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GB1583770A - Internal combustion engine carburation systems - Google Patents

Internal combustion engine carburation systems Download PDF

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Publication number
GB1583770A
GB1583770A GB4122579A GB4122579A GB1583770A GB 1583770 A GB1583770 A GB 1583770A GB 4122579 A GB4122579 A GB 4122579A GB 4122579 A GB4122579 A GB 4122579A GB 1583770 A GB1583770 A GB 1583770A
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GB
United Kingdom
Prior art keywords
engine
pulses
circuit
fuel
ratio
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
GB4122579A
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.)
Societe Industrielle de Brevets et dEtudes SIBE
Original Assignee
Societe Industrielle de Brevets et dEtudes SIBE
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 Societe Industrielle de Brevets et dEtudes SIBE filed Critical Societe Industrielle de Brevets et dEtudes SIBE
Publication of GB1583770A publication Critical patent/GB1583770A/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M3/00Idling devices for carburettors
    • F02M3/08Other details of idling devices
    • F02M3/09Valves responsive to engine conditions, e.g. manifold vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/02Circuit arrangements for generating control signals
    • F02D41/14Introducing closed-loop corrections
    • F02D41/1438Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
    • F02D41/1486Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor with correction for particular operating conditions
    • F02D41/1488Inhibiting the regulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/12Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
    • F02M7/18Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice
    • F02M7/20Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves with means for controlling cross-sectional area of fuel-metering orifice operated automatically, e.g. dependent on altitude

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)

