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    • 2. 发明授权
    • Gas turbine cogeneration apparatus for the production of domestic heat
and power
    • 用于生产国内热能和动力的燃气轮机加热装置
    • US5148670A
    • 1992-09-22
    • US727381
    • 1991-07-05
    • Peter H. BirchToshiyuki KondoKatsuhiro Mori
    • Peter H. BirchToshiyuki KondoKatsuhiro Mori
    • F02C3/00F02C6/00F02C6/04F02C6/18F02C7/08F02C7/26
    • F02C6/006F02C7/08F02C7/26Y02E20/14
    • An apparatus for the domestic cogeneration of heat and electrical energy utilizing an inverted Brayton cycle gas turbine, a combustion chamber, an electrical generator and a compressor. Combustion air is preheated in a heat exchanger by gaseous combustion gases or exhaust gases exiting from the turbine. The combustion air is supplied at substantially atmospheric pressure to the combustion chamber where fuel is burned. The cooled gaseous combustion gases exiting from the heat exchanger are then fed to the compressor where they are recompressed to atmospheric pressure, and are finally used to heat the working fluid of a domestic heating system before being exhausted to the atmosphere. The apparatus can also include an acoustically and thermally insulated housing, an electric air blower for start-up, an engine ignition device, a frequency converter which conditions the electric generator output for connection to the main supply and a control system which is cooled by the engine intake air and which detects thermal and electrical demand and adjusts the engine power accordingly.
    • 一种利用倒置布雷顿循环燃气轮机,燃烧室,发电机和压缩机进行国内热电联产的装置。 燃烧空气在热交换器中由气体燃烧气体或从涡轮机排出的排气预热。 燃烧空气以基本大气压供应到燃烧燃烧的燃烧室。 然后将从热交换器排出的冷却的气态燃烧气体送入压缩机,在压缩机中将其再次压缩至大气压力,最后用于在排气到大气之前加热家用加热系统的工作流体。 该装置还可以包括隔热隔热的壳体,用于启动的电动鼓风机,发动机点火装置,调节用于连接主电源的发电机输出的变频器和由主电源冷却的控制系统 发动机进气,并检测热和电力需求,并相应地调整发动机功率。
    • 5. 发明授权
    • Gas turbine engine driven auxiliary electric power unit with turbine
speed controlled in response to generator output current
    • 燃气涡轮发动机驱动的辅助电力单元,其响应于发电机输出电流而控制涡轮速度
    • US5635768A
    • 1997-06-03
    • US430373
    • 1995-04-28
    • Peter H. BirchTakeshi IkeyamaAnthony D. WearingMark G. Norton
    • Peter H. BirchTakeshi IkeyamaAnthony D. WearingMark G. Norton
    • F02C9/28F02C9/40H02P9/04H02P9/48F02C9/56
    • H02P9/04H02P9/48F05B2270/1033
    • A gas turbine engine driven auxiliary electric power unit which includes a turbine (9), an air compressor (7) for supplying compressed air to the turbine and driven by the turbine, fuel supplying means (2) for supplying gaseous fuel to the turbine, a generator (10) driven by the turbine for generating electrical output power which is fed to a main electric user supply (14), first detecting means (15) for monitoring turbine shaft speed, second detecting means (19) for monitoring the output power of the generator, first modulating means (16,18,13) for modulating the turbine shaft speed to cause it to coincide with a predetermined shaft speed (17) by means of controlling current flow from the generator to the main electric user supply, and second modulating means (20,22,23) for modulating the flow of gaseous fuel which is supplied from the fuel supplying means to the turbine so as to cause the monitored output power to coincide with a predetermined output power (21).
    • 一种燃气涡轮发动机驱动的辅助电力单元,包括涡轮机(9),用于向涡轮机供应压缩空气并由涡轮机驱动的空气压缩机(7),用于向涡轮机供应气体燃料的燃料供应装置(2) 由涡轮机驱动的发电机(10),用于产生供给主电用户供应装置(14)的电力输出功率;第一检测装置(15),用于监测涡轮轴转速;第二检测装置(19),用于监测输出功率 ,用于通过控制从所述发电机到所述主用户电源的电流来调制所述涡轮机轴速度以使其与预定轴速度(17)一致的第一调制装置(16,18,13),以及 第二调制装置(20,22,23),用于调节从燃料供应装置供应到涡轮机的气体燃料的流量,以使监测的输出功率与预定的输出功率一致。