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    • 4. 发明授权
    • Electrical power generator for a gas turbine engine
    • Stromgeneratorfüreinen Gasturbinenmotor
    • EP2910739B1
    • 2016-04-27
    • EP15152873.4
    • 2015-01-28
    • Rolls-Royce plc
    • Edwards, Huw Llewelyn
    • H02P9/00F01D15/10F02C9/28H02P9/04H02P9/48
    • H02P9/04F01D15/10F02C6/20F02C9/00F02C9/28F05D2220/323F05D2220/764F05D2220/7642F05D2220/7646F05D2270/01F05D2270/02F05D2270/061F05D2270/071F05D2270/304F05D2270/309F05D2270/332F05D2270/335H02P9/007H02P9/48
    • An electrical power generation system (100) for an aircraft gas turbine engine (10). The system comprises an alternating current electrical generator (110) having a rotor (114) comprising a plurality of electromagnetic rotor windings (118) and a stator (124) comprising a plurality of electrical stator windings (126). The rotor (114) is mechanically coupled to a shaft (36) of the gas turbine engine (10) by a transmission system (129). The electrical generator (110) further includes an electrical output frequency controller (130), a torque sensor arrangement configured to determine a torque imposed on the transmission system (129) by the generator (110) and a controller (112) configured to operate the electrical power generation system in first mode and second modes. In the first mode, the frequency of the electrical power output of the electrical generator (110) is controlled by the electrical output frequency controller (130) to lie within predetermined limits, and a reduced idle signal is provided to a gas turbine engine controller (132). In the second mode, the frequency of the electrical power output of the electrical generator (132) is not controlled by the electrical output frequency controller (130) and an increased idle signal is provided to the gas turbine engine controller (132). The electrical generator controller (112) is configured to operate the electrical power generation system (100) in the first mode when the torque is below a predetermined limit, and in the second mode when the torque is above a predetermined limit.
    • 一种用于飞机燃气涡轮发动机(10)的发电系统(100)。 该系统包括具有包括多个电磁转子绕组(118)和包括多个电定子绕组(126)的定子(124)的转子(114)的交流发电机(110)。 转子(114)通过传动系统(129)机械联接到燃气涡轮发动机(10)的轴(36)。 发电机(110)还包括电输出频率控制器(130),扭矩传感器装置被配置为确定由发电机(110)施加在传动系统(129)上的扭矩;以及控制器(112) 第一模式和第二模式下的发电系统。 在第一模式中,发电机(110)的电力输出的频率由电输出频率控制器(130)控制在预定的限度内,并且将降低的空闲信号提供给燃气涡轮发动机控制器 132)。 在第二模式中,发电机(132)的电力输出频率不受电输出频率控制器(130)的控制,并且向燃气涡轮发动机控制器(132)提供增加的空转信号。 发电机控制器(112)被配置为当转矩低于预定极限时在第一模式下操作发电系统(100),并且当扭矩高于预定极限时在第二模式中操作发电系统(100)。
    • 9. 发明公开
    • CONTROL METHOD AND DEVICE FOR TURBINE GENERATOR
    • VERRICHTUNGFÜREINEN TURINENGENERATOR的STEUERVERFAHREN
    • EP2620605A4
    • 2014-07-23
    • EP10857557
    • 2010-09-24
    • MITSUBISHI HEAVY IND LTD
    • ICHIKI YOSHIHIROSHIRAISHI KEIICHINISHIKAWA YOSHIHIKO
    • F01K23/02F01D15/10F01K23/06F01K23/10F01K23/12
    • F01D15/10F01K23/065F01K23/101F01K23/16F02C3/107F02C6/12F02C9/42F05D2220/62F05D2220/72F05D2270/07F05D2270/071Y02T10/16
    • [Problem] To provide a control method and device for a turbine generator, which can reduce generated power without wasting fuel consumption of a diesel engine when the demand power decreases and thereby the generated power is brought into an excess state. [Solution] A turbine generator configured by joining a power turbine (7) which is driven with exhaust energy of exhaust gas emitted from a diesel engine (3) as a power source and a steam turbine (9) in series, wherein the diesel engine (3) is provided with an exhaust turbosupercharger (5), extracts part of exhaust gas before the exhaust gas is supplied to the exhaust turbosupercharger (5), supplies the extracted exhaust gas to the power turbine (7) after adjusting the supply amount thereof, supplies steam generated by an economizer (11) to the steam turbine (9) after adjusting the supply amount thereof, and when the demand power decreases and thereby the generated power is brought into an excess state, decreases the supply amount of the exhaust gas to the power turbine (7) to minimize the output of the power turbine (7), and thereafter decreases the supply amount of the steam to the steam turbine (9).
    • 提供一种用于涡轮发电机的控制方法和装置,其可以在需求功率减小而不浪费柴油发动机的燃料消耗的同时降低发电功率,从而使发电功率达到过剩状态。 [解决方案]一种涡轮发电机,其通过将从作为电源的柴油发动机(3)排出的排气的排气能量驱动的动力涡轮机(7)和蒸汽涡轮机(9)串联连接而构成,其中,所述柴油发动机 (3)设置有排气涡轮增压器(5),在向排气涡轮增压器(5)供给排气之前,抽取废气的一部分,在将供给量调节后,将抽出的排气供给到动力涡轮机 在调节其供给量之后,将由节能器(11)产生的蒸汽供给到蒸汽涡轮机(9),并且当需求功率降低,从而使发电量达到过剩状态时,排气的供给量减少 到所述动力涡轮机(7),以使所述动力涡轮机(7)的输出最小化,然后减少所述蒸汽对蒸汽轮机(9)的供应量。