JP2006138228A - Flow control system for gas turbine engine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a flow control system controlling a variable displacement pump provided with a metering valve in fluid communication with the pump for metering an output of the pump. <P>SOLUTION: This system is a highly stable flow rate control system controlling the variable displacement pump. A regulating valve 36 receives part of the output of the pump 12 as a bypass flow as a first pressure wherein an output of the regulating valve 36 is at an interim pressure. The interim pressure is roughly equal to an average of the first pressure and a low reference pressure. An actuator 20 sets a displacement of the pump 12 by acting on a piston 18 connected to a cam ring 16 of the pump 12. The actuator 20 receives the interim pressure to determine the output of the variable displacement pump 12. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

(Field of Invention)
The present invention relates generally to a system for regulating fluid flow, and more particularly to a system for regulating the flow of liquid fuel from a variable displacement pump to a gas turbine by utilizing a bypass flow.

(Background of the Invention)
Metered fuel pumps are often excessive in capacity because they have an excess fuel flow capacity to deliver the proper amount of fuel to the engine involved. As a result, a large amount of boosted fuel is returned to the pump inlet for recirculation under many operating conditions. In fuel return and recirculation, the fuel temperature rises significantly due to the extra energy that is converted into heat after being added to the fuel as pressure decreases in the recirculation path. In new designs, heating of the fuel is an important issue because the fuel is used as a heat exchange medium that maintains the normal operating temperature. Other methods for heat exchange are undesirable due to size, weight and cost. This problem is exacerbated in new engines because the fuel pump needs to supply the engine with fuel. For example, new medium to large engines use linear motion pistons as guide vanes. A linear piston requires a drive source for rotating fuel. This rotation is a transient phenomenon that causes an extremely short supply of fuel to the engine.
The variable displacement fuel pump can overcome only a part of the drawbacks of the metering fuel pump by changing the fuel discharge amount. The fuel distributed by changing the fuel discharge amount further approaches the required amount of the engine. Therefore, this recirculation flow rate decreases together with the heat generated by recirculation. Variable displacement pumps are known in the art as disclosed in US Pat. No. 5,833,438 to Sunberg, the entire disclosure of which is incorporated herein by reference. Variable displacement pumps typically include a rotor having a fixed shaft and a rotating cam ring. The pump discharge is controlled by controlling the position of the cam ring relative to the rotor. The discharge amount is controlled by a servo valve driven by a torque motor. However, engine operating conditions are often accompanied by transient phenomena that occur during engine actuator rotation start and similar processes, as is known by those skilled in the art. Under such operating conditions involving rapid changes, the conventional pump control system cannot respond quickly and appropriately. In addition, many conventional pump control systems lack the stability required to fuel the engine in a reliable manner. As already mentioned, despite advances in the state of the art, variable displacement pumps are not stable and cannot respond sufficiently and quickly to change the fuel demanded by the engine. As a result, performance is not sufficient and fuel flow is usually excessive.
Examples of variable displacement pump controllers are given in U.S. Pat. No. 5,716,201 granted to Peck et al. And Router et al. (Reuter et al.), All of which are hereby incorporated by reference. U.S. Pat. No. 5,715,674. These pump control systems are intended to maintain fuel flow accurately throughout the full range of engine operating conditions. However, as mentioned above, such a system still has improper parts that are complex. Furthermore, such a system can achieve fuel supply only within a reasonable range of supply zones by distributing excess fuel that is recirculated. Also, it is undesirable to provide a pump control system with complex electronic circuitry and many additional equipment that add more expense and complexity than necessary.
In view of the above, it would be desirable to provide a flow control system with a simple design that quickly adjusts the discharge volume of a variable displacement pump that is both stable and free of the associated drawbacks found in the prior art.

(Summary of the Invention)
In one embodiment, the present invention relates to a flow control system for controlling a variable displacement pump, comprising a metering valve in fluid communication with the variable displacement pump for metering pump discharge. The control valve that maintains the differential pressure before and after the metering valve receives a part of the discharge of the variable displacement pump as a bypass flow rate that maintains the first pressure. Here, the output of the control valve is a temporary pressure, which is a low reference pressure that is approximately equal to the average of the first pressures. The actuator sets the discharge of the variable displacement pump by acting on the piston connected to the cam ring of the variable displacement pump. The set value of this actuator is determined by the differential pressure between the temporary pressure and the second part of the discharge of the variable displacement pump that maintains the first pressure.
The object of the present invention is to increase the responsiveness of the fuel metering unit while maintaining acceptable stability under all operating conditions.
Another object of the present invention is to provide a hydraulic mechanical fuel metering unit for a variable displacement pump. Yet another object is to provide a fuel metering unit that responds quickly and accurately to dynamic flow conditions.
In another embodiment, the invention relates to a method for metering a variable displacement pump that supplies fuel to an engine. This method accepts fuel that maintains a low reference pressure into the variable displacement pump, boosts the fuel with a variable displacement pump so that the discharge of the variable displacement pump becomes high pressure, and discharges the variable displacement pump with a metering valve. , The process of generating the return flow from the discharge of the variable displacement pump to respond quickly when the engine needs additional fuel, and adjusting the differential pressure across the metering valve using a regulating valve Process. The regulator valve is in fluid communication with the outflow return flow to generate a temporary pressure approximately equal to the average of the outflow return flow and the low reference pressure. The method also includes the step of adjusting the discharge of the variable displacement pump using a cam actuator connected to the cam ring of the variable displacement pump for adjusting the discharge. Here, the cam actuator accepts a temporary pressure to determine the cam actuator setting.

