurs.
Abstract translation: 提供了一种用于控制废气再循环（EGR）系统的方法和系统。 EGR系统使一部分排气通过涡轮机的入口部分再循环。 在再循环发生之前，EGR系统降低排气中有害成分的水平。
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公开(公告)号：US20100287943A1
公开(公告)日：2010-11-18
申请号：US12466184
申请日：2009-05-14
Applicant: Kevin Weston McMahan , Mark Allan Hadley , Geoffrey D. Myers , Sam D. Draper
Inventor： Kevin Weston McMahan , Mark Allan Hadley , Geoffrey D. Myers , Sam D. Draper
CPC classification number: F02C3/30 , F01D25/002 , F05D2260/607 , F23C15/00 , F23J3/00 , F23L7/002 , F23N1/002 , F23R3/28 , F23R2900/00004 , F23R2900/00013 , Y02E20/16 , Y02E20/328 , Y02T50/675
Abstract: Methods and systems are provided for inducing combustion dynamics within turbine engines to remove combustion deposits within the turbine engine during operation of the turbine engine.
Abstract translation: 提供的方法和系统用于在涡轮发动机的运行期间引起涡轮发动机内的燃烧动力学以去除涡轮发动机内的燃烧沉积物。
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Patent Agency Ranking
公开(公告)号：US20090178417A1
公开(公告)日：2009-07-16
申请号：US11971977
申请日：2008-01-10
Applicant: Sam D. Draper , Scott M. Hoyte , Eric Gebhardt , Erin K. Bauknight
Inventor： Sam D. Draper , Scott M. Hoyte , Eric Gebhardt , Erin K. Bauknight
CPC classification number: G01M15/14 , F05B2260/80 , F05D2260/80 , F05D2270/804
Abstract: A method of operating a turbine, the method including the steps of: 1) gathering measured creep data for a blade while the turbine operates at different operating temperatures, the measured creep data comprising at least a measured creep rate for the blade (wherein the different operating temperatures include at least a first operating temperature and a second operating temperature); and 2) given the measured creep data for the blade while the turbine operated at the first operating temperature and the measured creep data for the blade while the turbine operated at the second operating temperature, determining whether operating the turbine at the first operating temperature or the second operating temperature is more economically efficient.
Abstract translation: 一种运行涡轮机的方法，所述方法包括以下步骤：1）在涡轮机在不同的操作温度下运行时，收集测量到的叶片的蠕变数据，所测量的蠕变数据至少包括测量到的叶片的蠕变速率（其中不同的 工作温度至少包括第一工作温度和第二工作温度）; 和2）给出了在涡轮机在第一操作温度下操作的涡轮机的测量的蠕变数据，以及当涡轮机在第二操作温度下操作时测量的叶片的蠕变数据，确定在第一操作温度下操作涡轮机 第二工作温度更经济有效。
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公开(公告)号：US08720206B2
公开(公告)日：2014-05-13
申请号：US12466184
申请日：2009-05-14
Applicant: Kevin Weston McMahan , Mark Allan Hadley , Geoffrey D. Myers , Sam D. Draper
Inventor： Kevin Weston McMahan , Mark Allan Hadley , Geoffrey D. Myers , Sam D. Draper
IPC: F02C9/48
CPC classification number: F02C3/30 , F01D25/002 , F05D2260/607 , F23C15/00 , F23J3/00 , F23L7/002 , F23N1/002 , F23R3/28 , F23R2900/00004 , F23R2900/00013 , Y02E20/16 , Y02E20/328 , Y02T50/675
Abstract: Methods and systems are provided for inducing combustion dynamics within turbine engines to remove combustion deposits within the turbine engine during operation of the turbine engine.
Abstract translation: 提供的方法和系统用于在涡轮发动机的运行期间引起涡轮发动机内的燃烧动力学以去除涡轮发动机内的燃烧沉积物。
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公开(公告)号：US08402737B2
公开(公告)日：2013-03-26
申请号：US13028510
申请日：2011-02-16
Applicant: Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
Inventor： Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
CPC classification number: F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
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公开(公告)号：US08397483B2
公开(公告)日：2013-03-19
申请号：US13028490
申请日：2011-02-16
Applicant: Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
Inventor： Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
IPC: F02G5/02 , F02C7/052 , F02C7/055 , F02M35/024 , F02M25/07
CPC classification number: F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
Abstract translation: 本发明的一个实施例采用的系统的形式可以使至少一个涡轮机的排气的一部分再循环，在那里它可以与入口空气混合并重新进入涡轮机，而不会影响单元的可靠性和可用性。 本发明的实施例提供了一种用于废气再循环系统的入口系统。 该入口系统可以采取各种形式并且可优化再循环排气流的部分在入口系统内流动的方向。
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公开(公告)号：US20110131982A1
公开(公告)日：2011-06-09
申请号：US13028526
申请日：2011-02-16
Applicant: Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
Inventor： Sam D. Draper , Douglas S. Byrd , Carl G. Schott , Rahul J. Chillar , Amit S. Toprani
CPC classification number: F02C1/005 , F02C3/34 , F02C7/05 , F05D2270/08
Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit.An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.
Abstract translation: 本发明的一个实施例采用的系统的形式可以使至少一个涡轮机的排气的一部分再循环，在那里它可以与入口空气混合并重新进入涡轮机，而不会影响单元的可靠性和可用性。 本发明的实施例提供了一种用于废气再循环系统的入口系统。 该入口系统可以采取各种形式并且可优化再循环排气流的部分在入口系统内流动的方向。
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