GB1560551A - Fluid flow control system - Google Patents

Fluid flow control system Download PDF

Info

Publication number
GB1560551A
GB1560551A GB92576A GB92576A GB1560551A GB 1560551 A GB1560551 A GB 1560551A GB 92576 A GB92576 A GB 92576A GB 92576 A GB92576 A GB 92576A GB 1560551 A GB1560551 A GB 1560551A
Authority
GB
United Kingdom
Prior art keywords
signal
flow
signals
responsive
generating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB92576A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB92576A priority Critical patent/GB1560551A/en
Priority to JP14667376A priority patent/JPS5285613A/en
Priority to IT1901577A priority patent/IT1085851B/en
Priority to DE19772700473 priority patent/DE2700473A1/en
Priority to FR7700349A priority patent/FR2337903A1/en
Priority to US05/889,424 priority patent/US4146051A/en
Publication of GB1560551A publication Critical patent/GB1560551A/en
Expired legal-status Critical Current

Links

Landscapes

  • Flow Control (AREA)
  • Pipeline Systems (AREA)
  • Feeding And Controlling Fuel (AREA)

Description

(54) FLUID FLOW CONTROL SYSTEM (71) We, LUCAS INDUSTRIES LIMITED, a British Company of Great King Street, Birmingham B19 2XF, do hereby declare the invention for which we pray that a patent may be granted to us and the method by which it is to be performed, to be particularly described in and by the following statement: This invention relates to flow control systems for gases, and in particular to such systems when intended for control of a fuel gas supply to a gas turbine engine.
According to the invention a gas flow control system comprises a variable flow metering device, means for generating a first signal which is a function of a desired gas flow through said device, means, responsive to the gas pressure upstream of said device and to the effective flow area of said device, for generating a second signal which is a function of a choked gas flow through the device, means, responsive to said upstream pressure and said flow area and also to a pressure differential across said device, for generating a third signal which is a function of an unchoked gas flow through the device, actuator means responsive to a difference between said first signal and either said second or third signals, for varying said effective flow area, and selector means, responsive to a predetermined level of the ratio of said pressure differential to said upstream pressure, for rendering said actuator means responsive either to said second or said third signal, whereby said actuator means can control said device in accordance with a difference between desired and actual gas flows either in an unchoked or a choked flow condition.
Embodiments of the invention will now be described, by way of example only and with reference to the accompanying drawings, in which: Figure 1 is a block diagram of a gas flow control system adapted to deal with both choked and unchoked gas flows to a gas turbine engine, Figure 2 shows diagrammatically, a metering valve forming part of the system of Figure 1, and Figure 3 is a block diagram of the electrical control circuit of Figure 2.
It is an object of the system shown in Figures 1 to 3 to provide a flow control system for a fuel gas supply to an engine, wherein the gas supply pressure may vary so as to result in either choked or unchoked flow through a metering orifice, and in which a regulating device for the gas supply, separately from the metering valve, is unnecessary.
As shown in Figure 1, a gas turbine engine 50 is supplied with gaseous fuel whose flow is regulated by a metering arrangement 51. The metering arrangement 51 is located in a fuel supply passage 52.
The metering arrangement 51 is responsive to a control signal on a line 53 from an electronic control circuit 54, shown in more detail in Figure 3. Control circuit 54 is responsive to a digital first signal QD, corresponding to desired fuel flow, and supplied on a line 55 from a computer 56. The computer 56 is responsive to operating parameters of the engine 50, for example engine speed N and combustion temperature T, and also to a signal S dependent on the setting of a power demand control for the engine 50.
A temperature-responsive device 57 is responsive to the temperature T of the gas in the passage 52 upstream of the metering arrangement 51 to supply, on a line 58, a signal proportional to 1/ VT.
A transducer 59 is responsive to the fuel pressure in the passage 52 upstream of the metering arrangement 51 to supply, on a line 60 a signal P proportional to this pressure. A further transducer 61 is responsive to the pressure difference across the metering arrangement 51 to supply, on a line 62 a signal Dp proportional to this pressure difference. The electronic control circuit 54 is responsive to the aforesaid signals 1/ VT, P, Dp on lines 58, 60, 62 respectively.
The metering arrangement 51 is shown in detail in Figure 2 and includes a main hydraulically-operated flow control valve 70 having an axially-slidable control element 71. Control element 71 is movable by a double-acting piston 72. Piston 72 is urged in opposite directions by pressures applied to respective lines 73, 74, these pressures being controlled by an electro-hydraulic valve 75 which is responsive to the control signal on line 53 from the circuit 54. Hydraulic supply pressure and return lines 76, 77 communicate with the valve 75 and with a hydraulic pressure source 78, the lines 76, 77 being interconnected by a relief valve 79. A displacement transducer 80 is responsive to the position of the control element 71 to provide, on a line 81 a signal A proportional to the gas flow area of the main flow control valve 70.The signal A is also supplied to the electronic control circuit 54. Upstream of the main flow control valve 70 is a shut-off valve 82.
For choked flow through a metering orifice: Mass flow QF =K2 AP/ffT (1) For unchoked flow: Mass flow
Where K. and K4 are constants dependent on the characteristics of the gas and.
Where PB=P-DP.
The electronic control circuit 54 is operable to provide a control signal on line 53, this control signal being derived from second or third signals which are respective functions of mass flow equation (1) or (2) above, dependent on whether the flow through the main control valve 70 is choked or unchoked. The Dresence or otherwise of a choked flow condition is dependent on the function Dp/P, and the control circuit 54 is responsive, in a manner to be described, to the value of this function to select the manner in which the control signal on line 53 is calculated.
Control circuit 54 includes an analog to digital converter 90 which is responsive to the signal on line 58 to provide, on a line 91, a digital signal proportional to 1/ Analog to digital converters 92, 93 are respectively responsive to the signals on lines 60, 62 to provide, on lines 94, 95 digital signals proportional to P and Dp.
A dividing circuit 96 is responsive to the signals on lines 94, 95 to provide, on a line 97, a signal proportional to Dp/P. A function generator 98 is responsive to the signals on line 97 to perform the calculation indicated at equation (3) above and to provide, on a line 99, a function signal proportional to the value of +e.
The signal on line 97 is also supplied to a discriminator circuit 100 which supplies an output signal on a line 101 when the value of Dp/P is greater than or equal to .47, which corresponds to choked gas flow. A square root calculator 108 is also responsive to the signals on line 97 to provide, on a line 109, an output signal corresponding to /Dp/P.
A store 102 has two locations whose contents can be set to selected values of the constants K2 and K4 in equations (1) and (2) above. These values may be read out as respective fourth and fifth signals on lines 103, 104.
An analog to digital converter 105 is responsive to the signal on line 81 to provide, on a line 106 a digital signal A corresponding to the flow area of the main control valve 70.
A first multiplying circuit 110 is responsive to the signals on lines 91, 94, 103, 106 to supply, on a line 111 an output corresponding to QF =K2 AP/ v'T. A second 1 multiplying circuit 112 is responsive to the signals on lines 91, 94, 99, 104. 106 and 109 to provide, on a line 113, an output corresponding to QF =K4 A +2 s/P.DP/s/T.
A circuit 120 is responsive to the signals on lines 106, 111 to provide, on a line 121, a second signal proportional to QF -A, for the choked flow condition. A further circuit 122 is responsive to the signals on lines 106, 113 to provide, on a line123, a signal proportional to QF -A for the unchoked flow condition. The reason for the introduction of the A term will later be made apparent.
In the presence of a signal on line 101, corresponding to choked gas flow, a selector circuit 124 permits the signal on line 101 the unchoked control signals on converter 125. In the absence of a signal on line 101 the unchoked control signals on line 123 pass to the digital to analog to converter 125.
Output signals from the converter 125 are supplied to one input of a comparator 126. The digital signals on line 55, corresponding to desired fuel flow QD are supplied via a digital to analog converter 127 to a second input of the comparator 126.
Operation of the electro-hydraulic valve 75 may be expected to be vary rapid and to cause correspondingly rapid movement of the main flow control valve 70. Since as indicated, the greater part of the operations performed by the control circuit 54 are digital, these operations, together with analog to digital, or digital to analog convnrsion, may take up to 20 milliseconds to complete, during which time the control element 71 of the valve 70 may have moved appreciably. Accordingly therefore the valve position signal A on line 81 is supplied to the comparator circuit 126, to provide a negative feedback control. The selected QF-A signal from the digital to analog converter 125 is subtracted from the feedback signal A and the result compared with the Ql, signal from the converter 127.The comparator circuit 126 is such that there is no output signal on the line 53 when the result of this latter comparison is zero, that is when Q=Q,.
The system thus provides, in either choked flow or unchoked flow conditions, as appropriate, an actual fuel gas flow which corresponds to demanded gas flow, without the need for an additional gas pressure regulating valve.
WHAT WE CLAIM IS: 1. A gas flow control system comprising a variable flow metering device, means for generating a first signal which is a function of a desired gas flow through said device, means, responsive to the gas pressure upstream of said device and to the effective flow area of said device, for generating a second signal which is a function of a choked gas flow through the device, means, responsive to said upstream pressure and said flow area and also to a pressure differential across said device, for generating a third signal which is a function of an unchoked gas flow through the device, actuator means responsive to a difference between said first signal and either said second or third signals, for varying said effective flow area, and selector means, responsive to a predetermined level of the ratio of said pressure differential to said upstream pressure, for rendering said actuator means responsive either to said second or said third signal, whereby said actuator means can control said device in accordance with a difference between desired and actual gas flows either in an unchoked or a choked flow condition.
2. A system as claimed in Claim 1 which includes means for generating a signal dependent on a temperature of said gas, said means for generating said second and third signals being dependent on said temperaturedependent signal.
3. A system as claimed in claim 1 or claim 2 which includes means for generating fourth and fifth signals which are dependent on predetermined characteristics of the gas, said means for generating the second and third signals being respectively responsive to said fourth and fifth signals.
4. A system as claimed in Claim 3 in which said means for generating the second and third signals comprise respective first and second multiplying circuits.
5. A system as claimed in any preceding claim which includes means responsive to said ratio of said differential and upstream pressures for generating a function signal characteristic of an unchoked flow through said device, said means for generating the third signal being responsive to said function signal.
6. A gas flow control system substantially as hereinbefore described with reference to the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (6)

