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公开(公告)号:US10767556B2
公开(公告)日:2020-09-08
申请号:US15999280
申请日:2017-02-10
发明人: Ghenadie Bulat , Timothy Hughes , Jonathan May , Ian Wilkinson
IPC分类号: F02C3/24 , F23C9/06 , F23C6/04 , F02C3/20 , F02C3/34 , F01K23/10 , F01K23/18 , F02C3/22 , F02C6/04
摘要: A method for the combustion of ammonia, wherein a first combustion chamber receives ammonia and hydrogen in controlled proportions, and an oxygen-containing gas. Combustion of the ammonia and hydrogen produces NH2 ions among other combustion products. A second combustion chamber receives the combustion products from the first combustion chamber and receives further ammonia and further hydrogen in controlled proportions, wherein combustion produces nitrogen oxides among other combustion products. A third combustion chamber receives the nitrogen oxides along with further ammonia and further hydrogen in further controlled proportions along with further oxygen-containing gas, such that the nitrogen oxides are combusted into nitrogen and water.
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公开(公告)号:US20200141282A1
公开(公告)日:2020-05-07
申请号:US16555152
申请日:2019-08-29
发明人: Yingyun Qiao , Yuanyu Tian , Kechang Xie , Lanyi Sun , Rui Liu , Lichao Hu , Ze Yang
摘要: The present disclosure relates to the technical field of natural gas power generation, and particularly discloses a natural gas combined power generation process with zero carbon emission, the process comprising: introducing the pressurized air into an air separation facility to obtain liquid oxygen and liquid nitrogen, wherein the liquid oxygen is used for gasification and power generation, the liquid nitrogen is applied as the coolant of flue gas, and then used for the gasification and power generation; the liquid nitrogen and a part of liquid oxygen stored during the valley period with low electricity load are provided for use during the peak period with high electricity load; the natural gas, oxygen and the recyclable CO2 jointly enter a combustion gas turbine for burning to drive an air compressor and a generator to rotate at a high speed, the air compressor compresses the air to a pressure of 0.4˜0.8 MPa, the generator generates electricity; the high-temperature combustion flue gas performs the supercritical CO2 power generation, its coolant is liquid oxygen; the moderate temperature flue gas then exchanges heat with liquid nitrogen, the liquid nitrogen vaporizes for power generation, the cooled flue gas is dehydrated and subjects to distillation and separation to obtain the recovered CO2, a part of the CO2 can be returned for circulation and temperature control, another part of the CO2 may be used for replenishment of work medium for supercritical CO2 power generation, and the remaining part of CO2 may be sold outward as liquid CO2 product. During the peak period with high electricity load, the liquid nitrogen stored during the valley period with low electricity load and separated during the peak period is pumped and pressurized and then subjects to heat exchange and vaporization for power generation. The power generation process provided by the present disclosure not only solves the difficult problems in the existing natural gas combined power generation technology such as high water consumption, low power generation efficiency and small range of peak load adjustment capacity; but also can compress air with high unit volume for energy storage with a high conversion efficiency, and greatly reduce load of the air compressor, thereby perform CO2 capture and utilization with low cost, zero NOx emission and discharging fuel gas at a normal temperature, and significantly improve the power generation efficiency.
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公开(公告)号:US20200023987A1
公开(公告)日:2020-01-23
申请号:US16221383
申请日:2018-12-14
申请人: JETOPTERA, INC.
发明人: Andrei Evulet
IPC分类号: B64D33/04 , B64C39/02 , B64C15/14 , B64C9/38 , B64C15/00 , B64C21/00 , B64D27/10 , B64C21/04 , B64D27/18 , B64D29/02 , B64D33/02 , F02K1/36 , F02K1/00 , F02C3/04 , F02C6/04
摘要: A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore conduit. At least one tail ejector is fluidly coupled to the at least one tail conduit. The fore ejectors respectively include an outlet structure out of which gas from the at least one fore conduit flows. The at least one tail ejector includes an outlet structure out of which gas from the at least one tail conduit flows. First and second primary airfoil elements have leading edges respectively located directly downstream of the first and second fore ejectors. At least one secondary airfoil element has a leading edge located directly downstream of the outlet structure of the at least one tail ejector.
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公开(公告)号:US10012146B2
公开(公告)日:2018-07-03
申请号:US14623152
申请日:2015-02-16
发明人: Olivier Pelagatti , Thomas Deguin , Ronan Bodet
CPC分类号: F02C6/08 , B64D13/02 , B64D13/04 , B64D2013/0644 , B64D2013/0648 , F02C3/10 , F02C6/04 , F02C6/06 , F02C9/18 , F02K3/115 , Y02T50/56
摘要: A turbojet comprising a low-pressure compressor, a high-pressure compressor and a bleeding system configured to bleed air in the turbojet and to deliver the air to an air system. The bleeding system comprises a first air intake configured to bleed air at low pressure, a second air intake configured to bleed air at high pressure, a first valve and a second valve having inlets connected to the first air intake, a compressor having an inlet connected to an outlet of the second valve, a high-pressure valve connected to the second air intake, a control valve connected to the air system, and a controller to control opening and closing of the valves depending on a pressure at the first air intake.
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公开(公告)号:US09915201B2
公开(公告)日:2018-03-13
申请号:US14140959
申请日:2013-12-26
IPC分类号: F02C6/16 , F02C7/045 , F02C3/13 , F02C6/14 , F02C7/27 , F02K3/12 , F02C3/30 , F02C6/08 , F02C6/04 , F02C9/18 , F02C7/262 , F02C9/52 , F02C1/02 , F02C6/06 , F02C7/26 , F02C9/50
CPC分类号: F02C7/045 , F02C1/02 , F02C3/13 , F02C3/305 , F02C6/04 , F02C6/06 , F02C6/08 , F02C6/14 , F02C6/16 , F02C7/26 , F02C7/262 , F02C7/27 , F02C9/18 , F02C9/50 , F02C9/52 , F02K3/12 , F05B2260/42 , F05B2270/103 , F05B2270/1031 , F05B2270/1033 , F05B2270/1073 , F05B2270/111 , F05D2260/42 , F05D2260/963 , F05D2270/05 , F05D2270/051 , F05D2270/093 , F05D2270/13 , F05D2270/3061
摘要: A gas turbine engine is disclosed which includes a bypass passage that in some embodiments are capable of being configured to act as a resonance space. The resonance space can be used to attenuate/accentuate/etc a noise produced elsewhere. The bypass passage can be configured in a number of ways to form the resonance space. For example, the space can have any variety of geometries, configurations, etc. In one non-limiting form the resonance space can attenuate a noise forward of the bypass duct. In another non-limiting form the resonance space can attenuate a noise aft of the bypass duct. Any number of variations is possible.
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公开(公告)号:US20180038280A1
公开(公告)日:2018-02-08
申请号:US15667873
申请日:2017-08-03
IPC分类号: F02C7/14 , F02C3/04 , F02C7/22 , B64D15/02 , F02C6/04 , B64D27/10 , B64D33/02 , F01D25/24 , F02C7/047
CPC分类号: F02C7/14 , B64D15/02 , B64D27/10 , B64D33/02 , F01D25/02 , F01D25/24 , F02C3/04 , F02C6/04 , F02C7/047 , F02C7/222 , F02C7/224 , F02C9/18 , F05D2220/323 , F05D2260/205 , F05D2260/213 , Y02T50/671 , Y02T50/675
摘要: A dual-flow turbomachine including a nacelle, compressors, turbines, a fuel supply line, a transfer line, a de-icing circuit, and a heat management system having: a first heat exchanger providing an exchange of heat between fuel in the supply line and oil in the transfer line, a loop comprising a main line and a pump which circulates a heat transfer fluid in the main line, where the main line is connected to an outlet of the pump and enters an inlet of a third heat exchanger, where at the outlet of the third heat exchanger the main line meets an inlet of the de-icing circuit, where at the outlet of the de-icing circuit the main line meets the inlet of the pump, and where the third heat exchanger transfers heat between the heat transfer fluid of the main line and the oil of the transfer line.
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公开(公告)号:US09803546B2
公开(公告)日:2017-10-31
申请号:US14068447
申请日:2013-10-31
申请人: The Boeing Company
IPC分类号: B64D13/02 , F02C7/04 , F02C7/141 , F04D29/58 , F02C7/18 , F02C6/08 , B64D13/06 , F02C6/04 , B64D33/02
CPC分类号: F02C7/04 , B64D13/02 , B64D13/06 , B64D2033/024 , B64D2241/00 , F02C6/04 , F02C6/08 , F02C7/141 , F02C7/18 , F02C7/185 , F04D29/584 , F05D2250/51 , Y02T50/675 , Y10T137/0536
摘要: A method and apparatus for supplying air to a precooler. Air flow is created through a fan duct in an engine system. A first portion of the air flow is directed into a first inlet of an inlet system to feed a first half of the precooler. A second portion of the air flow is directed through the fan duct into a second inlet of the inlet system to feed a second half of the precooler.
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公开(公告)号:US09790816B1
公开(公告)日:2017-10-17
申请号:US15483225
申请日:2017-04-10
申请人: Masoud Darvishian
发明人: Masoud Darvishian
CPC分类号: F01K25/08 , F01B17/00 , F01B17/02 , F01B17/022 , F01B29/10 , F01K7/00 , F01K27/00 , F01K27/005 , F02C1/04 , F02C6/00 , F02C6/04 , F02C6/06
摘要: This invention presents a method for conversion of heat to electrical power through absorption of heat from any types of fluids with temperatures both higher and lower than 0° C. Heat can be absorbed from fossil or renewable energy resources. The mechanism in this invention uses fluid internal energy and enthalpy difference to generate power, where a reciprocating piston-cylinder system provides the required force to rotate a turbine for power generation.
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公开(公告)号:US20170260902A1
公开(公告)日:2017-09-14
申请号:US15609799
申请日:2017-05-31
发明人: Yukimasa NAKAMOTO , Kazunori FUJITA
IPC分类号: F02C6/04 , F01K13/02 , F01K23/10 , F02C3/20 , F02C3/30 , F02C6/00 , F02C6/18 , H01M8/04082 , H01M8/04111 , H01M8/124
CPC分类号: F02C6/04 , F01K13/02 , F01K23/10 , F02C3/20 , F02C3/30 , F02C6/00 , F02C6/18 , H01M8/04111 , H01M8/04201 , H01M2008/1293 , H01M2250/402 , Y02B90/12 , Y02E20/16
摘要: This power generation system is provided with: a gas turbine having a compressor, a combustor and a turbine; a first compressed air supply line that supplies compressed air, which has been compressed by the compressor, to the combustor; a solid oxide fuel cell (SOFC) having an air electrode and a fuel electrode; a compressed air supply device capable of generating compressed air; and a second compressed air supply line that supplies compressed air, which has been compressed by the compressed air supply device to the SOFC. The fuel cell can thus be stably operated regardless of the operating state of the gas turbine.
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公开(公告)号:US09562479B2
公开(公告)日:2017-02-07
申请号:US13801498
申请日:2013-03-13
发明人: Yuhui Chen , John Dalton Warren
CPC分类号: F02C9/00 , F02C9/28 , F05D2270/02 , F05D2270/061
摘要: A system includes a controller configured to control an operational behavior of a turbine system. The controller includes a droop response system configured to detect one or more operational characteristics of the turbine system as an indication of a frequency variation of an electric power system associated with the turbine system. The droop response system is further configured to generate a response to vary an output of the turbine system in response to the indication of the frequency variation. The controller includes a multivariable droop response correction system configured to determine one or more possible errors associated with the one or more operational characteristics of the turbine system, and to generate a plurality of correction factors to apply to the response generated by the droop response system. The plurality of correction factors is configured to correct the response generated by the droop response system.
摘要翻译: 系统包括被配置为控制涡轮机系统的操作特性的控制器。 控制器包括下垂响应系统,其被配置为检测涡轮机系统的一个或多个操作特性,作为与涡轮机系统相关联的电力系统的频率变化的指示。 下垂响应系统还被配置为响应于频率变化的指示而产生响应以改变涡轮机系统的输出。 控制器包括多变量下垂响应校正系统,其被配置为确定与涡轮机系统的一个或多个操作特性相关联的一个或多个可能误差,并且生成多个校正因子以应用于由下垂响应系统产生的响应。 多个校正因子被配置为校正由下垂响应系统产生的响应。
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