(Detailed description of the invention)
Referring to FIG. 1, a schematic representation of a flow control system according to the present invention, generally indicated at 10, is shown. For clarity of the following description, the arrows shown in the flow control system 10 system indicate the direction in which the fuel flows, and the annotation letter “P” is used to indicate the pressure maintained at a certain position. Here, all the related descriptions such as right and left and up and down refer to the flow rate control system 10 as shown in FIG. 1 and are not meant to be limiting. In addition, conventional means such as filters and shut-off solenoids are not included in FIG. 1 for clarity. The flow control system 10 maintains the discharge rate of the movable vane variable displacement pump 12 to quickly respond to engine fuel demand in a stable manner while avoiding undue complexity.
The variable displacement pump 12 includes a rotor 14 and a rotating cam ring 16. For a detailed description of the moveable wing variable displacement pump, reference is made to US Patent Application Publication No. 2002/0103849 published June 5, 2003, which is hereby incorporated by reference in its entirety. The variable displacement pump 12 receives the fuel flow rate that maintains the inlet pressure PAF, and discharges the fuel flow rate at the discharge pressure PF. The piston 18 is operatively connected to a cam ring 16 that controls the position of the cam ring 16 relative to the rotor 14, thereby changing the discharge amount of the variable displacement pump 12. The cam actuator device 20 positions the piston 18 as described below. It will be apparent to those skilled in the art that similar and modified arrangements that function in this manner, and thus other types of actuators that are considered merely design choices, are within the scope of the claimed invention. The maximum flow rate setting value of the variable displacement pump 12 occurs when the piston 18 moves the maximum distance in the left direction.
A feedback line 21 in fluid communication with the discharge of the variable displacement pump 12 supplies fuel to the line 29 connected to the inlet 22 of the cam actuator 20 at a pressure P1W. Orifices 24 and 26 restrict the flow rate to line 29. The pressure in line 29 is approximately equal to P1W + PAF divided by 2 and is shown as P11 in FIG. It will be apparent to those skilled in the art that the pressure maintaining P1W is approximately equal to the pressure PF. The feedback line 21 also supplies fuel that maintains the pressure P1W to other locations not shown such as the engine, main metering valve and bleed band servo valve (not shown) when needed. This line 29 also connects to a low reference pressure PAF. The other inlet 28 of the cam actuator 20 receives fuel that maintains a temporary pressure P12 as described below.
The housing 23 of the cam actuator 20 holds a piston 18 that divides the interior of the housing 23 into two parts. The coil spring 30 biases the piston 18. The pressure on the right side of the piston 18 in the housing 23 is approximately equal to the average pressure of P1W and PAF. The balance between the method of determining the dimensions of the coil spring 30 and the differential pressure between the left and right chambers of the housing 23 serves to position the piston 18 in the cam actuator 20. The cam ring 16 moves in accordance with the piston operation, and the discharge amount of the variable displacement pump 12 changes. Preferably, the coil spring 30 is sized and configured to position the piston 18 at the maximum flow rate for starting the variable displacement pump 12. Throughout the flow control system 10, the coil spring is dimensioned as a function of the product of piston area and fuel pressure, as will be apparent to those skilled in the art, and therefore will not be described in detail here.
The discharge of the variable displacement pump 12 passes through the main metering valve 34 and the wash filter 32 which removes deposits before entering the line 21. The main metering valve 34 is disposed between the variable displacement pump 13 and the engine (not shown) for supplying fuel to the engine while maintaining a selected speed and pressure PM. The main metering valve 34 reliably increases the pressure PF from a substantially constant value PM, which is selected in advance. Suitable main metering valves 34 are well known in the art. Therefore, detailed explanation is not given here. A preferred main metering valve 34 serves to selectively change the amount of fuel passing therethrough. The metering valve 34 receives the fuel that maintains the pressure PF, and the fuel flows out at the pressure PM.