**WARNING** start of CLMS field may overlap end of DESC **. circuit 122 is responsive to the signals on lines 106, 113 to provide, on a line123, a signal proportional to QF -A for the unchoked flow condition. The reason for the introduction of the A term will later be made apparent. In the presence of a signal on line 101, corresponding to choked gas flow, a selector circuit 124 permits the signal on line 101 the unchoked control signals on converter 125. In the absence of a signal on line 101 the unchoked control signals on line 123 pass to the digital to analog to converter 125. Output signals from the converter 125 are supplied to one input of a comparator 126. The digital signals on line 55, corresponding to desired fuel flow QD are supplied via a digital to analog converter 127 to a second input of the comparator 126. Operation of the electro-hydraulic valve 75 may be expected to be vary rapid and to cause correspondingly rapid movement of the main flow control valve 70. Since as indicated, the greater part of the operations performed by the control circuit 54 are digital, these operations, together with analog to digital, or digital to analog convnrsion, may take up to 20 milliseconds to complete, during which time the control element 71 of the valve 70 may have moved appreciably. Accordingly therefore the valve position signal A on line 81 is supplied to the comparator circuit 126, to provide a negative feedback control. The selected QF-A signal from the digital to analog converter 125 is subtracted from the feedback signal A and the result compared with the Ql, signal from the converter 127.The comparator circuit 126 is such that there is no output signal on the line 53 when the result of this latter comparison is zero, that is when Q=Q,. The system thus provides, in either choked flow or unchoked flow conditions, as appropriate, an actual fuel gas flow which corresponds to demanded gas flow, without the need for an additional gas pressure regulating valve. WHAT WE CLAIM IS:
1. A gas flow control system comprising a variable flow metering device, means for generating a first signal which is a function of a desired gas flow through said device, means, responsive to the gas pressure upstream of said device and to the effective flow area of said device, for generating a second signal which is a function of a choked gas flow through the device, means, responsive to said upstream pressure and said flow area and also to a pressure differential across said device, for generating a third signal which is a function of an unchoked gas flow through the device, actuator means responsive to a difference between said first signal and either said second or third signals, for varying said effective flow area, and selector means, responsive to a predetermined level of the ratio of said pressure differential to said upstream pressure, for rendering said actuator means responsive either to said second or said third signal, whereby said actuator means can control said device in accordance with a difference between desired and actual gas flows either in an unchoked or a choked flow condition.
2. A system as claimed in Claim 1 which includes means for generating a signal dependent on a temperature of said gas, said means for generating said second and third signals being dependent on said temperaturedependent signal.
3. A system as claimed in claim 1 or claim 2 which includes means for generating fourth and fifth signals which are dependent on predetermined characteristics of the gas, said means for generating the second and third signals being respectively responsive to said fourth and fifth signals.
4. A system as claimed in Claim 3 in which said means for generating the second and third signals comprise respective first and second multiplying circuits.
5. A system as claimed in any preceding claim which includes means responsive to said ratio of said differential and upstream pressures for generating a function signal characteristic of an unchoked flow through said device, said means for generating the third signal being responsive to said function signal.
6. A gas flow control system substantially as hereinbefore described with reference to the accompanying drawings.
GB92576A 1976-01-10 1976-01-10 Fluid flow control system Expired GB1560551A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB92576A GB1560551A (en) 1976-01-10 1976-01-10 Fluid flow control system
JP14667376A JPS5285613A (en) 1976-01-10 1976-12-08 Gas flow control equipment
IT1901577A IT1085851B (en) 1976-01-10 1977-01-04 FLUID FLOW CONTROL SYSTEM
DE19772700473 DE2700473A1 (en) 1976-01-10 1977-01-07 GAS FLOW CONTROL SYSTEM
FR7700349A FR2337903A1 (en) 1976-01-10 1977-01-07 FLUID FLOW CONTROL DEVICE
US05/889,424 US4146051A (en) 1976-01-10 1978-03-23 Fluid flow control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB92576A GB1560551A (en) 1976-01-10 1976-01-10 Fluid flow control system

Publications (1)

Publication Number Publication Date
GB1560551A true GB1560551A (en) 1980-02-06

Family

ID=9712938

Family Applications (1)

Application Number Title Priority Date Filing Date
GB92576A Expired GB1560551A (en) 1976-01-10 1976-01-10 Fluid flow control system

Country Status (5)

Country Link
JP (1) JPS5285613A (en)
DE (1) DE2700473A1 (en)
FR (1) FR2337903A1 (en)
GB (1) GB1560551A (en)
IT (1) IT1085851B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2175120A3 (en) * 2008-10-08 2017-10-18 General Electric Company Method and system for operating a turbomachine having an unchoked valve

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1588124A (en) * 1976-10-28 1981-04-15 Lucas Industries Ltd Gas flow control system
JPS5636493Y2 (en) * 1977-06-28 1981-08-28
JPS5929700Y2 (en) * 1977-06-28 1984-08-25 三菱レイヨン株式会社 Dental restorative component processing equipment
DE3700898A1 (en) * 1987-01-14 1988-07-28 Herion Werke Kg Flow control valve
DE102008032565A1 (en) 2008-07-11 2010-01-14 Rolls-Royce Deutschland Ltd & Co Kg Fuel supply system for a gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2175120A3 (en) * 2008-10-08 2017-10-18 General Electric Company Method and system for operating a turbomachine having an unchoked valve

Also Published As

Publication number Publication date
DE2700473A1 (en) 1977-07-14
IT1085851B (en) 1985-05-28
FR2337903A1 (en) 1977-08-05
JPS5285613A (en) 1977-07-16
FR2337903B1 (en) 1981-11-27

Similar Documents

Publication Publication Date Title
US4146051A (en) Fluid flow control system
US4171613A (en) Device for controlling the rotational speed of turbo-jet engines
GB1560551A (en) Fluid flow control system
US2933894A (en) Fuel proportioning dual fuel system
US3041822A (en) Nozzle control for turbojet engine
US2990847A (en) Fluid flow regulator
US4380148A (en) Device for adjusting gas turbine engine fuel control system in accordance with engine parameter
US3587230A (en) Gas turbine engine control apparatus
GB1058927A (en) Improvements in fuel control devices for gas turbine engines
US4505293A (en) Fluid flow control valve
Ioannou et al. A time headway autonomous intelligent cruise controller: Design and simulation
US3820321A (en) Acceleration control for gas turbine engine
US3979682A (en) Hysteresis compensator for control systems
GB1588124A (en) Gas flow control system
US3085556A (en) Rate signal generator
Martin Flow saturated step response of a hydraulic servo
Yepifanov Aircraft turbine engine automatic control based on adaptive dynamic models
US3323308A (en) Constant flow, variable area hybrid engine injector
GB1170505A (en) Fuel System and Electrical Control therefor
Taiwo Design of multivariable controllers for an advanced turbofan engine by Zakian’s method of inequalities
MK et al. Valvistor based modern servo package
US3084675A (en) Hydraulic computer system
US2941359A (en) Control system controlling one output variable and providing limits for other outputs
GB1520300A (en) Fluidic control apparatus for aircraft fuel systems
US3131863A (en) Method and apparatus for limiting a regulating impulse

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee