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公开(公告)号：US4326376A
公开(公告)日：1982-04-27
申请号：US69141
申请日：1979-08-23
Applicant: Charles F. Stearns , David L. Chapski , Kenneth F. Vosseller
Inventor： Charles F. Stearns , David L. Chapski , Kenneth F. Vosseller
CPC classification number: F02C9/28
Abstract: Fuel flow to a gas turbine engine is controlled in response to power lever position and CDP. Fuel is supplied to the engine through three fuel flow regulating circuits which are in parallel. In one of these circuits there is a valve which establishes a minimum fuel flow which decreases with increasing power lever advance. In a second circuit there is a valve which modifies fuel flow in response to CDP. In a third circuit there is a valve which modifies fuel flow in response to CDP and receives fuel from a valve which opens with increasing power lever advance. The fuel control system includes a low power sensitive torque motor which may be activated to increase the pressure drop across the three circuits whose flow thus increases proportionally. Normal engine operation is obtainable without the use of the torque motor which provides an interface to an electronic control unit which senses various engine and ambient parameters and activates the torque motor in order to modify fuel flow accordingly.
Abstract translation: 响应于功率杆位置和CDP控制到燃气涡轮发动机的燃料流量。 燃料通过并联的三个燃料流量调节回路供给发动机。 在其中一个回路中，有一个阀，其建立了最小的燃料流量，其随着功率杆提前量的增加而减小。 在第二回路中，存在响应于CDP改变燃料流量的阀。 在第三回路中，存在响应于CDP改变燃料流量并且从增加的功率杆提前打开的阀接收燃料的阀。 燃料控制系统包括低功率敏感力矩电动机，其可以被激活以增加跨过三个电路的压力降，其流量因此成比例地增加。 可以在不使用向电子控制单元提供与各种发动机和环境参数的接触的转矩马达的情况下获得正常的发动机运行，并且启动扭矩马达以相应地改变燃料流。
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公开(公告)号：US4282710A
公开(公告)日：1981-08-11
申请号：US15252
申请日：1979-02-26
Applicant: William W. Avant
Inventor： William W. Avant
CPC classification number: F02C9/44
Abstract: A system and method for selectively and controllably supplying a preselected pressure source for controlling a pressure-responsive fuel flow metering system, the system being especially capable for use as a Mach number hold unit for controlling fuel flow to aircraft jet engines.
Abstract translation: 一种用于选择性和可控地供应用于控制压力响应燃料流量计量系统的预选压力源的系统和方法，该系统特别能够用作用于控制到飞机喷气发动机的燃料流量的马赫数保持单元。
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公开(公告)号：US4238926A
公开(公告)日：1980-12-16
申请号：US943090
申请日：1978-09-18
Applicant: Ernest A. Timby , Rodney H. Walsh
Inventor： Ernest A. Timby , Rodney H. Walsh
Abstract: Apparatus for degrading safety fuel of the type containing an antimisting polymer and comprising a cylindrical vaned stator and vaned rotor in radially concentric array, whereby rotation of the rotor will cause safety fuel pumped through the apparatus to be subjected to sufficient shear and local acceleration to be degraded to a state acceptable to engines and their control apparatus.
Abstract translation: 用于降低包含抗起泡聚合物的安全燃料的装置，包括径向同心的圆柱形的定子和叶片式转子，由此转子的旋转将引起泵送通过设备的安全燃料经受足够的剪切和局部加速度 降级到发动机及其控制装置可接受的状态。
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公开(公告)号：US4209979A
公开(公告)日：1980-07-01
申请号：US863361
申请日：1977-12-22
Applicant: Geoffrey D. Woodhouse , George B. Mattson
Inventor： Geoffrey D. Woodhouse , George B. Mattson
Abstract: A free turbine engine for driving ground vehicles with various deceleration or braking actions including power feedback braking wherein the turbine compressor is selectively interconnected with the power output shaft only in such a manner whereby compressor inertia assists in decelerating the vehicle.