Description

PATENT SPECIFICATION
( 21) Application No 41225/79 ( 22) Filed 6 May 1977 N ( 62) Divided out of No 1 583 769 3 ( 31) Convention Application No 7614742 ( 32) Filed 14 May 1976 in X ( 33) France (FR) 1 f) ( 44) Complete Specification published 4 Feb 1981 ( 51) INT CL 3 G 05 D 11/13 ( 52) Index at Acceptance G 3 R A 23 A 24 A 625 BE 69 ( 54) IMPROVEMENTS IN OR RELATING TO INTERNAL COMB ENGINE CARBURATION SYSTEMS ( 71) We, SOCIETE INDUSTRIELLE DE BREVETS FT D'ETUDES S I B E, a French Body Corporate of 3 Villa Bergerat, 92200 Neuillysur-Seine, France, 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:-
The invention relates to internal combustion engine carburation systems of the kind comprising a main fuel circuit and at least one second "idling" or transfer circuit for supplying the engine with air-fuel mixture at a rate ensuring proper operation of the engine at low speed and low load.
According to the invention there is provided a carburation system for an internal combustion engine comprising at least one fuel circuit for supplying the engine with air-fuel mixture at a flow rate ensuring proper operation of the engine and a corrective system which comprises, in a fuel supply to the fuel circuit an electrically operated valve and closed loop regulation means for delivering electric actuating pulses to said valve, the ratio between the time length of the pulses and the time period between successive pulses being controlled in response to the composition of the exhaust gases of the engine associated with the carburation system, and means for opening the closed loop upon occurrence of predetermined operating conditions, and memory means for storing the value of said ratio at opening of the closed loop and for adjusting the ratio between the time length of the pulses and the time period between successive pulses at a value which is in poroportion to said stored value immediately after said opening.
The specification of our co-pending Application No 19149/77 (Serial No 1583769) discloses and claims a carburation system for an internal combustion engine comprising a main fuel circuit, at least one second circuit for supplying the engine with air-fuel mixture at a flow rate ensuring proper operation of the engine at low speed and low load, and a closed loop corrective system which comprises a first solenoid valve disposed in a fuel supply to the first circuit, a second solenoid valve disposed in a fuel supply to the second circuit, and means for delivering electric actuating pulses to said valves, the ratio between the time length of the pulses and the time period, between successive pulses being controlled in response to at least one engine operating parameter 55 An embodiment of the present invention is used in conjunction with the carburettor and X system disclosed in the above referred to copending Application, will now be described by way of example with reference to the accom 60 panying drawings in which: Figure 1 is a simplified vertical cross-section of a downdraught carburettor according to the above referred to co-pending Application No.
19149/77 (Serial No 1583769) 65 Figure 2 is a block diagram of an embodiment of an electronic circuit for controlling the solenoid valve of the main fuel circuit; Figure 3 is a simplified representation of part of the circuitry in the block diagram of 70 Figure 2.
Referring to Figure 1, there is shown a carburettor comprising an intake passage 1 having a main throttle means or butterfly 2 controlled by the driver via a linkage (not 75 shown) Passage 1 has an air inlet 3, usually provided with an air filter (not shown) The carburettor has a starting device which is not shown.
The main fuel circuit of the carburettor is 80 supplied with fuel from a float chamber 4 via one or more main calibrated nozzles or calibrated orifices In Figure 1, there are provided two main nozzles 5 a, Sb disposed in parallel.
Air for the fuel emulsion is provided by a cali 85 brated orifice 6 which takes air from inlet 3 via a duct 7 The air and fuel mix in a well 8 into which a conventional emulsion tube 9 projects, the tube having the calibrated orifice 6 at its top; A rich primary mixture is formed 90 inside tube 9 and flows out through duct 10 which opens at the throat 11 of a venturi 12.
The second circuit (idling and progression circuit) opens into intake passage 1 via ports 13, 14 and 14 a Port 13 is permanently down 95 stream of the edge of the main throttle means 2, whereas apertures 14, 14 a successively move from upstream to downstream of the edge when means 2 opens from its minimum opening position, which is adjusted by an abutment (not 100 ( 11) 1583770 1 583 770 shown).
Apertures 13, 14, 14 a are supplied with fuel through a channel 15 and a duct 16 whose inlet is connected either to well 8 (as shown by continuous lines in the drawing) or directly to the float chamber (as shown by broken lines).
In the first case, the fuel supplies to the main circuit and the second circuit are not completely independent, since the duct 16 supplying fuel to the idling circuit takes the fuel from well 8 downstream of the main nozzles Sa, Sb.
However, since the flow cross-sectional area controlling the flow rate in the second circuit is small compared with that of nozzles Sa and Sb, the interaction between the two circuits is very limited and usually acceptable If it is desired to make the circuits completely independent, the system represented by broken lines can be adopted.
Fuel is supplied to the second circuit by an idling nozzle 17 having a calibrated flow crosssection and located at the inlet of duct 16 The air for forming the air-fuel emulsion, which is subsequently introduced into the intake passage I via apertures 13, 14 and 14 a is supplied through an air intake 18 having a calibrated cross-section A screw 19 is provided for adjusting the amount of air-fuel mixture supplied by the idling circuit through aperture 13 downstream of butterfly 2.
The main nozzle Sb and the idling nozzle 17 are controlled by solenoid valves 20, 21 respectively It will be assumed hereinafter that when valve 20 or 21 is energized, it closes the corresponding nozzle Sb or 17 (a reversed control system being also acceptable) The frequency of the actuation of jets Sb and 17 and the time for which they are maintained in closed or actuated condition are determined by electric pulses for control means The control means shown in Figure 1 comprise an electronic circuit 22 which delivers pulses at a rate which may be either fixed or variable (but is sufficiently high to avoid unsteady operation), the ratio between the pulse length and period being determined by the value of one or more signals representing one or more respective engine operating parameters detected by one or more probes such as probe 23.
The electronic device 22 comprises a single probe 23 which provides e g a signal representing a physical or chemical property of the engine exhaust gases Device 22 can e g have a construction similar to that of the corresponding device described in French Patent Specification 2,228,158.
Alternatively, use can be made of a system adapted to receive a number of input signals representing engine operating parameters, some signals being representative of variation in the fuel supply rate, resulting in a closed looped system (examples of such parameters are the difference between the duration of successive engine cycles, the temperature of the exhaust gases, etc), whereas other parameters are independent (e g the ambient temperature or pressure) Alternatively, device 22 can be designed so that one of the signals has an overriding action under given engine conditions e g.
idling, whereas another signal preponderates when the engine conditions are different, e g.
maximum speed or deceleration.
In addition, different signals representing different parameters can be selected to control the main and the second circuit For example, device 22 and the connections between it and valves 20, 21 can be adapted so that valve 21, which controls the second circuit, receives electric pulses having a length-toperiod ratio determined by instabilities in engine operation, whereas solenoid valve 20, which controls the main circuit, receives electric pulses having a ratio determined by a probe detecting the characteristics of the engine exhaust gases.
The actuating means can be designed so that they control the richness and operate under "closed loop" conditions only under particular operating conditions of the engine.
The actuating means can for instance be designed to hold valves 20, 21 permanently open when the engine is under full load; for that purpose a pneumatically controlled contactor may be located between the output of device 22 and the input of valves 20 and 21, the contactor being connected to a suitable place along the intake pipe 1.
Referring to Figure 1, there is shown a contactor 24 comprising a pneumatic element connected by a pipe 26 to the throat 11 of venturi 12 The movable diaphragm of the pneumatic element carries a movable contact 27 and a return spring biases contact 27 against a fixed contact 28 to close a circuit between the output of device 22 and the solenoid valves 20, 21.
When the depression at throat 11 of venturi 12 becomes sufficiently high to overcome the force of the return spring, the diaphragm of the pneumatic element moves and separates the electric contacts 27 and 28, thus cutting off the electric power supply to the valves Nozzles Sb and 17 are then permanently open, so that the fuel supply cannot be controlled by reduction of the flow cross-section and the system operates under open loop conditions.
A substantially equivalent result can be obtained by replacing contactor 24 with contactor 25; then connections A' and B' of contactor 25 are substituted for connections A and B of contactor 24 Contactor 25 comprises a pneumatic element which is connected by a pipe 29 to pipe 1 downstream of butterfly 2.
The depression transmitted by pipe 29 tends to close contacts 30, 31 of contactor 25 against the action of a return spring During idling and low load, a considerable depression prevails downstream of butterfly 2 (which is then in its minimum opening position or in a partial opening position) and contactor 25 is closed Under full load, on the other hand, butterfly 2 is com1 583 770 pletely open, the depression transmitted by pipe 29 to the pneumatic element of contactor decreases and the return spring opens contacts 30, 31 This avoids any reduction in richness under full load, i e when maximum torque is required.
A single main nozzle can be used (i e by eliminating jet 5 a) or more than two jets can be provided, one jet being permanently open and the others being actuated by solenoid valves, if advisable in dependence on different parameters Each solenoid valve can have a seat which is distinct from the nozzle and disposed upstream or downstream thereof.
Referring now to Figure 2, there is shown the block diagram of a system according to the invention, adapted to fulfill several functions:
-under normal operating conditions, it constitutes a closed loop system which controls airfuel ratio for maintaining an acceptable exhaust gas composition; -under full load conditions, it constitutes an open loop system providing the air-fuel mixture enrichment necessary for obtaining maximum torque from the engine; -under acceleration conditions and while the engine is cold, it provides a fuel enrichment which is adjusted responsive to the rate of flow of fuel which was delivered to the engine immediately before acceleration begins.
For that purpose, the system illustrated in block form on Figure 2 comprises several circuits which will be described in succession.
A regulation circuit 35 for closed loop control has an input connected to an oxygen probe 23 located in the exhaust gas flow of the engine and which delivers an input signal to circuit 35.
A circuit 36 for modulated enrichment under acceleration conditions has its input connected to the output of circuit 35 The outputs of circuits 35 and 36 are connected to respective analog inputs of a selection circuit 37 A control input of circuit 37 receives a logic or binary signal which has a first predetermined level (which may be considered as a binary 1) if a temperature threshold circuit 39 indicates a temperature lower than a predetermined value and if simultaneously a micro-switch 41 indicative of acceleration conditions is closed and receives a signal at a second level (a binary zero) if either one or neither condition is fulfilled.
For that purpose, circuit 39 and a circuit 42 responsive to closure of switch 41 have their outputs connected to respective inputs of an AND gate 38 whose output is connected to the control input of 37 Circuit 37 is so constructed that if a binary one is received on the control input, the signal from circuit 35 is passed to the output; if a binary zero is received, the signal from 36 is passed to the output Circuit 37 may consist of a pair of analog gates.
