Method and equipment for combustion of ammonia

    公开(公告)号:US10767556B2

    公开(公告)日:2020-09-08

    申请号:US15999280

    申请日:2017-02-10

    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.

    NATURAL GAS COMBINED POWER GENERATION PROCESS WITH ZERO CARBON EMISSION

    公开(公告)号:US20200141282A1

    公开(公告)日:2020-05-07

    申请号:US16555152

    申请日:2019-08-29

    IPC分类号: F01K23/08 F02C6/04 H02K7/18

    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.

    FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

    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

    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.

    Systems and methods of droop response control of turbines
    100.
    发明授权
    Systems and methods of droop response control of turbines 有权
    涡轮机下垂响应控制的系统和方法

    公开(公告)号:US09562479B2

    公开(公告)日:2017-02-07

    申请号:US13801498

    申请日:2013-03-13

    IPC分类号: F02C9/00 F02C6/04 F02C9/28

    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。