公开(公告)号：US3921390A

公开(公告)日：1975-11-25

申请号：US50610074

申请日：1974-09-16

申请人： GEN MOTORS CORP

发明人： STOLTMAN DONALD D

IPC分类号： F02C7/10 ,  F02C7/18 ,  F02C9/10 ,  F02C9/14

CPC分类号： F02C7/10

摘要： A control system for a two-shaft regenerative gas turbine has a low emission burner with a pedal operated throttle for proportioning the flow of primary and secondary air into a combustion chamber of the low emission burner and includes means for controlling fuel flow to maintain the outlet temperature of the burner in a range of temperatures to cover the power and speed range of the turbine engine. Secondary air is modulated to temper the turbine inlet temperature for a particular power level and speed of operation of the engine. The controller regulates the fuel supply at the burner in accordance with primary air flow by means for sensing the mass air flow to the engine compressor and means for automatically adjusting the fuel flow in correct proportion to the primary air flow to the burner so that the temperature of the primary combustion zone will be held at a desired level without adjusting the burner variable geometry or without sensing primary combustion zone temperature. An improved thermostat multiplier mechanism adjusts a fuel orifice to compensate for inlet air temperature to the burner.

摘要翻译： 用于双轴再生燃气轮机的控制系统具有低排放燃烧器，其具有踏板操作的节流阀，用于将一次空气和二次空气的流量与低排放燃烧器的燃烧室配比，并且包括用于控制燃料流量以维持出口 在一定温度范围内燃烧器的温度以覆盖涡轮发动机的功率和速度范围。 调节二次空气以调节涡轮机入口温度以达到发动机的特定功率水平和运行速度。 控制器通过用于感测到发动机压缩机的质量空气流量的装置来调节燃烧器处的燃料供应，以及用于与燃烧器的主要空气流量正确比例自动调节燃料流量的装置，使得温度 的主燃烧区域将被保持在期望的水平，而不调整燃烧器可变几何形状或者不检测主燃烧区温度。 改进的恒温器倍增器机构调节燃料孔口以补偿燃烧器的入口空气温度。

公开(公告)号：US3878676A

公开(公告)日：1975-04-22

申请号：US39776373

申请日：1973-09-17

申请人： GEN MOTORS CORP

发明人： HITZELBERGER ALAN L

IPC分类号： F02C9/36 ,  F02C9/10

CPC分类号： F02C9/36

摘要： A fuel supply system for a gas turbine engine such as a gascoupled vehicle driving engine includes a pump driven by the engine, a resistance valve between the pump outlet and the engine combustion chamber fuel nozzle, and a by-pass from the pump outlet to the pump inlet flowing through a by-pass valve and a resistance valve in series. The fuel nozzle provides a fuel metering orifice. The by-pass valve is biased to open by fuel pump discharge pressure and is biased to close by a pressure derived from the engine compressor discharge pressure. Compressor discharge pressure is fed through an orifice into a chamber to bias a diaphragm which operates to close the valve. Compensation for ambient temperature and pressure are provided by suitably controlled bleeds from this chamber. Limitation of metered fuel pressure for acceleration is accomplished by the compressor discharge pressure as so modified, and steady state fuel pressure is limited by a relief valve from the chamber the pressure setting of which is varied by manual control. The resistance valve in the engine fuel line establishes a suitable bias tending to open the by-pass valve to accommodate its characteristics to those of the engine, and a resistance valve in the by-pass line which has a higher setting enforces flow of fuel to the engine during starting.

摘要翻译： 用于诸如气体联接车辆驱动发动机的燃气涡轮发动机的燃料供应系统包括由发动机驱动的泵，泵出口和发动机燃烧室燃料喷嘴之间的阻力阀，以及来自泵出口的旁路 到通过旁路阀和电阻阀串联的泵入口。 燃料喷嘴提供燃料计量孔。 旁通阀被燃料泵排出压力偏压打开，并通过来自发动机压缩机排气压力的压力偏压关闭。 压缩机排出压力通过孔进料到室中以偏压操作以关闭阀的隔膜。 环境温度和压力的补偿由适当控制的来自该腔室的出血提供。 加压的计量燃油压力的限制是通过如此修改的压缩机排气压力来实现的，并且稳态燃料压力受到其压力设定由手动控制而改变的腔室的安全阀的限制。 发动机燃油管路中的阻力阀建立了适合于打开旁通阀以适应其发动机特性的偏压，并且具有较高设定值的旁通管线中的阻力阀将燃料流动 发动机起动时。

公开(公告)号：US3800534A

公开(公告)日：1974-04-02

申请号：US3800534D

申请日：1972-03-27

申请人： SUNDSTRAND CORP

发明人： KACEK D

IPC分类号： F02C6/20 ,  B64D41/00 ,  F02C9/08 ,  F02C9/10

CPC分类号： B64D41/00

摘要： An emergency hydraulic power supply for an aircraft or the like, including a hydraulic pump arranged to be driven by a turbine in turn driven by hot gas from a decomposition chamber, a fuel pump driven by the turbine for supplying fuel to the decomposition chamber, primary flow control valve means in the pump outlet for controlling fuel flow responsive to turbine speed, an ignition chamber communicable with the decomposition chamber and having a start grain for initiating turbine operation to start the fuel pump, a secondary control valve in the pump outlet, and control means for sensing turbine speed and opening the secondary valve when the turbine attains a speed indicating the start grain has about burned out, and closing the secondary valve in the event that the turbine attains a speed indicating the primary flow control valve means is inoperative to control turbine speed.

摘要翻译： 一种用于飞机等的应急液压动力源，包括被涡轮机驱动的液压泵，其又由来自分解室的热气驱动，由涡轮驱动的用于向分解室供应燃料的燃料泵，初级 用于控制响应于涡轮转速的燃料流量的流量控制阀装置，可与分解室通信的点火室，并且具有用于启动涡轮机操作以启动燃料泵的启动谷物，泵出口中的二次控制阀，以及 控制装置，用于当涡轮达到指示起始谷物已经烧尽的速度时，用于感测涡轮速度和打开次级阀，并且在涡轮达到指示主流量控制阀装置的速度不起作用的情况下关闭次级阀 控制涡轮机转速。

公开(公告)号：US3795104A

公开(公告)日：1974-03-05

申请号：US3795104D

申请日：1972-11-03

申请人： FORD MOTOR CO

发明人： MC LEAN A

IPC分类号： F02C9/28 ,  F02C9/48 ,  F02C9/54 ,  F02C9/10

CPC分类号： F02C9/48

摘要： A simple, low cost control system for a single shaft gas turbine engine in which steady state operation is controlled by movement of the stator vanes of a torque converter fixed to the compressor shaft, to load or unload the shaft; accelerations are controlled by controlling fuel flow as a function of engine temperatures and speeds; and engine starting and idle speed operations, as well as overtemperature operations are controlled by opening or closing a nozzle constituted by variable angle compressor inlet guide vanes.

摘要翻译： 一种用于单轴燃气涡轮发动机的简单的低成本控制系统，其中通过固定到压缩机轴的变矩器的定子叶片的运动来控制稳态操作，以装载或卸载轴; 通过控制燃料流量作为发动机温度和速度的函数来控制加速度; 并且通过打开或关闭由可变角度压缩机入口导叶构成的喷嘴来控制发动机起动和怠速操作以及过热操作。

