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Publication numberUS2310773 A
Publication typeGrant
Publication dateFeb 9, 1943
Filing dateJan 26, 1940
Priority dateJan 27, 1939
Publication numberUS 2310773 A, US 2310773A, US-A-2310773, US2310773 A, US2310773A
InventorsOttavio Fuscaldo
Original AssigneeOttavio Fuscaldo
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Electromagnetically controlled fuel injection
US 2310773 A
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Description  (OCR text may contain errors)

Feb. 39, 1943. o. FUSCALDO ELECTROMAGNET I CALLY' CONTROLLED FUEL INJECTION Filed Jan. 26, 1940 2 Sheets-Sheet 1 INVENTOR O/fawo Fusca/do.

(m/w, Gm-lab? ATTORNEYS Feb. 9, 1943. r 0. FUSCALDQ 2,310,773

ELECTROMAGNETICALLY CONTROLLED FUEL INJECTION Filed Jan. 26, 1940 2 Shets-Sheet 2 T1 :i .4; I 57 Z9 INVENTOR 1 0/7 //0 Fusca/db BY D1 Kwwwb ATTORNEYS.

.Pat ented Feb. 9, 1943 ELECTROMAGNETICAILY con'rnonnm FUEL INJECTION Ottavio Fuscaldo, Milan, Italy; vested in the I i Alien Property Custodian I Application January 26, 1940, Serial No. 315,734

In Italy January 27, 1939 2 Claims.

This invention relates to electromagnetically controlled fuel injection, and its general object is to deliver automatically a constant air-fuel ratio under all operating conditions of explosion 'engines fed by electromagnetic fuel injection.

The mechanism of the present invention in its illustrated embodiment comprises in combination a series of electromagnetic injectors, at least one volumetric fuel-pump for feeding liquid fuel to said injectors, a device for gauging the fuel-flow placed as a bypass between the suction pipe and the pressure pipe of said pump, means for adjusting said gauging device through a pressure responsive instrument, and means which is controlled by the engines speed for influencing the electric circuit breaker which controls the ener-' gizing of the winding of the electromagnetic injector.

The invention will now be described with reference to the attached drawings, given solely by way of an example.

Fig. 1 is a View, substantially diagrammatic, of an embodiment of the device as applied to an explosion engine.

Fig. 2 is a portion of Fig. 1, showing details.

Fi 3 is a central section view of the electromagnetic injector of Fig. 1.

Fig. 4 is a longitudinal central section view of the current distributor of Fig. 1; and Fig. 5 is a right end view of Fig. 4 with the cover plate omitted.

1 shows an electromagnetically controlled injector I, which may be one of a series, energized from battery l5 and supplied under pressure from one or more fuel pumps 5, through pipes 9. Each injector may be constructed as in Fig. 3, wherein the solenoid winding 30, in circuit with the battery or current source I5 can attract the spring-resisted core 3! which pulls the injector valve and rod 32 to open the valve and cause each injection; the liquid flow and spring pressure closing the valve when the coil circuit is broken. This construction is the subject of copump extends a bypass passage back around the pump and adapted to permit backfiow of fuel not passing'to the valves I; and in this passage is arranged a controller 8 for varying the delivery, in-

dependently of the pump speed. Pump 5 draws the fuel from the tank I through the pipe 8 and 55 sends it to the injector l or to the series of injectors feeding the various cylinders of the engine. The bypass controller or valve 6 is varied in its action by a pressure responsive device, as a manometric Sylphon-capsule or bellows til, the interior of which is in constant communication by a small pipe H with the engine intake conduit 2|, leading to the usual inlet valves. The bellows device, thus responsive to intake pressure or suction. controls the bypass 6 by means of a link l2, piv

oted to a lever I3, fulcrumed at l3, so as to reduce the fuel volume flow, by discharging, into the inlet pipe 8 from pipe 9 in increased fraction of the fuel pumped, with the decrease of the absolute pressure of feed-air, i. e. with the increase of suction; and vice versa. I The timing of current distribution to the injectors I may be by means of a distributor M of a type that contains means for varying the angular closing time of the contacts, as for instance that shownin Figs. 4 and 5 containing features disclosed in copending applications and not herein claimed. The distributor It has a shaft 35 which is driven from and intime with the engine shaft and carries a cam 36 of shape to swing a 7 contact arm 31 in proper coordination. The arm carries an insulated contact 38 which is connected by a conducting strip 39 to a terminal post 60. The strip may be also a spring pressing arm 37 to close contact 38 against an opposing contact M. The cam 35 therefore causes the contact 38 to separate from and return .to the contact 4!, to break and make the circuit. The contact ll while relatively fixed is operatively adjustable, for c which purposeit is mounted on an extension or' car 152 outstanding from an adjustably movable plate 63. This plate may swing slightly and for convenience is shown pivoted to the same stud or pin at about which the contact arm 31 oscillates. Adjustments of plate 43 and contact 4! are effected by an eccentric "25 on a shaft 46, the eccentric occupying snugly a slot in the plate. The shaft fit carries an arm 4'! for efiecting these adjustments, and this arm, as shown in Fig. 1, is adjustably swung under control from the engine speed so that the higher the speed the longer the angular period of current flow in each cycle.

The electric current may flow through the circuit from battery l5, when the master switch It is closed. A centrifugal regulator ll, driven by the engine, operates through a lever l9 and link l8 to swing-the arm ll of the distributor M,

thereby to vary the angular period of closure of the contacts in each cycle in direct relation to the speed of theengine which period is therefore made substantially constant in point of time.

It is manifest that if the angular timing of closure of the contacts remains constant at all speeds, the actual timing, or period of time, varies evidently in inverse ratio to the engine running speeds consequently in that case an increase in speed of the engine increases also the fuel pressure in the injectors, as the actual time during which the injection is operative diminishes, while the volume flow in the pump must increase, the latter being of the volumetric type. Therefore, while the fuel feed pressure is very low at the start, it becomes very high at the highest speeds of the engine; this causes an excessive drop in the volumetric efficiency of said pump (because the leakage increases in all existing gaps and crevices), and causes also a rapid wear of the pump (with consequent increase in said gapsand leakage), resulting in a great reduction in the flow factor of the injection nozzles and a quicker erosion of the. same (owing to the increase of the discharge velocity), as weli as too penetrating an injection (causing the atomised fuel to strike against the walls and build up large drops) and a greater diiilculty in keeping the pipes and fixtures perfectly tight. These difilculties it is an object of the present invention to overcome. r I

The inclusion of a centrifugalgovemor in the present combination of elements substantially eliminates all of the stated inconveniences, by annulling their cause, namely the undue increase in injection pressure. In fact, while the volumetric pump'provides automatically a volume of fuel which is proportional to the engine's speeds, the centrifugal governor provides auto-'- matically a way to maintain the time of injection substantially constant, so that the pressure of the fuel also remains constant.

The device of this invention operates as folair throttle 20 constantly open) are imposed by load changes,.as is the case with the power curve, the amount of fuel and of air for each feed stroke of the engine remain constant and therefore the fuel-air ratio remains constant, -as desired.

The slight decrease in the intake of air into the cylinders which unavoidably occurs on'increasing the speed of the engine, caused by the increase of friction in the intake pipe 21, causes in its turn a slight increase in the depression in-said inlet pipe and therefore also in the manometric bellows or capsule Ill, which responsively shortens and, acting on the by-pass 6 of the pmnp, causes its delivery to' decrease.

When the changes in the sp ed of the engine are brought about by changes in the volume of feed-air, through the adjusting action of the throttle 20, as the case may be when working on the utilization curve, then the manometric bellows l undergoesan extreme action, because in this case the change in the depression is very great. The more the throttle 20 is closed, the

' tended of the variations of the absolute air lows: When changes in the engine's speed (with w feeding pressure. In order to fulfill the general requirement that the entire range of variation in the length of the bellows may cause in the distributor the complete range of variation in the length of time of contact closure, it issufflcient that the bellows should be of proper dimensions and properly adjusted for the purpose.

Considering now the performance of the system in sudden changes of engine speed (accelerations or decelerations) it should be noted that upon a quick opening of the throttle, whereupon the cylinders are immediately and completely filled with air, the fuel feed tends to lag, as it can only increase in consequence of the engine's acceleration, that is; of the pump's and governors increase. in speed. But this lag is somewhat reduced because the simultaneous decrease ing with the pipe 9.. During the normal running conditions the fuel in said chamber maintains a certain level above whichthere is a cushion of compressed air at the same pressure. The actign of this refinement will now be explained.

Supposing the engine to be running at slow speed, on opening quickly the throttle, the air inflow to the engine is complete and rapid as stated above, and the reserve of fuel contained in chamber 22, urged by the air pressure above it, feeds partly into pipe 9 and so provides the fuel needed to allow the engine to accelerate sufficiently to allow in turn the pump to increase its delivery, while the automatic closure of the by-pass helps out. When conditions become settied the fuel reserve in chamber 22 refills auto matically and rapidly, affording a cushioned auxiliary supply.

If the air throttle be closed suddenly, what happens is that, while the feed of the air ceases immediately and almost completely, the pumped fuel goes on feeding in a large measure, as it with electromagnetic injection is exclusively obtained by cutting-oil the current from the injectors. At this exact moment, the fuel pressure in the piping 9 rises, because the injectors have closed, while the pump goes on running awhile, although at a decreasing speed. In the connection from inverted chamber or flask 22 to the pipe 9 is a'cock 23 to cut of! the communication. Now, if at the instant the engine'stops the cock 23 is closed, cutting oi! the communication of chamber'22 with pipe 9, it will be possible to keep stored in thecha'mber a quantity of fuel under pressure; and this will prove useful for an easy restarting of the engine, even after a rather long stop, and without any other outside help. It will be sufficient to open at the proper moment the cock 23 while the engine is running only slowly, or is driven by the starting motor, and while the pump has yet too small a. delivery for full operation.

It should be understood that the details of construction, arrangement, design and application of the invention may be varied in many ways without thereby exceeding the scope of the invention.

Having now described my invention and ho the same is to be carried out, what I claim as my invention is:

substantially steady actual time duration of each injection; an engine-driven volumetric fuel pump delivering by its pressure pipe to the series of 1. Fuel injection apparatus for explosion engines, comprising a. series of valved fuel injectors injectors, adjustable means associated with the pump for modifying the rateof flow of pumped fuel to the-injectors, and a pressure-responsive capsule instrument in communication with and operated from the air pressure in the engine intake for adjusting said fuel-flow-modifying means and arranged to reduce the rate of fuel flow to the injectors with decrease of intake air pressure and vice versa; whereby the fuel injected into each cylinder in each cycle is proportioned substantially to the air inflow to maintain substantially steady the air-fuel ratio under varying intake pressures and engine speeds.

2 In an explosion engine fuel injection apparatus as in claim 1, a fuel passage extended laterally from the pump pressure pipe, a closed fuel reserve vessel to which said passage extends adapted to contain compressed air above the reserve fuel therein, and a cock in said passage to shut off and isolate said vessel and contained fuel and air; whereby on stopping the enginethe cock may be closed to seal and confine under pressure the liquid and air in the vessel, thereby to provide initial fuel pressure by opening the cock on restarting the engine.


Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2859741 *Sep 20, 1956Nov 11, 1958Edward R GlennFuel injecting apparatus
US2948272 *Nov 16, 1956Aug 9, 1960Bendix Aviat CorpFuel supply system
US3017873 *Jul 17, 1956Jan 23, 1962Gen Motors CorpFuel injection system
US3240191 *May 29, 1963Mar 15, 1966Ass Eng LtdFuel injection systems for internal combustion engines
US3662721 *Nov 6, 1969May 16, 1972Volkswagenwerk AgFuel injection device for internal combustion engines
US3724435 *Jan 29, 1970Apr 3, 1973Holley Carburetor CoRemote metering system
US3796206 *May 26, 1972Mar 12, 1974Bosch Gmbh RobertPump-and-nozzle assembly for injecting fuel in internal combustion engines
US3921604 *May 30, 1972Nov 25, 1975Bosch Gmbh RobertFuel injection apparatus for internal combustion engines
US4014301 *Apr 14, 1975Mar 29, 1977Daimler-Benz AktiengesellschaftExternally ignited internal combustion engine with ignition chamber
US4030668 *Jun 17, 1976Jun 21, 1977The Bendix CorporationElectromagnetically operated fuel injection valve
US4057190 *Jun 17, 1976Nov 8, 1977Bendix CorporationFuel break-up disc for injection valve
EP0214522A1 *Aug 20, 1986Mar 18, 1987Hitachi, Ltd.Single or twin valve type fuel injection system
U.S. Classification123/473, 261/76
International ClassificationF02M69/30, F02M69/34, F02M51/02, F02M69/16, F02M69/44, F02M69/20
Cooperative ClassificationF02M51/02, F02M69/20, F02M69/44, F02M69/34
European ClassificationF02M69/20, F02M69/44, F02M51/02, F02M69/34