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    • 41. 发明授权
    • Control system for gas turbine engine
    • 燃气轮机发动机控制系统
    • US4276744A
    • 1981-07-07
    • US76890
    • 1979-09-19
    • Alan D. Pisano
    • Alan D. Pisano
    • F02C9/28F02C9/56F02C3/10
    • F02C9/28F05D2220/329
    • A gas turbine engine control system is provided. In a preferred control system for use in combination with a helicopter, input signals respectively representative of power turbine speed error, power turbine shaft torque, and compressor shaft speed are employed. From these input signals, five intermediate signals are developed. One of the intermediate signals represents the main rotor speed error. Each of the five intermediate signals is provided with a separate predetermined gain and coupled to summation means. The predetermined gains are selected to be of values which reduce the effects of resonances provided by the mail and tail rotors of the helicopter. The output of the summation means represents a control signal and may be employed to operate a fuel control valve.
    • 提供燃气涡轮发动机控制系统。 在与直升机组合使用的优选控制系统中,采用分别代表动力涡轮机转速误差,功率涡轮机轴转矩和压缩机轴转速的输入信号。 从这些输入信号,开发了五个中间信号。 中间信号之一表示主转子速度误差。 五个中间信号中的每一个被提供有单独的预定增益并且耦合到求和装置。 预定增益被选择为降低由直升机的邮件和尾转子提供的共振效应的值。 求和装置的输出表示控制信号,并可用于操作燃油控制阀。
    • 43. 发明授权
    • Gas turbine-transmission plant
    • 燃气轮机变电站
    • US4220057A
    • 1980-09-02
    • US835035
    • 1977-09-20
    • Sven-Olof Kronogard
    • Sven-Olof Kronogard
    • F02C7/36F02C9/22F02C9/56F16H47/08
    • F02C7/36Y10S74/05
    • In an automotive gas turbine power plant including at least one power turbine rotor and a further turbine rotor driving the compressor of the plant, the latter rotor is undersized with respect to the power consumption by the compressor during normal operation and is augmented from the power turbine rotor. The auxiliaries of the power plant are driven from the power turbine rotor, which is connected to the power output shaft, as well as to the compressor turbine rotor by means of a planetary gearing permitting a braking of the output shaft to standstill without the speed of the power turbine rotor being reduced to below that necessary for operating the auxiliaries.
    • 在包括驱动设备的压缩机的至少一个动力涡轮机转子和另外的涡轮转子的汽车燃气轮机发电厂中,相对于压缩机在正常运行期间的功率消耗,后一个转子的尺寸不足,并且从动力涡轮 转子。 动力装置的辅助设备由与动力输出轴连接的动力涡轮转子以及通过行星齿轮传动到压缩机涡轮转子的动力驱动,允许输出轴的制动停止,而不会以 动力涡轮转子减少到低于操作辅助设备所必需的。
    • 45. 发明授权
    • Combined cycle electric power plant having an improved digital/analog
hybrid gas turbine control system
    • 具有改进的数字/模拟混合燃气轮机控制系统的联合循环发电厂
    • US4195231A
    • 1980-03-25
    • US495726
    • 1974-08-08
    • Terry J. ReedJack R. SmithRoy W. Kiscaden
    • Terry J. ReedJack R. SmithRoy W. Kiscaden
    • F01K23/10F02C9/28F02C9/56H02P9/04
    • F02C9/28F01K23/105F05D2270/021F05D2270/101Y02E20/16
    • A digital computer system provides automatic control for a steam turbine and two gas turbines in a combined cycle electric power plant during startup and load modes of operation. The gas turbine automatic control system provides speed, load and blade path temperature control functions in developing an output fuel control signal for application to each gas turbine fuel valve control. An analog control for each gas turbine selectively provides startup and temperature and load control functions as a backup for the automatic gas turbine control, and further provides gas turbine overspeed, surge and other limit controls continuously. An operator panel functions with the analog and digital controls to provide an operator interface with the plant, and an interface circuit ties the digital and analog controls together for bumpless transfer between manual and automatic modes of operation. A sequencer is provided for each gas turbine and it provides gas turbine startup sequence control, gas turbine trip protection and other functions in both the automatic and the backup modes of operation. A gas turbine monitor develops temperature and vibration signals for the sequencer and the fuel controls.
    • 数字计算机系统在启动和负载运行模式期间为联合循环发电厂中的蒸汽轮机和两个燃气轮机提供自动控制。 燃气轮机自动控制系统提供速度,负载和叶片路径温度控制功能,用于开发输出燃料控制信号,以应用于每个燃气轮机燃油阀控制。 每个燃气轮机的模拟控制选择性地提供启动和温度和负载控制功能,作为自动燃气轮机控制的备份,并进一步提供燃气涡轮超速,喘振和其他极限控制。 操作面板具有模拟和数字控制功能,可与工厂提供操作员界面,并且接口电路将数字和模拟控制连接在一起,在手动和自动操作模式之间进行无扰动传输。 为每个燃气轮机提供了一个定序器,并且在自动和备用操作模式下提供燃气轮机启动顺序控制,燃气轮机跳闸保护和其他功能。 燃气轮机监控器为定序器和燃料控制器提供温度和振动信号。
    • 47. 发明授权
    • Control method and apparatus for a single shaft turbine with prewhirl of air entering the compressor
    • 用于进口压缩机的空气压缩机的单轴涡轮机的控制方法和装置
    • US3797230A
    • 1974-03-19
    • US3797230D
    • 1972-08-09
    • GEN MOTORS CORP
    • AMANN CRUCINS E
    • F02C9/20F02C9/54F02C9/56F02C9/14
    • F02C9/54F02C9/20F02C9/56Y10S74/05
    • A vehicle turbine propels the vehicle through a change-speed transmission. To reduce vehicle acceleration time with an acceptable penalty with respect to fuel consumption, the compressor of the engine has variable inlet guide vanes which are shifted into a positive prewhirl angle at idling speeds when the transmission is shifted into a drive condition. Thus the engine has a low speed idle, with axially oriented guide vanes and normal air entrance, when the transmission is in neutral or park, and a high speed idle with positive prewhirl when the transmission is in a drive condition. Also, the vanes are shifted at full speed of the engine to provide negative prewhirl and thus reduce the engine speed corresponding to maximum power output. Because of the higher idle and lower maximum speeds, the acceleration time of the turbine is reduced.
    • 车辆涡轮机通过变速传动推动车辆。 为了以相对于燃料消耗的可接受的惩罚来减少车辆加速时间,发动机的压缩机具有可变的入口导向叶片,当变速器转换到驱动条件时,它们以空转速度偏移到正的预旋转角度。 因此,当变速器处于空档或停车状态时,发动机具有低速怠速,轴向定向的导向叶片和正常的空气入口,以及当变速器处于驱动状态时具有正向预热的高速怠速。 此外,叶片以发动机的全速移动以提供负的前轮,并因此降低对应于最大功率输出的发动机转速。 由于较高的空转和较低的最大速度,涡轮机的加速时间减少。