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Gas turbine engine driven auxiliary electric power unit with turbine speed controlled in response to generator output current

机译:燃气涡轮发动机驱动的辅助电力装置,其涡轮速度根据发电机输出电流进行控制

摘要

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).
机译:燃气涡轮发动机驱动的辅助电力单元,其包括涡轮机(9),向涡轮机供应压缩空气并由涡轮机驱动的空气压缩机(7),向涡轮机供应气态燃料的燃料供应装置(2),由涡轮驱动的发电机(10),用于产生电力输出,该电力被馈送到主用户电源(14),用于监测涡轮轴速的第一检测装置(15),用于监测输出功率的第二检测装置(19)在发电机的第一调节装置(16、18、13)中,该第一调节装置(16、18、13)通过控制从发电机到主用电用户的电流来调节涡轮轴的转速,使其与预定的轴转速(17)一致,以及第二调节装置(20、22、23)用于调节从燃料供应装置提供给涡轮机的气态燃料的流量,以使所监测的输出功率与预定的输出功率(21)相一致。

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