公开(公告)号：US3777480A

公开(公告)日：1973-12-11

申请号：US3777480D

申请日：1972-03-20

申请人： GEN MOTORS CORP

发明人： STOLTMAN D

IPC分类号： F02C9/32 ,  F02C9/36 ,  F02C9/10

CPC分类号： F02C9/32 ,  F02C9/36

摘要： A fuel control disclosed in connection with a gas-coupled gas tubine engine for shaft power output purposes. The fuel control is supplied by a transfer pump and a pressure pump in series and delivers fuel to a nozzle in the engine combustion apparatus. The control receives an input of gas generator speed and an input of compressor discharge pressure. It receives electrical inputs serving to limit turbine inlet temperature and power turbine speed, and may include an electrical On-Off input. Flow of fuel to the engine is directly controlled by a slave valve which responds to pressure of fuel delivered to the nozzle and to a control pressure derived from the pressure pump outlet. The control pressure is developed between an upstream orifice and parallel downstream valves which include a solenoid valve operated to limit turbine inlet temperature and power turbine speed, a valve responsive to compressor discharge pressure, and a governor valve responsive to gas generator turbine speed. The OnOff control bleeds the nozzle to the fuel tank when the engine is turned off. During engine deceleration, the slave valve stops fuel flow without emptying the nozzle and the fuel line to it. The metering head across the slave valve is controlled by a differential pressure responsive by-pass valve which discharges excess fuel to the pressure pump inlet. The by-pass valve may define a passage for fuel to maintain a pilot flame during deceleration.

摘要翻译： 关于用于轴功率输出目的的气体联接气体发动机公开的燃料控制。 燃料控制由输送泵和压力泵串联提供，并将燃料输送到发动机燃烧装置中的喷嘴。 控制器接收气体发生器速度的输入和压缩机排放压力的输入。 它接收用于限制涡轮机入口温度和功率涡轮机速度的电输入，并且可以包括电开关输入。 燃料流向发动机的流量直接由从动阀控制，从动阀响应输送到喷嘴的燃料的压力和来自压力泵出口的控制压力。 控制压力在上游孔口和并行下游阀门之间形成，其包括操作以限制涡轮机入口温度和功率涡轮机速度的电磁阀，响应于压缩机排气压力的阀门以及响应于气体发生器涡轮机速度的调速阀。 当发动机关闭时，On-Off控制器将喷嘴喷射到燃油箱。 在发动机减速期间，从动阀停止燃油流动，而不会将喷嘴和燃油管路排空。 从阀的计量头由压差响应的旁通阀控制，该压力阀将多余的燃料排放到压力泵入口。 旁路阀可以限定用于燃料的通道，以在减速期间保持导向火焰。

公开(公告)号：US3769791A

公开(公告)日：1973-11-06

申请号：US3769791D

申请日：1971-11-05

申请人： LUCAS INDUSTRIES LTD

发明人： LEWIS G

IPC分类号： F02C9/32 ,  F02C9/10

CPC分类号： F02C9/32 ,  Y10T137/2622

摘要： A fuel supply system for a gas turbine engine has a positivedisplacement pump driven by the engine a valve downstream of the pump having an inlet and two outlets. A control element varies flow through the two outlets simultaneously. One of the outlets supplies fuel to the engine and the other outlet communicates with a pressure-responsive spill valve with the low pressure side of the pump. The spill valve arrangement is such that the pressures at the valve outlets remain substantially equal.

摘要翻译： 用于燃气涡轮发动机的燃料供应系统具有由发动机驱动的正排量泵，泵的下游具有入口和两个出口。 控制元件同时改变两个出口的流量。 其中一个出口向发动机供应燃料，另一个出口与具有低压侧的压力响应溢流阀连通。 泄漏阀装置使得阀出口处的压力保持基本相等。

公开(公告)号：US3686859A

公开(公告)日：1972-08-29

申请号：US3686859D

申请日：1970-09-25

申请人： CHANDLER EVANS INC

发明人： WHITE ALBERT H

IPC分类号： F02C7/26 ,  F02C9/08 ,  F02C9/10

CPC分类号： F02C7/26

摘要： A starting circuit for a regenerative gas turbine engine wherein a fuel metering valve and power turbine inlet nozzles are positioned in response to control signals provided by a closed loop system. Engine operating parameters, including gas generator turbine inlet temperature, are sensed and electrical signals commensurate therewith are delivered as inputs to the logic circuitry where, in combination with selected operational mode inputs provided by the operator, they are operated upon to provide control signals for the power turbine nozzle actuators and the gas generator fuel control metering valve.