Line 35 connects the discharge of variable displacement pump 12 to bypass pressure control valve device 36. The flow rate in the line 35 is referred to as the outflow return flow rate that maintains the pressure PP. The regulator valve device 36 includes a housing 38 that forms an interior that incorporates a spring-biased spool 40 operatively disposed therein. The left side of the spool 40 has fuel that exerts a pressure PF thereon. A metering head adjustment screw 42 is attached to the spool 40 to calibrate the position of the spool 40 in the adjustment valve device 36 during flow rate setting. The housing 38 forms an inlet 44 connected to the line 35 for receiving fuel at pressure PF. The other inlet 46 of the housing 38 receives fuel that maintains the pressure PM from the static line 37 to slow the operation of the spool 40. An orifice 48 is placed in line 37 for slow operation. The housing 40 also forms an outlet 50 that restricts fuel exiting the regulator valve device 36. This outlet 50 is in fluid communication with line 28 of variable displacement pump 12 through line 51. Line 51 also connects to a low reference pressure PAF, in which orifice 52 limits the flow rate to a low reference pressure PAF. The pressure in line 51 is approximately equal to the average of PF and PAF, which in the following description refers to temporary pressure P12. The balance of the differential pressure between the PF acting on the left side of the housing 40 and the PM acting on the right side to which the bias amount by the spring of the spool 40 is added finally positions the spool 40.
During operation in a steady state, the left side of the control valve device 36 and the right side of the cam actuator 20 maintain substantially the same pressure. The recirculation flow rate through the regulator valve device 36 is kept low in pressure by a spool 40 that blocks a portion of the outlet 50 and the flow control system 10 can respond quickly and sufficiently to transient events. In the preferred embodiment, during normal operation, the spool 40 in the regulator valve device 36 is held in a substantially normal position. In the newest engines, the changes in fuel demand that occur with engine operation are relatively small compared to the variations associated with engine rotation.
When a transient phenomenon occurs, the variable displacement pump 12 must quickly deliver a large amount of fuel. For example, the transient phenomenon is an actuator operation using a rotational drive source having a pressure P1W in the line 21. In response to a transient increase in fuel demand, the main metering valve 34 is opened to immediately increase the fuel flow rate to the engine, and a series of operations to increase the discharge amount of the variable displacement pump 12 starts. Since the variable displacement pump 12 cannot immediately respond to the increase in the discharge rate, the increase request flows from the outflow return flow rate of the line 35. As a result, the pressure PM increases and the pressure PF decreases (that is, the pressure difference (PF-PM) before and after the main metering valve 34 decreases). The regulating valve device 36 senses the differential pressure, and the spool 40 moves to the left. The pressure at the outlet 50 decreases, while the pressure acting on the left side of the cam actuator 20 decreases. The piston 18 moves to the left due to a decrease in pressure acting on the left side of the cam actuator 20. When the piston 18 moves to the left, the discharge amount of the variable displacement pump 12 increases. This increased pump discharge increases the pressure PF until the differential pressure across the main metering valve 34 returns to the standard steady state and the steady condition is achieved again.
In an alternative embodiment, the variable metering pump 12 closes the main metering valve 20 to reduce the fuel flow to the engine when the discharge must be quickly reduced, preventing excessive fuel recirculation, A series of operations for reducing the discharge amount of the variable displacement pump 12 starts. Since the variable displacement pump 12 cannot immediately respond to the decrease in the discharge amount, the flow control system 10 responds immediately. That is, the decrease request causes a decrease in the pressure PM and an increase in the pressure PP (that is, an increase in the differential pressure (PF-PM) before and after the main metering valve 34). The regulating valve device 36 senses an increase in the differential pressure, and the spool 40 moves to the right. As a result, the pressure at the outlet 50 increases, while the pressure acting on the left side of the cam actuator 20 increases. The piston 18 moves to the right due to the increase in pressure acting on the left side of the cam actuator 20. When the piston 18 moves to the right, the discharge amount of the variable displacement pump 12 decreases until the differential pressure (PF-PM) before and after the main metering valve 14 returns to the normal steady state where the spool 40 is approximately at the standard position.
In short, the regulator valve device 36 is used to minimize the recirculation flow rate while allowing the flow control system 10 to respond quickly to transient demands. The recirculation flow rate is adjusted and the position of the spool 40 is at a normal position during operation at steady state. A pressure approximately equal to the average of the low reference pressure and the pump discharge pressure is used for setting by the control valve and cam actuator.
While the invention has been described in terms of a preferred embodiment, it will be readily appreciated that various changes and / or modifications can be made by those skilled in the art without departing from the spirit or scope of the invention as defined in the appended claims. be able to.

Reference is made to FIG. 1 so that those skilled in the art to which the present invention pertains will readily understand how to practice the invention and how to use it.
1 is a schematic representation of a flow control system constructed in accordance with the present invention.

Claims (22)

A highly stable flow rate control system for controlling a variable displacement pump,
A metering valve in fluid communication with the variable displacement pump for metering pump discharge;
A regulating valve device for maintaining a differential pressure before and after the metering valve;
An actuator connected to the variable displacement pump for setting the discharge of the variable displacement pump,
The regulator valve device accepts a portion of the pump discharge of the variable displacement pump as a bypass flow rate that maintains a first pressure, and the valve output from the regulator valve device is temporarily equal to the average of the first pressure and the low reference pressure. Maintaining pressure,
A highly stable flow rate control system in which the actuator receives a valve output and thus pump discharge to determine a setpoint value of the actuator. The fuel metering unit according to claim 1, wherein the second pressure in the actuator exerts a pressure opposite to the temporary pressure. The fuel metering unit of claim 1, wherein the second pressure is approximately equal to a temporary pressure during operation in a steady state. The fuel metering unit of claim 1, further comprising a filter in fluid communication with the discharge side of the variable displacement pump to remove deposits. 2. The fuel metering unit according to claim 1, further comprising a first line connected between a metering output side of the metering valve and the control valve in order to make a response of the control valve device moderate. 6. The fuel metering unit according to claim 5, wherein the first line is a static line. The fuel metering unit according to claim 5, further comprising an orifice in the first line. 6. The fuel metering unit according to claim 5, further comprising a second line connected between the control valve device and the cam actuator for applying a temporary pressure to the cam actuator. The fuel metering unit according to claim 1, wherein the actuator includes a piston connected to a movable cam ring of the variable displacement pump. A fuel metering unit that controls a variable displacement pump that receives a fuel that maintains a low reference pressure and generates a high-pressure discharge.
First means in fluid communication with the variable displacement pump for metering the discharge of the variable displacement pump;
Second means in fluid communication with the first means for maintaining a constant differential pressure across the third means and generating a temporary pressure approximately equal to the average of the high pressure and the low reference pressure;
Third means operatively connected to the variable displacement pump for controlling the discharge rate of the variable displacement pump;
A fuel line connected between the discharge side of the variable displacement pump and the third means for applying an opposing pressure to the third means;
The fuel metering unit, wherein the set value of the third means is based on a differential pressure between the temporary pressure and the opposing pressure. 11. The fuel metering unit according to claim 10, wherein the fuel metering unit is connected to a low reference pressure so that a temporary pressure and an opposing pressure are equal while the fuel line operates in a steady state. 11. The fuel metering unit according to claim 10, wherein the first means is a metering valve. The fuel metering unit according to claim 10, wherein the second means is a control valve. 11. The fuel metering unit according to claim 10, wherein the third means is a cam actuator. 11. The fuel metering unit of claim 10, further comprising a filter in fluid communication with the discharge side of the variable displacement pump to remove deposits. 11. The fuel metering unit according to claim 10, further comprising first means connected between the metering output side of the first means and the third means in order to moderate the response of the third means. The fuel metering unit according to claim 15, wherein the first means is a static line. The fuel metering unit according to claim 15, further comprising an orifice in the first means. 11. The fuel metering unit according to claim 10, further comprising a second line connected between the third means and the second means in order to moderate the response of the second means. A method of metering a variable displacement pump that supplies fuel to an engine, the step of receiving fuel that maintains a low reference pressure into the variable displacement pump;
Boosting the fuel with the variable displacement pump so that the discharge of the variable displacement pump becomes high pressure;
A process of measuring the discharge amount of the variable displacement pump with a metering valve;
Generating an effluent return flow from the discharge of the variable displacement pump to respond quickly when the engine requires additional fuel;
The process of adjusting the differential pressure before and after the metering valve using the control valve,
Adjusting the discharge amount of the variable displacement pump using a cam actuator connected to the cam ring of the variable displacement pump to adjust the discharge amount,
The regulator valve is in fluid communication with the outlet return flow rate so that the regulator valve generates a temporary pressure approximately equal to the average of the outlet return flow rate and the low reference pressure;
A method in which the cam actuator receives a temporary pressure to determine a setting value for the cam actuator. 21. The method of claim 20, further comprising the step of applying a second pressure to the cam actuator opposite the temporary pressure. 21. The method of claim 20, further comprising the step of slowing the response of the regulator valve by directing the metering output of the metering valve to the regulator valve.

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