GB2073464A - Engine-alternator sets - Google Patents
Engine-alternator sets Download PDFInfo
- Publication number
- GB2073464A GB2073464A GB8109838A GB8109838A GB2073464A GB 2073464 A GB2073464 A GB 2073464A GB 8109838 A GB8109838 A GB 8109838A GB 8109838 A GB8109838 A GB 8109838A GB 2073464 A GB2073464 A GB 2073464A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- alternator
- control system
- alarm conditions
- parameters
- 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.)
- Withdrawn
Links
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H7/00—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
- H02H7/06—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric generators; for synchronous capacitors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M1/00—Pressure lubrication
- F01M1/18—Indicating or safety devices
- F01M1/20—Indicating or safety devices concerning lubricant pressure
- F01M1/22—Indicating or safety devices concerning lubricant pressure rendering machines or engines inoperative or idling on pressure failure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B63/00—Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices
- F02B63/04—Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices for electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D17/00—Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling
- F02D17/04—Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling rendering engines inoperative or idling, e.g. caused by abnormal conditions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Control Of Eletrric Generators (AREA)
Abstract
An engine-alternator set 10 connected to an electrical load is controlled by a system having a facia 20 for displaying alternator (electrical) parameters 21, engine (non-electrical) parameters 22 respectively associated with alternator alarms and engine alarms, and status parameters 23 associated with manually-operable READY/RESET and START/STOP switches 23B, 23A. The control system incorporates preprogrammable logic which is responsive to a START signal to effect programmed start-up of the set 10 and which is responsive to preselected alarm conditions to shutdown the set 10 automatically. <IMAGE>
Description
SPECIFICATION
Engine-alternator sets
This invention relates to engine-alternator sets and to a control system therefor.
Engine driven alternator sets have a variety of applications. For example they may be used as a source of electrical power where a mains supply is not available, or, where a mains supply is available, they may provide an emergency back-up supply. In any event such sets require to be controlled both during start-up and normal running and the present invention is concerned with a control system which, after initiation, operates automatically to control the functioning of the engine-alternator set.
According to the present invention there is provided a control system for an engine-alternator set comprising means for sensing and displaying the electrical quantities generated by the alternator, means for comparing the sensed quantities with preset values to detect alarm conditions, means for sensing and displaying engine parameters, means for comparing the sensed parameters with preset values to detect alarm conditions, logic means responsive to a start signal to effect starting of the engine-alternator set and responsive to preselected alarm conditions arising to shut down the enginealternator set automatically.
Preferably the sensed engine parameters are oil pressure, water temperature, and speed; low oil pressure, high water temperature and high speed giving rise to said preselected alarm conditions.
Preferably also the sensed electrical quantities are frequency, voltage, amperage and wattage; low frequency, high voltage, high current, high wattage and reverse wattage giving rise to said preselected alarm conditions.
Said start signal may be manually generated or automatically generated upon detection of a mains failure.
An embodiment of the present invention will now be described by way of example with reference to the accompanying drawings, in which:
Figure 1 shows a typical electrical system incorporating a control system according to the present invention;
Figure 2 illustrates a module of the instrument panel of the control system;
Figure 3 illustrates the control logic of the module of Figure 2;
Figure 4 shows the control system in block diagram form;
Figure 5 illustrates a preferred form of one of the blocks of Figure 4; and
Figure 6 illustrates a preferred form of another block of Figure 4.
Figure 1 of the drawings illustrates a typical application of an engine-alternator set 10 as an emergency stand-by power supply for a load 11normally supplied by electrical mains 12. The set 10 is connected to the load 11 via an alternator contactor 13 which is normally open and the mains 12 is connected to the load via a mains contactor 14 which is normally closed. The set 10 comprises an engine 15 the output shaft of which drives an alternator 16. The electrical system is 3-phase and neutral.
The control system for the set 10 comprises a module which can be fitted as required to an instrument panel, the module facia 20 being shown in Figure 2. Facia 20 displays electrical parameters as a group 21, engine parameters as a group 22, and status parameters as a group 23.