摘要翻译： 一种用于再生燃气涡轮发动机的启动电路，其中响应于由闭环系统提供的控制信号而定位燃料计量阀和动力涡轮机入口喷嘴。 发动机操作参数（包括气体发生器涡轮机入口温度）被感测，并且与之相称的电信号作为输入传送到逻辑电路，其中结合操作者提供的所选择的操作模式输入，它们被操作以提供控制信号 动力涡轮喷嘴执行器和气体发生器燃料控制计量阀。

公开(公告)号：US3600889A

公开(公告)日：1971-08-24

申请号：US3600889D

申请日：1969-06-17

申请人： LUCAS INDUSTRIES LTD

发明人： IFIELD RICHARD J

IPC分类号： F02C9/00 ,  F02C9/10

CPC分类号： F02C9/32

摘要： A system for controlling the fuel supply to a gas turbine engine includes a valve between the fuel pump and the burners of the engine and arranged to spill fuel delivered by the pump. Fuel flows to the burners via a venturi and the spill valve is urged in a direction to spill fuel by the pressure upstream of the venturi and in the other direction by a spring-assisted piston subjected to the pressure at the venturi throat. Cooperating with the spring-assisted piston is a lever actuated by a diaphragm forming one wall of a chamber which is subjected to an air pressure signal derived from the output of the engine compressor and modified by a blade movable in a kinetic orifice. The blade is movable by a governor mechanism and a linkage coupled to the engine throttle control, so that the blade is moved to reduce the pressure in the chamber when the desired engine speed is greater than the actual speed, and thereby move the lever so that the spill valve may operate to increase spillage of fuel. The valve is similarly operated to reduce spillage when the desired speed is greater than the actual speed. An opposite wall of the chamber is formed by a smaller diaphragm biased towards the first diaphragm by a spring. Stops on the respective diaphragms maintain them in spaced relationship. These stops separate at a predetermined pressure to ensure that a sufficient margin for acceleration exists at all engine speeds.

公开(公告)号：US3568439A

公开(公告)日：1971-03-09

申请号：US3568439D

申请日：1968-07-24

申请人： HOLLEY CARBURETOR CO

发明人： CANALE RAYMOND P

IPC分类号： F02C9/26 ,  F02C9/10

CPC分类号： F02C9/26

摘要： A TURBINE ENGINE FUEL CONTROL IS PROVIDED WITH A FUEL INLET, METERING-TYPE GOVERNOR VALVE ASSEMBLY RESPONSIVE TO SIGNALS GENERATED IN RESPONSE TO ENGINE SPEED AND INDICIA OF OPERATOR POWER REQUEST, FUEL BYPASS VALVING MEANS FOR RETURNING UNMETERED FUEL FROM THE FUEL CONTROL TO AN ASSOCIATED FUEL SUPPLY SYSTEM, COMPRESSOR DISCHARGE PRESSURE SENSING MEANS FOR TENDING TO FURTHER CLOSE THE BYPASS VALVING MEANS AS COMPRESSOR DISCHARGE PRESSURE INCREASES AND PRESSURE RESPONSIVE MEANS RESPONSIVE TO THE DIFFERENTIAL IN PRESSURE WHICH METER THE FUEL FOR OPENING SAID BYPASS VALVING MEANS IN ORDER TO ACHIEVE A RATE OF METERED FUEL FLOW CORRESPONDING TO COMPRESSOR DISCHARGE PRESSURE.

公开(公告)号：US3514946A

公开(公告)日：1970-06-02

申请号：US3514946D

申请日：1968-02-06

申请人： LUCAS INDUSTRIES LTD

发明人： WARNE EUGENE HAROLD

IPC分类号： F02C9/30 ,  F02C9/06 ,  F02C9/08 ,  F02C9/10

CPC分类号： F02C9/30