The signal delivered from the output of circuit 37 is amplified at 48 and then fed to the solenoid valve 20.
Last, a circuit 43 is provided for opening the control loop when a micro switch 44 is open to indicate full load operation of the engine.
Referring now to Figure 3, an embodiment of the circuits referred to above will be described with more details.
The input element of the regulation circuit is the probe 23 which is typically a resistor associated with a voltage source for delivering to an amplifier 45 a signal representative of the oxygen content in the exhaust gases The oxygen probe is typically a probe comprising a body of electrolyte in solid form (Zr O 2 doped with yttrium oxide) and platinum electrodes.
When the amount of free oxygen in the exhaust gases decreases the voltage delivered by the probe increases, all the more since residual oxygen is used for oxidizing carbon monoxide on the surface of the probe with platinum operating as a catalyst.
The analog output voltage from 23 is amplified at 45 and applied to a first input of a differential amplifier 46 whose other input receives a reference voltage The switch 44 which closes responsive to the degree of vacuum which prevails in passage I under full load operation is located on a line from the first input to ground.
The output signal of amplifier 46, in the form of square pulses whose time length depends on the oxygen content of the exhaust gas, is applied to a first input of a second differential amplifier 47 via a normally closed movable contact 48 of a relay 49 The input is also connected to ground via a storage capacitor 50 and is connected by a diode 51 to the mid-point of a resistive voltage divider.
The other input of amplifier 47 receives a saw tooth signal from a circuit comprising an oscillator 72 and a triggered ramp generator 73 of conventional type.
The circuit 36 for temporary enrichment includes a differential amplifier 52 whose two inputs are connected to the output of amplifier 47 via two different branches The first branch comprises a single shot multivibrator 53 which delivers a short pulse responsive to the trailing edge of each output pulse from amplifier 47 and a switching transistor 54 As long as transisitor 54 is cut off, a current source 55 loads a capacitor 56 When transistor 54 is conducting, it unloads 56 to ground.
The second branch comprises an inverter 57 and a switching transistor 58 When the transistor 58 is cut off, a capacitor 59 is loaded by a current generator 60 and the voltage at the corresponding input of differential amplifier 52 increases.
The amplifier 48 receives an input signal from 35 via the rest contact of a switch 62 (actuated at the same time as switch 48) as long as coil 49 is not energized It receives an input signal from 36 when 49 is energized.
The coil of relay 49 is located in a circuit in series relation with the contact 64 of a first, temperature responsive relay which constitutes 1 583 770 circuit 39 with a differential amplifier and with the contact 65 of the second acceleration responsive relay 42 The coil of that relay is energized upon closure of a contact connected to the movable wall of a pneumatic element (Fig 2) A first chamber of the pneumatic element is connected to the induction passage I and the other chamber is connected to the first chamber by a restricted orifice; at rest, a return spring maintains contact 41 in open condition.
Operation of the device is as follows.
During closed loop operation (as illustrated in Figure 3), the square pulses delivered by amplifier 46 are directed to the storage capacitor 50 which unloads through the output impedance of amplifier 46 when the latter is blocked.
The differential amplifier 47 operates as a comparator and delivers a positive output pulse as long as the value of the saw tooth voltage is lower than the voltage across the electrodes of capacitor 50.
As long as contact 62 is in rest condition, the pulses from the output of amplifier 47 are directed to solenoid valve 20 and retain it in closed condition during short time durations at a rate which is determined by oscillator 72.
If the level of the voltage peaks from probe 23 increases due to insufficient contents of oxygen at the exhaust, the voltage across capacitor 50 increases, the output pulses from 47 are longer and the time periods of closure of valve 20 increase.
Under full load operation, switch 24 is closed and energizes its associated relay whose contact 44 grounds the input of amplifier 46.
Amplifier 47 remains blocked, the voltage across 50 decreases until a value which is determined by diode 51 and the associated voltage divider; the length of the pulses directed to valve 20 decreases to a value which provides the enrichment necessary to satisfactory full load operation.
During acceleration while the engine is cold, contact 64 is closed and switch 65 remains closed until pressure balance has been achieved across the diaphragm of pneumatic motor 67 by airflow across restricted orifice 68 (Fig 2).
Simultaneous closure of contacts 64 and 65 results in opening of contact 48 From that time on, the voltage across 50 will remain constant and will retain, at least temporarily, the last value before opening of 48 Consequently, there appears at the output of amplifier 47 square pulses of constant length.
During the positive square pulses of constant duration delivered by amplifier 47 and inverted by 57, transistor 58 is blocked and capacitor 59 is loaded under a constant current.
At the end of said constant duration, there occurs simultaneously: 60 -delivery of a short pulse by 53 which results in 54 becoming conductive and almost instantaneously reducing to zero the voltage across capacitor 56, which loads progressively again immediately after the end of the short 65 pulse.
-switching of 58 to conduction state, thereby unloading 59 and maintaining it in unloaded condition until a new positive square pulse increases 70 The values of the components are so selected that the voltage of 59 increases with time at a faster rate than that of 56; as soon as they are equal, the output of amplifier 52 becomes zero and solenoid valve 20 opens 75 Due to the memory effect of capacitor 50, the opening time of solenoid valve is increased with respect to the direct relation with the opening time before acceleration.