Abstract translation: 一种用于驱动地面车辆的自由涡轮发动机，其具有包括动力反馈制动的各种减速或制动动作，其中，涡轮压缩机仅以这样的方式选择性地与动力输出轴相互连接，使得压缩机惯性有助于使车辆减速。
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公开(公告)号：US4185460A
公开(公告)日：1980-01-29
申请号：US864857
申请日：1977-12-27
Applicant: M. Samuel Moore , Charles F. Paluka
Inventor： M. Samuel Moore , Charles F. Paluka
CPC classification number: F02C9/42 , Y02T50/671
Abstract: An aircraft having two turbine engines is provided with both torque and temperature sensitive electronic circuitry to control the fuel supplied to the turbine engines. Pushbutton switches are provided for the selection of the desired torque level by the pilot. The fuel to either engine is reduced, regardless of output torque and its relationship to the pushbutton values of selected torque, when the engine temperature exceeds a predetermined safety level. Failsafe operation is provided through the use of a main fuel supply path including a manual fuel control valve extending from the fuel pump to the engine fuel nozzles, and a normally closed bypass fuel control line which selectively diverts fuel from the principal path under the control of the temperature and torque responsive electronic circuitry. An electromagnetically operated valve in the bypass line is normally closed and is selectively operated to the desired open condition under the control of the torque and temperature responsive circuitry mentioned above, to reduce fuel supplied to the turbine engines.
Abstract translation: 具有两个涡轮发动机的飞机设置有扭矩和温度敏感的电子电路，以控制供应到涡轮发动机的燃料。 提供按钮开关用于由飞行员选择所需的扭矩水平。 当发动机温度超过预定的安全水平时，不管输出扭矩和其与所选转矩的按钮值的关系如何，对任一发动机的燃料减少。 通过使用包括从燃料泵延伸到发动机燃料喷嘴的手动燃料控制阀的主要燃料供给路径以及在主控制路径下选择性地转移燃料的常闭旁路燃料控制线来提供故障保护操作， 温度和转矩响应电子电路。 旁路管路中的电磁操作阀常闭，并在上述转矩和温度响应电路的控制下选择性地操作到所需的开启状态，以减少供应到涡轮发动机的燃料。
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Patent Agency Ranking6.发明授权
公开(公告)号：US4185203A
公开(公告)日：1980-01-22
申请号：US897678
申请日：1978-04-19
Applicant: Tohru Takeuchi
Inventor： Tohru Takeuchi
IPC: H02J9/08 , F02C3/10 , F02C9/28 , F02D29/06 , G05B11/32 , G05D13/62 , H02P9/04 , F02C9/04 , G05D13/00
CPC classification number: F02C9/28 , F05D2270/02 , F05D2270/05
Abstract: A reference signal generator generates a variable reference signal with which a signal indicating the momentary rotational speed of the prime mover (such as a gas turbine) for a generator is compared, to produce a rotational speed control signal in accordance with a signal representing the load applied to the prime mover, so as to compensate for the rotational speed fluctuation caused by load connection by holding the rotational speed of the prime mover above the desired level during no-load operation and at the desired level under load.
Abstract translation: 参考信号发生器产生可变参考信号，通过该可变参考信号比较表示发电机的原动机（例如燃气轮机）的瞬时转速的信号，以根据表示负载的信号产生转速控制信号 以便通过在空载操作期间将原动机的转速保持在期望水平以上并且在负载下达到期望水平，来补偿由负载连接引起的转速波动。
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公开(公告)号：US4178754A
公开(公告)日：1979-12-18
申请号：US815251
申请日：1977-07-13
Applicant: Ernest R. Earnest
Inventor： Ernest R. Earnest
Abstract: A method and apparatus for control of an integrated combined cycle Brayton-Rankine engine is disclosed. The engine has a combustor and main power turbine operating on the Brayton cycle. Combustion air is supplied by a compressor independently driven by a Rankine vapor turbine. The closed loop Rankine cycle derives its heat energy from the exhaust of the Brayton turbine. Engine speed and power level are controlled by varying the fuel flow to the combustor and by throttling the air flow to the compressor.
