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1. 发明授权

US09541197B2 Seal system and method of manufacture 有权
标题翻译：密封系统和制造方法
公开(公告)号：US09541197B2
公开(公告)日：2017-01-10
申请号：US13151205
申请日：2011-06-01
申请人： Gerardo Plata Contreras , Douglas Alan Jones , Sofia Cayón Aguilar
发明人： Gerardo Plata Contreras , Douglas Alan Jones , Sofia Cayón Aguilar
IPC分类号： F28F7/00 , F16J3/04 , F16J15/52 , B29C43/20
CPC分类号： F16J3/041 , B29C43/203 , F16J15/52
摘要： A system including a seal is provided. The seal includes a first layer made of a first non-metallic, elastic material. The seal further includes a second layer made of a second non-metallic, heat resistant material. The second layer is configured to thermally protect the first layer from heat. The seal is configured to extend across a gap between first and second surfaces, and the first and second layers are formed into a bended structure configured to expand and contract in response to a dimensional change in the gap.
摘要翻译：提供包括密封件的系统。密封件包括由第一非金属弹性材料制成的第一层。密封件还包括由第二非金属的耐热材料制成的第二层。第二层被配置为热保护第一层免受热。密封件构造成延伸穿过第一和第二表面之间的间隙，并且第一和第二层形成为弯曲结构，其构造成响应于间隙中的尺寸变化而膨胀和收缩。

2. 发明授权

US08899008B2 System and method for heat recovery in a gas turbine engine 有权
标题翻译：燃气轮机发动机热回收系统及方法
公开(公告)号：US08899008B2
公开(公告)日：2014-12-02
申请号：US13471926
申请日：2012-05-15
申请人： Douglas Alan Jones , Gerardo Plata Contreras , Robert Allen Baten , Victor Gerardo Cabal Velarde , Jingmei Zhang , Jesus Elios Almendarez Mendez , Richard Michael Watkins
发明人： Douglas Alan Jones , Gerardo Plata Contreras , Robert Allen Baten , Victor Gerardo Cabal Velarde , Jingmei Zhang , Jesus Elios Almendarez Mendez , Richard Michael Watkins
IPC分类号： F02C7/047 , F02C7/08 , F02C7/057
CPC分类号： F02C7/047 , F01D25/02 , F02C7/057 , F02C7/08 , F05D2260/213 , F05D2260/95 , F05D2270/03 , F05D2270/11 , F05D2270/303
摘要： A system includes an anti-icing heat recovery system, which includes a first heat exchanger, a second heat exchanger, and a variable speed fan. The first heat exchanger is configured to receive a working fluid from an exhaust section of a gas turbine engine and to transfer heat from the working fluid to a cooled intermediate heat transfer medium to generate a heated intermediate heat transfer medium. The second heat exchanger is configured to receive the heated intermediate heat transfer medium from the first heat exchanger and to transfer heat from the heated intermediate heat transfer medium to air entering the gas turbine engine. The variable speed fan is configured to urge the working fluid from the exhaust section of the gas turbine engine through the first heat exchanger.
摘要翻译：一种系统包括防冰热回收系统，其包括第一热交换器，第二热交换器和变速风扇。第一热交换器被配置为从燃气涡轮发动机的排气部分接收工作流体并将热量从工作流体传递到冷却的中间传热介质以产生加热的中间传热介质。第二热交换器构造成从第一热交换器接收加热的中间传热介质，并将热量从加热的中间传热介质传递到进入燃气涡轮发动机的空气。变速风扇构造成通过第一热交换器促使来自燃气涡轮发动机的排气部的工作流体。

3. 发明授权

US08813503B2 Gas turbine control systems and methods 有权
标题翻译：燃气轮机控制系统及方法
公开(公告)号：US08813503B2
公开(公告)日：2014-08-26
申请号：US13523857
申请日：2012-06-14
申请人： Douglas Alan Jones
发明人： Douglas Alan Jones
IPC分类号： F02K1/00
CPC分类号： F02C7/143 , F05D2260/211 , F05D2270/311 , F05D2270/313 , Y02E20/16 , Y02E20/18
摘要： Methods and systems for controlling a gas turbine system are provided herein. In one embodiment, a method includes the steps of receiving at least one parameter of turbine inlet air and determining, based on the at least one parameter, an expected condensation level at an intercooler disposed downstream of an inlet air chilling system and in-line between a low pressure compressor and a high pressure compressor. The method further includes determining a desired temperature of the turbine inlet air corresponding to substantially no expected condensation at the intercooler and controlling the inlet air chilling system to chill the turbine inlet air to the desired temperature.
摘要翻译：本文提供了用于控制燃气轮机系统的方法和系统。在一个实施例中，一种方法包括以下步骤：接收涡轮机入口空气的至少一个参数，并且基于所述至少一个参数确定设置在入口空气冷却系统下游的中间冷却器的预期冷凝水平，并且在低压压缩机和高压压缩机。该方法还包括确定对应于中间冷却器基本上不期望冷凝的涡轮机入口空气的期望温度，并且控制入口空气冷却系统将涡轮机入口空气冷却至所需温度。

4. 发明申请

US20130333393A1 GAS TURBINE CONTROL SYSTEMS AND METHODS 有权
标题翻译：气体涡轮控制系统及方法
公开(公告)号：US20130333393A1
公开(公告)日：2013-12-19
申请号：US13523857
申请日：2012-06-14
申请人： Douglas Alan Jones
发明人： Douglas Alan Jones
IPC分类号： F02C7/143 , F01D1/04 , F02C3/06 , F01D25/12
CPC分类号： F02C7/143 , F05D2260/211 , F05D2270/311 , F05D2270/313 , Y02E20/16 , Y02E20/18
摘要： Methods and systems for controlling a gas turbine system are provided herein. In one embodiment, a method includes the steps of receiving at least one parameter of turbine inlet air and determining, based on the at least one parameter, an expected condensation level at an intercooler disposed downstream of an inlet air chilling system and in-line between a low pressure compressor and a high pressure compressor. The method further includes determining a desired temperature of the turbine inlet air corresponding to substantially no expected condensation at the intercooler and controlling the inlet air chilling system to chill the turbine inlet air to the desired temperature.
摘要翻译：本文提供了用于控制燃气轮机系统的方法和系统。在一个实施例中，一种方法包括以下步骤：接收涡轮机入口空气的至少一个参数，并且基于所述至少一个参数确定设置在入口空气冷却系统下游的中间冷却器的预期冷凝水平，并且在低压压缩机和高压压缩机。该方法还包括确定对应于中间冷却器基本上不期望冷凝的涡轮机入口空气的期望温度，并且控制入口空气冷却系统将涡轮机入口空气冷却至所需温度。

5. 发明申请

US20130305737A1 SYSTEM AND METHOD FOR HEAT RECOVERY IN A GAS TURBINE ENGINE 有权
标题翻译：燃气轮机发动机热回收系统及方法
公开(公告)号：US20130305737A1
公开(公告)日：2013-11-21
申请号：US13471926
申请日：2012-05-15
申请人： Douglas Alan Jones , Gerardo Plata Contreras , Robert Allen Baten , Victor Gerardo Cabal Velarde , Jingmei Zhang , Jesus Elios Almendarez Mendez , Richard Michael Watkins
发明人： Douglas Alan Jones , Gerardo Plata Contreras , Robert Allen Baten , Victor Gerardo Cabal Velarde , Jingmei Zhang , Jesus Elios Almendarez Mendez , Richard Michael Watkins
IPC分类号： F02C7/047 , F02C7/00
CPC分类号： F02C7/047 , F01D25/02 , F02C7/057 , F02C7/08 , F05D2260/213 , F05D2260/95 , F05D2270/03 , F05D2270/11 , F05D2270/303
摘要： A system includes an anti-icing heat recovery system, which includes a first heat exchanger, a second heat exchanger, and a variable speed fan. The first heat exchanger is configured to receive a working fluid from an exhaust section of a gas turbine engine and to transfer heat from the working fluid to a cooled intermediate heat transfer medium to generate a heated intermediate heat transfer medium. The second heat exchanger is configured to receive the heated intermediate heat transfer medium from the first heat exchanger and to transfer heat from the heated intermediate heat transfer medium to air entering the gas turbine engine. The variable speed fan is configured to urge the working fluid from the exhaust section of the gas turbine engine through the first heat exchanger.
摘要翻译：一种系统包括防冰热回收系统，其包括第一热交换器，第二热交换器和变速风扇。第一热交换器被配置为从燃气涡轮发动机的排气部分接收工作流体并将热量从工作流体传递到冷却的中间传热介质以产生加热的中间传热介质。第二热交换器构造成从第一热交换器接收加热的中间传热介质，并将热量从加热的中间传热介质传递到进入燃气涡轮发动机的空气。变速风扇构造成通过第一热交换器促使来自燃气涡轮发动机的排气部的工作流体。

6. 发明申请

US20120306164A1 SEAL SYSTEM AND METHOD OF MANUFACTURE 有权
标题翻译：密封系统及其制造方法
公开(公告)号：US20120306164A1
公开(公告)日：2012-12-06
申请号：US13151205
申请日：2011-06-01
申请人： Gerardo Plata Contreras , Douglas Alan Jones , Sofia Cayón Aguilar
发明人： Gerardo Plata Contreras , Douglas Alan Jones , Sofia Cayón Aguilar
IPC分类号： F01D11/00 , B29C43/20 , F16J15/52
CPC分类号： F16J3/041 , B29C43/203 , F16J15/52
摘要： A system including a seal is provided. The seal includes a first layer made of a first non-metallic, elastic material. The seal further includes a second layer made of a second non-metallic, heat resistant material. The second layer is configured to thermally protect the first layer from heat. The seal is configured to extend across a gap between first and second surfaces, and the first and second layers are formed into a bended structure configured to expand and contract in response to a dimensional change in the gap.
摘要翻译：提供包括密封件的系统。密封件包括由第一非金属弹性材料制成的第一层。密封件还包括由第二非金属的耐热材料制成的第二层。第二层被配置为热保护第一层免受热。密封件构造成延伸穿过第一和第二表面之间的间隙，并且第一和第二层形成为弯曲结构，其构造成响应于间隙中的尺寸变化而膨胀和收缩。

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