Claims (2)

WHAT WE CLAIM IS: 80
1 A carburation system for an internal combustion engine comprising at least one fuel circuit for supplying the engine with air-fuel mixture at a flow rate ensuring proper operation of the engine and a corrective system 85 which comprises, in a fuel supply to the fuel circuit an electrically operated valve and closed loop regulation means for delivering electric actuating pulses to said valve, the ratio between the time length of the pulses and the 90 time period between successive pulses being controlled in response to the composition of the exhaust gases of the engine associated with the carburation system, and means for opening the closed loop upon occurrence of 95 predetermined operating conditions, and memory means for storing the value of said ratio at opening of the closed loop and for adjusting the ratio between the time length of the pulses and the time period between successive pulses 100 at a value which is in proportion to said stored value immediately after said opening.
2 A carburation system according to Claim 1, wherein said memory means consists of a capacitor which is loaded under a voltage in 105 direct proportion with said ratio.
For the Applicants:
F J CLEVELAND & COMPANY, Chartered Patent Agents, 40-43 Chancery Lane, London WC 2 A l JQ Printed for Her Majesty's Stationery Office by MULTIPLEX medway ltd, Maidstone, Kent, ME 14 IJS 1981 Published at the Patent Office, 25 Southampton Buildings, London WC 2 IAY, from which copies may be obtained.
GB4122579A 1976-05-14 1977-05-06 Internal combustion engine carburation systems Expired GB1583770A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7614742A FR2351269A1 (en) 1976-05-14 1976-05-14 IMPROVEMENTS TO THE CARBURATION DEVICES FOR INTERNAL COMBUSTION ENGINES

Publications (1)

Publication Number Publication Date
GB1583770A true GB1583770A (en) 1981-02-04

Family

ID=9173198

Family Applications (2)

Application Number Title Priority Date Filing Date
GB4122579A Expired GB1583770A (en) 1976-05-14 1977-05-06 Internal combustion engine carburation systems
GB1914977A Expired GB1583769A (en) 1976-05-14 1977-05-06 Internal combustion engine carburatio systems

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB1914977A Expired GB1583769A (en) 1976-05-14 1977-05-06 Internal combustion engine carburatio systems

Country Status (5)

Country Link
AU (1) AU514616B2 (en)
DE (1) DE2721774C2 (en)
FR (1) FR2351269A1 (en)
GB (2) GB1583770A (en)
IT (1) IT1078128B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2012369B (en) * 1978-01-11 1982-05-12 Gen Motors Corp Carburettor and method of calibration
FR2419403A1 (en) * 1978-03-08 1979-10-05 Sibe Mixture control for IC engine carburettor - has fuel pipe for enrichment dividing to issue into venturi throttle section and air channel
GB2193537A (en) * 1986-08-04 1988-02-10 Ford Motor Co I.c. engine fuel metering system
FR2625262B1 (en) * 1987-12-23 1992-12-11 Solex ELECTRIC SLOW MOTION CARBURETOR

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD80589A (en) *
US2747561A (en) * 1954-05-06 1956-05-29 Gen Motors Corp Anti-detonating carburetor
US3690305A (en) * 1968-10-04 1972-09-12 Hitachi Ltd Fuel supply control system for automobile engines
DE1900930A1 (en) * 1969-01-09 1970-09-03 Josef Schwarz Interrupt impulse-controlled electronic speed monitor to shut off the idle jet by means of an electromagnetically controlled shut-off valve on petrol carburetors
US3661366A (en) * 1971-03-01 1972-05-09 Cletus W Shinkle Fluid cleaning and cooling apparatus and method
DE2246625C3 (en) * 1972-09-22 1982-02-18 Robert Bosch Gmbh, 7000 Stuttgart Fuel metering system
JPS5153131A (en) * 1974-11-01 1976-05-11 Nissan Motor Kikaki
US3986352A (en) * 1975-05-08 1976-10-19 General Motors Corporation Closed loop fuel control using air injection in open loop modes

Also Published As

Publication number Publication date
FR2351269A1 (en) 1977-12-09
AU2516777A (en) 1978-11-23
IT1078128B (en) 1985-05-08
DE2721774C2 (en) 1984-08-09
FR2351269B1 (en) 1981-04-17
AU514616B2 (en) 1981-02-19
GB1583769A (en) 1981-02-04
DE2721774A1 (en) 1978-01-19

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