Group 21 includes frequency, voltage, amperage and wattage meters 21A, 21 B, 21 C, 21 D respectively with a selector switch 21 E for selecting either line-to-line voltages or line-to-neutral voltages and a further selector switch 21 Ffor selecting step or hold of the displays on meters 21 B and 21 C. Additionally group 21 includes visual alarms for low frequency, overvoltage, overcurrent, power overload and reverse power 21 G, 21 H, 211, 21J and 21K respectively.
Group 22 includes meter 22A for display of engine oil pressure, engine water temperature, battery voltage, and accumulated hours run, with engine alarms sub-grouped (a) for starting (22B) viz. "no residual" meaning alternator voltage below 2V after 2 seconds with the starter engaged; "start failed" meaning starting sequences completed without alternator frequency reaching a preset frequency, say 34 Hz, (b) for warning (22C) viz. "water temperature" meaning high water temperature, "battery voltage" meaning low battery voltage, and "fuel low" meaning inadequate fuel supplies, and (c) for shut down (22D) viz. "low oil pressure", "high water temperature", "overspeed" meaning frequency greater than a preset value, say 70 Hz and "hand stop" meaning that the start/stop button has been operated during operation of the set 10.
Group 23 includes the start/stop button 23A, a ready/reset button 23B and visual status checks 23C viz. "mains return" which indicates return of the mains voltage when the alternator is running, "auto" which indicates selection of automatic start rather than manual start, "running" which indicates that the alternator is running, and 'panel outputs/c' which indicates an overload of the electronics of the control system.
The parameters of group 21 are taken from the alternator output by conventional sensors, the sensed analogue signals being converted to digital signals for the purpose of metering. The frequency meter has a nominal range of 50-60 Hz with a maximum of 75 Hz and an accuracy of +0.1 Hz. The low frequency alarm setting is typically 34 Hz and is non-operational until after successful start up. The voltage meter has a nominal range of either 110-125 or 220-250V between phase and neutral and a metering accuracy ofjl%F.S.D. +1 digit (RMS scaled average). Overvoltage alarm setting may be 130, 140, 150 or 260,280, 300V. The current meter has a nominal range of 0-5A (at the CT secondary) with a maximum of 1 0A and a metering accuracy of +1% F.S.D. +1 digit (RMS scaled average).The overcurrent alarm is set at 5A (at the CT secondary) for each phase. The watt meter has an accuracy of 1% F.S.D. +1 digit and the power overload is 3 x 120 x CT rating if 130, 140 or 150 overvoltage is selected and 3 x 240 x CT rating if 260, 280 or 300
overvoltage is selected. The reverse power alarm
setting is 5% of the power overload alarm.
The parameters of group 22 which are displayed
on meter 22A are taken from the engine by conven
tional sensors (transducers). The low oil pressure
alarm may be set at 10,20,30 or 40 psi, the warning
water temperature alarm at 205"F and the shut-down
water alarm at 210"F. The battery voltage may be in
the range 8-40V, metered with an accuracy of +0.3V
and the low battery voltage alarm may be set at 11V
for a nominal 1 2V battery,22V for a 24V battery, or
29.3Vfora 32V battery.
The various settings above mentioned are prog
rammed on screwdriver-adjustable switches which
are accessible at the rear of the module where all
input connections to the module are made. As will
be appreciated the control system module is multi
purpose and requires to be preset to suit a particular engine alternator set 10. Additionally, the module
includes control logic 30 (Figure 3) which controls
the operation of the module and various alternative
operational procedures are available from the con
trol logic and these require to be preset or pre
selected.These are:
1 or 3 attempt start
Duration of each start attempt
Delay between each start attempt (3 attempt start)
Delay between mainsfailure and automatic set
starting
Delay between mains return and alternator
contactor drop-out
Delay between successful start and closure of
alternator-contactor
If single start is selected the starter on time is set in
the range 8-80 seconds in steps of 8 seconds. If triple
start is selected the starter on time is selected as for
the single start and the off-time is set in the range
4-40 seconds in steps of 4 seconds. A successful start
is determined by alternator frequency exceeding the
preset value (typically 34 Hz) whereafter the alterna torcontactor is closed (provided the mains contactor
has dropped out) following a delay in the range 2-20
seconds set in steps of 2 seconds.The delay
between mains contactor return and alternator con
tactor drop-out is set in the range 0.2-2.0 hrs in steps
of 6 minutes.
As shown in Figure 3 the control logic 30 outputs
signal 30A to the engine starter solenoid, 30B to the
engine air intake solenoid, 30C to the engine fuel
valve, 30D to the alternator contactor, 30E to the
mains return indicator at 23C, 30Fto the electrical
alarms 216-21K, and 30G to the engine alarms 22B,
C and D. The inputs to the control logic 30 are
provided by the various programme options, the
operator's control buttons 23A, 23B together with
master control buttons for manual/auto selection
and startinhibitto be described latertogetherwith the previously described sensor signals.
In the manual mode the logic 30 operates as
follows:
Actuation of ready/reset button 23B energises the
power supply for the control system usually for a
duration of 15 seconds during which time start-up
can be initiated by actuation of the start/stop button
23A. Thus the output signals 30A-30C cause starting of the engine 15 according to the preselected programme option. After a successful start the starter solenoid signal 30A is disabled and signal 30D enabled in order to close the alternator contactor 13. The alternator is shut down by further actuation of the button 23A which disables signals 30B, C and D and after a 15 second time delay the power supply for the control system is disabled.
In the automatic mode actuation of ready/reset button 23B or detection of mains failure causes energisation of the power supply for the control system and the start-up procedure is undertaken automatically thereafter following a preset time delay in the range 2-20 seconds set in steps of 2 seconds. Following return of the mains supply the alternator contactor signal 30D is disabled and the alternator shut down automatically thereafter following a 30 second delay period.
In either the manual or automatic mode the operation of the set 10 is dependent upon the absence of an engine shut-down alarm as indicated on the module facia (Figure 2). Should any one of these alarms come into operation the set 10 is automatically shut down by logic 30. The alarm fault then remains in a latched condition and prevents a restart attempt until the ready/reset button 23B is actuated. Because the electrical alarms 21G-21Kare not very critical not all of these alarms need to operate in a latching manner but those which are set to do so are combined in the electrical alarm signal 30Fwhich inhibits a restart attempt until reset by button 23B.
The control system may also be operated to monitor the electrical parameters on the load side of the alternator contactor 13 by actuation of a master start inhibit switch. In this mode of operation the set 10 is inhibited from starting but the control system power supply is energised to permit metering of the electrical parameters.
Figure 4 is a simplified block diagram of the control system from which it will be evident that the battery used for restarting the engine 15 also energises the power supplies which in turn energise the remaining electrical components of the system.
All parameters are measured in analogue fashion and are converted to digital for display and control purposes. It will be noted that priorto display of voltage and current stepping controls are provided.
These controls are arranged to step repeatedly around the monitored electrical parameters so that, for example in the case of current the metered value is that of phase A, then phase B, then phase C, then phase A again, and so on. However, by actuation of switch 21 F (Figure 2) the stepping controls can be held on one metered value, e.g. the current of phase
B, and stepping is inhibited. The stepping control prior to the voltage display 21 B can be switched by switch 21 E (Figure 2) to monitor either line-to-line voltages or line-to-neutral voltages. These stepping controls are preferably of the kind described in our
U.K. Patent Specification No. 2057148A utilizing RCA type CD 4019 AND/OR select gates.
For the purpose of providing a remote indication of power generated the d.c. analogue output of a wattage computer is fed to a signal transmitter. This transmitter takes the form shown in Figure 5 which is fed with antiphase square wave voltages A,B whose amplitudes need not be well controlled. These square waves are each fed through a diode and CT coil of N1 turns to the collector of a common transistor the base current of which is provided by an operational amplifier. In one arrangement the emitter current of the transistor is forced by the action of the operational amplifier to the value of the input signal i. Consequently the transistor collector current is substantially equal to ii also and this current is drawn alternately from square waves A and B according to the polarity thereof.The driving mmf in the CT is therefore always proportional to i1 but its direction changes at the frequency of the waves A and B because of the winding arrangements of the CT coils. The CT has an output coil of N2 turns which feeds through a full wave rectifier to a load resistor R1 providing a current wherein. If the
CT has sufficiently high inductance it can be shown that iL = il ' N/N2 For improved accuracy the error introduced by the transistor base current can be reduced or eliminated by use of a Darlington connected transistor pair (or triple) or an FETtransistor. Alternatively, a second differential amplifier can be used to sense the actual transistor collector current, the output of this second differential amplifier then being level shifted to provide a differential voltage for the basic differential amplifier. A further alternative is to sense i1 via a further CT coil in the CT secondary circuit since the current through the secondary circuit is proportional to the CT mmf as is i1. In this case the output of the further CT coil would require to be rectified.
Figure 6 illustrates a form of analogue-to-digital converter that may be used on receipt of an analogue signal to be displayed provided by a conventional stepping controller. The analogue input signal (which is negative) is at terminal A of Figure 6 while the counter and display is supplied from terminal C and is controlled by an enabling signal LE and a reset signal R both supplied by a counter the only input of which is a clock signal of period P at terminal B. The counter is set with a count number N and generates a NxPtimeinterval between reset signal R rising and enabling signal LE rising.
A NOR latch is provided by NOR gates 5 and 6 coupled to a second counter whose output Y is at logic 0 (0 volts) if its input R is at logic 1 (+ V Volts) and when R falls to logic 0 output Y rises to logic 1
M x P later. The output x of gate 5 is fed back to the input of integrator 3 through a small value resistor
R2 so that if x is at logic 1 the integrator output ;Z falls. When Z reduces below the threshold of NOR gate 4 the next clock pulse at terminal B causes the
NOR latch to be set so that x becomes logic 0 and this situation remains until output Y of the second counter becomes logic 1. During the time that output
X is at logic 0 integrator output rises at a rate dependent on how negative the analogue signal A is and resets the NOR latch so that it is again at logic 1.
Integrator 3 does not draw any d.c. current compo
It can readily be shown that the number produced in the output counter is proportional to the input analogue voltage VA, the constant of proportionality comprising N/M SO that either or both of these values can be altered. This can be utilised in the wattmeter or ameter A/D converters of Figure 4 where it is necessary to correlate the digital read-out with the
CT ratio used to sense current. For example N/M can be changed in ratios 2,2.5,3 etc. which are BS standard CT rated primary current values.
Claims (7)
1. A control system for an engine-alternator set comprising means for sensing and displaying the electrical quantities generated by the alternator, means for comparing the sensed quantities with preset values to detect alarm conditions, means for sensing and displaying engine parameters, means for comparing the sensed parameters with preset values to detect alarm conditions, logic means responsive to a start signal to effect starting of the engine-alternator set and responsive to pre-selected alarm conditions arising to shut down the enginealternator set automatically.
2. A control sysem as claimed in claim 1, wherein the sensed engine parameters are oil pressure, water temperature, and speed; low oil pressure, high water temperature and high speed giving rise to said preselected alarm conditions.
3. A control system as claimed in claim 1 or claim 2, wherein the sensed electrical quantities are frequency, voltage, amperage and wattage; low from quency, high voltage, high current, high wattage and reverse wattage giving rise to said preselected alarm conditions.
4. A control system as claimed in any preceding claim, wherein a regulated power supply which is fed from the engine battery and said logic means is effective to start the engine after a time delay following said start signal during which said regulated power supply becomes stabilised.
