-
公开(公告)号：US09470149B2
公开(公告)日：2016-10-18
申请号：US12332383
申请日：2008-12-11
申请人： Abbas Motakef , Peter Feher
发明人： Abbas Motakef , Peter Feher
摘要： A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor.
摘要翻译： 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括热能储存箱充电回路，与热能存储充电回路连通的冷却回路，以及与冷却回路和涡轮压缩机的入口空气连通的加热回路。
-
公开(公告)号：US08468830B2
公开(公告)日：2013-06-25
申请号：US12332380
申请日：2008-12-11
申请人： Abbas Motakef , Peter Feher
发明人： Abbas Motakef , Peter Feher
CPC分类号： F02C7/143 , F02C6/14 , F05D2260/20
摘要： A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a fluid coil positioned about the turbine compressor and a thermal energy storage tank. The fluid coil and the thermal energy storage tank are in fluid communication such that fluid is both provided to the fluid coil from the thermal energy storage tank for exchanging heat with the inlet air and returned to the thermal energy storage tank without further heat exchange.
摘要翻译： 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕涡轮压缩机和热能储存器定位的流体盘管。 流体盘管和热能储存罐是流体连通的，使得流体都从热能储存罐提供给流体盘管，用于与入口空气进行热交换并返回到热能储存罐而不需要进一步的热交换。
-
公开(公告)号：US20100146976A1
公开(公告)日：2010-06-17
申请号：US12332380
申请日：2008-12-11
申请人： Abbas Motakef , Peter Feher
发明人： Abbas Motakef , Peter Feher
CPC分类号： F02C7/143 , F02C6/14 , F05D2260/20
摘要： A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a fluid coil positioned about the turbine compressor and a thermal energy storage tank. The fluid coil and the thermal energy storage tank are in fluid communication such that fluid is both provided to the fluid coil from the thermal energy storage tank for exchanging heat with the inlet air and returned to the thermal energy storage tank without further heat exchange.
摘要翻译： 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕涡轮压缩机和热能储存器定位的流体盘管。 流体盘管和热能储存罐是流体连通的，使得流体都从热能储存罐提供给流体盘管，用于与入口空气进行热交换并返回到热能储存罐而不需要进一步的热交换。
-
公开(公告)号：US20100146930A1
公开(公告)日：2010-06-17
申请号：US12332385
申请日：2008-12-11
申请人： Abbas Motakef , Peter Feher
发明人： Abbas Motakef , Peter Feher
摘要： A heating and cooling system for inlet air of a gas turbine engine in a combined cycle power plant having a steam turbine. The heating and cooling system may include a fluid coil positioned about the gas turbine engine, a heat exchanger in communication with the fluid coil, and a condenser in communication with the steam turbine and the heat exchanger such that waste heat from the steam turbine is forwarded to the fluid coil.
摘要翻译： 一种具有蒸汽涡轮机的联合循环发电厂中的燃气涡轮发动机的入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕燃气涡轮发动机定位的流体线圈，与流体线圈连通的热交换器以及与蒸汽轮机和热交换器连通的冷凝器，使得来自蒸汽涡轮机的废热被转发 到流体盘管。
-
公开(公告)号：US20100101209A1
公开(公告)日：2010-04-29
申请号：US12257731
申请日：2008-10-24
申请人： Peter Feher , Abbas Motakef
发明人： Peter Feher , Abbas Motakef
IPC分类号： F02K3/08
摘要： An embodiment of the present invention takes the form of an application and process that incorporates an external heat source to increase the temperature of the airstream entering a compressor section of a combustion turbine. An embodiment of the present invention may perform an anti-icing operation that may not require an Inlet Bleed Heat system (IBH) to operate. An embodiment of the present invention may perform an anti-icing operation that may allow for the IGV angle to remain nearly constant. An embodiment of the present invention may increase the output and efficiency of a combustion turbine operating at partload by delaying IBH operation and delaying the closing IGVs.
摘要翻译： 本发明的实施例采用包含外部热源以增加进入燃气轮机的压缩机部分的气流的温度的应用和过程的形式。 本发明的一个实施例可以执行防冰操作，该操作可能不需要入口放热加热系统（IBH）的操作。 本发明的一个实施例可以执行防冰操作，其可以允许IGV角保持几乎恒定。 本发明的一个实施例可以通过延迟IBH操作并延迟关闭IGV来增加在部分负载下工作的燃气轮机的输出和效率。
-
公开(公告)号：US08266910B2
公开(公告)日：2012-09-18
申请号：US12257731
申请日：2008-10-24
申请人： Peter Feher , Abbas Motakef
发明人： Peter Feher , Abbas Motakef
IPC分类号： F02C1/00
摘要： An application and process that incorporates an external heat source to increase the temperature of the airstream entering a compressor section of a combustion turbine. The application and process may perform an anti-icing operation that may not require an Inlet Bleed Heat system (IBH) to operate. Additionally, the application and process may perform an anti-icing operation that may allow for the IGV angle to remain nearly constant. The application and process may increase the output and efficiency of a combustion turbine operating at partload by delaying IBH operation and delaying the closing IGVs.
摘要翻译： 包括外部热源以增加进入燃气轮机的压缩机部分的气流的温度的应用和过程。 应用程序和过程可以执行防冰操作，这可能不需要入口泄放热系统（IBH）的操作。 另外，应用和过程可以执行可以使IGV角度几乎保持恒定的防冰操作。 应用和过程可以通过延迟IBH操作和延迟闭合IGV来增加在部分负载下工作的燃气轮机的输出和效率。
-
公开(公告)号：US20100146978A1
公开(公告)日：2010-06-17
申请号：US12332378
申请日：2008-12-11
申请人： Peter Feher , Abbas Motakef
发明人： Peter Feher , Abbas Motakef
IPC分类号： F02C1/00
摘要： A control system for a base load output of a gas turbine engine. The control system may include an inlet chilling coil system for providing air to the gas turbine engine at a desired temperature, a temperature control valve in communication with the inlet chilling coil system, a temperature sensor positioned about the gas turbine engine, and a temperature controller in communication with the temperature control valve and the temperature sensor. The temperature controller modulates the temperature control valve until the air provided to the gas turbine engine by the inlet chilling coil system reaches the desired temperature as sensed by the temperature sensor.
摘要翻译： 一种用于燃气涡轮发动机的基本负载输出的控制系统。 控制系统可以包括用于在期望温度下向燃气涡轮发动机提供空气的入口冷却盘管系统，与入口冷却盘管系统连通的温度控制阀，围绕燃气涡轮发动机定位的温度传感器和温度控制器 与温度控制阀和温度传感器通信。 温度控制器调节温度控制阀，直到由入口冷却线圈系统提供给燃气涡轮发动机的空气达到温度传感器感测到的所需温度。
-
公开(公告)号：US20080098891A1
公开(公告)日：2008-05-01
申请号：US11552535
申请日：2006-10-25
申请人： Peter Feher , Abbas Motakef
发明人： Peter Feher , Abbas Motakef
IPC分类号： B01D47/00
CPC分类号： F02C7/052 , F02C3/30 , F02C7/04 , F05D2240/40 , F05D2250/132 , F05D2250/232
摘要： An inlet air treatment system. The inlet air treatment system includes a housing with more than two symmetric sides. Each of the sides includes a number of air filters and a number of spray arrays. A central air deflector is positioned within the housing.
摘要翻译： 进气处理系统。 入口空气处理系统包括具有多于两个对称侧的壳体。 每个侧面包括多个空气过滤器和多个喷射阵列。 中央空气导流板位于壳体内。
-
公开(公告)号：US08356466B2
公开(公告)日：2013-01-22
申请号：US12332385
申请日：2008-12-11
申请人： Abbas Motakef , Peter Feher
发明人： Abbas Motakef , Peter Feher
摘要： A heating and cooling system for inlet air of a gas turbine engine in a combined cycle power plant having a steam turbine. The heating and cooling system may include a fluid coil positioned about the gas turbine engine, a heat exchanger in communication with the fluid coil, and a condenser in communication with the steam turbine and the heat exchanger such that waste heat from the steam turbine is forwarded to the fluid coil.
摘要翻译： 一种具有蒸汽涡轮机的联合循环发电厂中的燃气涡轮发动机的入口空气的加热和冷却系统。 加热和冷却系统可以包括围绕燃气涡轮发动机定位的流体线圈，与流体线圈连通的热交换器以及与蒸汽轮机和热交换器连通的冷凝器，使得来自蒸汽涡轮机的废热被转发 到流体盘管。
-
公开(公告)号：US20100146981A1
公开(公告)日：2010-06-17
申请号：US12332383
申请日：2008-12-11
申请人： Abbas Motakef , Peter Feher
发明人： Abbas Motakef , Peter Feher
IPC分类号： F02C7/08
摘要： A heating and cooling system for inlet air of a turbine compressor. The heating and cooling system may include a thermal energy storage tank charging loop, a cooling loop in communication with the thermal energy storage charging loop, and a heating loop in communication with the cooling loop and the inlet air of the turbine compressor.
摘要翻译： 一种用于涡轮压缩机入口空气的加热和冷却系统。 加热和冷却系统可以包括热能储存箱充电回路，与热能存储充电回路连通的冷却回路，以及与冷却回路和涡轮压缩机的入口空气连通的加热回路。
-
-
-
-
-
-
-
-
-
搜索结果
24 条记录 (耗时 0.014 秒)