Abstract translation: 公开了一种综合联合循环布雷顿 - 兰金发动机的控制方法和装置。 发动机具有在布雷顿循环上运行的燃烧器和主动力涡轮机。 燃烧空气由独立由兰金汽轮机驱动的压缩机供应。 闭环兰金循环从Brayton涡轮机的排气中获得其热能。 发动机速度和功率水平通过改变到燃烧器的燃料流量并通过节流到压缩机的气流来控制。
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8.发明授权Control system for and method of zero error automatic calibration of gas turbine temperature control parameters 失效燃气轮机温度控制参数的零误差自动校准控制系统及方法
公开(公告)号：US4161101A
公开(公告)日：1979-07-17
申请号：US722066
申请日：1976-09-09
Applicant: Thane M. Drummond
Inventor： Thane M. Drummond
CPC classification number: F02C9/28 , F05D2260/80 , F05D2270/303
Abstract: A control system including a controller for reading temperature values from sensors in a gas turbine, determining the reliability of the sensors, and issuing a fuel control signal for use in controlling the turbine is disclosed. The fuel control signal has a calculated value which is a function of the turbine operating temperature derived from the values of temperature signals generated by the sensors.
Abstract translation: 公开了一种控制系统，其包括用于从燃气轮机中的传感器读取温度值的控制器，确定传感器的可靠性，以及发出用于控制涡轮机的燃料控制信号。 燃料控制信号具有根据由传感器产生的温度信号的值导出的涡轮机运行温度的函数的计算值。
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9.发明授权Fan R. P. M. control loop stabilization using high rotor speed 失效Fan R. P. M. control control stabilization using high rotor speed
公开(公告)号：US4104876A
公开(公告)日：1978-08-08
申请号：US746649
申请日：1976-12-02
Applicant: Hals N. Larsen , Peter W. Kamber
Inventor： Hals N. Larsen , Peter W. Kamber
CPC classification number: F02C9/56 , F02C9/28 , F05D2270/023 , Y02T50/671
Abstract: A fan spool stabilization loop which improves the stability of the low speed or fan spool in a two spool turbofan engine. In a preferred embodiment, the actual rate of rotation of the high speed spool is compared with the desired rate of rotation determined by integrating the difference between the desired rate of rotation of the fan spool and the actual rate of rotation. The difference therebetween controls the flow of fuel to the turbofan engine. In an alternate preferred embodiment of the invention, the rate of change of rotation of the high speed spool is added to the actual rate of rotation of the fan spool and the result is compared with the desired rate of rotation of the fan spool. The difference therebetween is utilized to control the flow of fuel to the turbofan engine.
Abstract translation: 风扇阀芯稳定回路，提高了两个卷轴涡轮风扇发动机中低速或风扇阀芯的稳定性。 在优选实施例中，将高速线轴的实际转速与通过将风扇阀芯的期望转速与实际转速之差的差积分确定的所需转速进行比较。 其间的差异控制到涡轮风扇发动机的燃料流。 在本发明的替代优选实施例中，将高速滑阀的转动速率加到风扇滑阀的实际旋转速率上，并将其结果与风扇阀芯的期望转速进行比较。 它们之间的差异用于控制到涡轮风扇发动机的燃料流。
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10.发明授权Twin-spool gas turbine power plant with means to spill compressor interstage airflow 失效双管式燃气轮机发电厂具有溢出压缩机级间气流的手段
公开(公告)号：US4055946A
公开(公告)日：1977-11-01
申请号：US671517
申请日：1976-03-29
Applicant: William H. Sens
Inventor： William H. Sens
CPC classification number: F04D27/0207 , F02C9/16
Abstract: In order to take advantage of the efficient utilization of fuel occasioned by operating a turbine type power plant of the multiple spool design at very high overall pressure ratios, the high pressure spool is operated at substantially full speed and substantially full pressure ratio at low altitude and the high pressure compressor exit temperature is maintained at or near the value for which the engine was designed to operate at the climb or altitude cruise condition by controlling the pressure of the air admitted to the high pressure compressor.
Abstract translation: 为了充分利用在非常高的整体压力比下操作多线轴设计的涡轮机型发电厂而引起的燃料的有效利用，高压阀芯在低空处以基本全速和基本全压比运行， 通过控制进入高压压缩机的空气的压力，高压压缩机出口温度保持在或接近发动机设计为在爬升或高度巡航条件下操作的值。
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