5. A control system as claimed in any preceding claim, wherein said logic means forms part of a module incorporating optional programmes and presettable means are provided in the module to control said logic means to follow one of said optional programmes.
6. A control system as claimed in claim 5, wherein said optional programmes include single or multi attempt engine start; duration of starter on time; duration of interstart delay in the multi start option.
7. A control system as claimed in claim 1 and substantially as hereinbefore described with reference to the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8109838A GB2073464A (en) | 1980-04-01 | 1981-03-30 | Engine-alternator sets |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8010880 | 1980-04-01 | ||
GB8109838A GB2073464A (en) | 1980-04-01 | 1981-03-30 | Engine-alternator sets |
Publications (1)
Publication Number | Publication Date |
---|---|
GB2073464A true GB2073464A (en) | 1981-10-14 |
Family
ID=26275046
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8109838A Withdrawn GB2073464A (en) | 1980-04-01 | 1981-03-30 | Engine-alternator sets |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2073464A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2558566A1 (en) * | 1984-01-24 | 1985-07-26 | Bijur Lubricating Corp | CONTROL CIRCUIT OF A LUBRICATION DEVICE |
FR2745127A1 (en) * | 1996-02-21 | 1997-08-22 | Automation Et Dev Ind Du Sud | Automatic emergency generator control circuit for three=phase electrical networks |
EP0704612A3 (en) * | 1994-09-30 | 1998-11-25 | General Motors Corporation | Integrated small engine control |
US6664791B2 (en) | 2000-06-26 | 2003-12-16 | Snap-On Technologies, Inc. | Alternator tester with improved heat dissipation |
EP1422802A2 (en) * | 2002-11-25 | 2004-05-26 | Goodrich Control Systems Limited | A method of and apparatus for detecting sensor loss in a generator control system |
DE102010010360A1 (en) | 2010-03-05 | 2011-09-08 | Gamptec Gmbh | Taurolidine formulations and process for its preparation |
CN110164081A (en) * | 2018-02-13 | 2019-08-23 | 大唐国际发电股份有限公司陡河发电厂 | Generating set assists early warning system |
CN113217202A (en) * | 2021-05-26 | 2021-08-06 | 河南柴油机重工有限责任公司 | Diesel generator control system |
-
1981
- 1981-03-30 GB GB8109838A patent/GB2073464A/en not_active Withdrawn
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2558566A1 (en) * | 1984-01-24 | 1985-07-26 | Bijur Lubricating Corp | CONTROL CIRCUIT OF A LUBRICATION DEVICE |
GB2153570A (en) * | 1984-01-24 | 1985-08-21 | Bijur Lubricating Corp | Lubricating system control circuit |
US4674030A (en) * | 1984-01-24 | 1987-06-16 | Bijur Lubricating Corp. | Lubricating system control circuit |
EP0704612A3 (en) * | 1994-09-30 | 1998-11-25 | General Motors Corporation | Integrated small engine control |
FR2745127A1 (en) * | 1996-02-21 | 1997-08-22 | Automation Et Dev Ind Du Sud | Automatic emergency generator control circuit for three=phase electrical networks |
US6664791B2 (en) | 2000-06-26 | 2003-12-16 | Snap-On Technologies, Inc. | Alternator tester with improved heat dissipation |
US6777941B2 (en) | 2000-06-26 | 2004-08-17 | Snap-On Incorporated | Alternator testing method and system using timed application of load |
EP1422802A2 (en) * | 2002-11-25 | 2004-05-26 | Goodrich Control Systems Limited | A method of and apparatus for detecting sensor loss in a generator control system |
DE102010010360A1 (en) | 2010-03-05 | 2011-09-08 | Gamptec Gmbh | Taurolidine formulations and process for its preparation |
CN110164081A (en) * | 2018-02-13 | 2019-08-23 | 大唐国际发电股份有限公司陡河发电厂 | Generating set assists early warning system |
CN113217202A (en) * | 2021-05-26 | 2021-08-06 | 河南柴油机重工有限责任公司 | Diesel generator control system |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |