US2117105A - Device for regulating the running of injection engines at different speeds of revolution - Google Patents

Device for regulating the running of injection engines at different speeds of revolution Download PDF

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US2117105A
US2117105A US17758A US1775835A US2117105A US 2117105 A US2117105 A US 2117105A US 17758 A US17758 A US 17758A US 1775835 A US1775835 A US 1775835A US 2117105 A US2117105 A US 2117105A
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revolution
fuel
engines
regulating
engine
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US17758A
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Schimanek Emil
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2700/00Mechanical control of speed or power of a single cylinder piston engine
    • F02D2700/02Controlling by changing the air or fuel supply
    • F02D2700/0269Controlling by changing the air or fuel supply for air compressing engines with compression ignition
    • F02D2700/0271Controlling the air supply as well as the fuel supply

Description

May), 1938. scHlMANEK 2,117,105
DEVICE FOR REGULATING THE RUNNING OF INJECTION ENGINES AT DIFFERENT SPEEDS OF REVOLUTION Filed April 25, 1935 2 Sheets-Sheet l May 10, 1938. E. SCHIMANEK DEVICE FOR REGULATINGEHE RUNNING 3F INJECTION ENGINES AT DIFFERENT SPEEDS OF REVOLUTION Filed April 23, 1935 2 Sheets-Sheet 2 Patented May 10, 1938 UNITED STATES DEVICE FOR REGULATING THE RUNNING F INJECTION ENGINES AT DIFFERENT SPEEDS 0F REVOLUTION Emil Schirnanek, Budapest, Hungary Application April as, 1935, Serial No. 17,758 In Austria July 13, 1934 2 Claims.
This invention relates generally to internal combustion engines.
It is known that in internal combustion engines the power is determined by the speed of 5 revolution and by the quantity of fuel that can be burned in the cylinder during a power stroke. The quantity of fuel that can be burned at any one time in the cylinder is, however, limited by the quantity of air or the quantity of oxygen 0 present in the cylinder. With engines operating with variable speeds of revolution, for instance vehicle engines, the quantity of air filling the cylinder is less at higher speeds of revolution tion.
In the case of explosion engines the quantity of fuel introduced into the cylinder is proportional to the quantity of air admitted to the cylinder, as in such engines a mixture of air and fuel is introduced or drawn by suction into the cylinder. Hence at lesser speeds of revolution, an increase in the quantity of air means a greater increase in the quantity of fuel entering the cylinder at each suction stroke or working cycle than at higher speeds.
In the case of injection engines, such for instance as Diesel engines, the fuel to be introduced in one stroke is delivered by the fuel pump independently of the quantity of air passing intothe cylinder. In vehicle engines of this kind the regulation of the fuel delivery is mostly effected by hand. The greatest quantity of fuel which can be adjusted for by this hand regulation is however in the case of all Diesel engines limited by a stop or the like, In vehicle engines operating on the Diesel principle with fuel injection this stop and consequently also the quantity of fuel highly heated by compression. The maximum quantity of fuel which can be introduced in one stroke remains unchanged at all speeds of revolution and consequently the maximum torque also remains unchanged at all speeds of revolution. In the case' of mixture engines, however, the maximum quantity of fuel used up in one stroke is not constant but changes proportionatethan at lower speeds at a given throttle posi- 1y to the quantity of air drawn in by suction with a fixed throttle position.
The fact that in a Diesel engine the maximum torque is invariable has great disadvantages when such injection engines are used as vehicle 5 engines. Such engines lack the elasticity which is characteristic of the mixture engines. In measuring the elasticity of an engine the product of two factors is controlling. The first factor is determined by the amount of change, which the 10 maximum torque shows when the speed of revolution changes; and the second factor is determined by the ratio between the greatest and the smallest speed of revolution at which the engine can still be operated properly. Measured in this 15 Way, however, the elasticity of Diesel engines is equal to zero, because the first factor is equal -to zero.
The present invention is based on the fact that even with injection engines, such as Diesel en- 2 gines, an elasticity can be obtained which is equal to that obtainable with mixture engines, ifthe two factors which determine the elasticity, when changing the speed of revolution, are changed in the same manner as in mixture engines. Thus, a change of the torque in injection engines, which corresponds to the change of the torque when changing the speed of revolution, can be obtained by regulating the maximum quantity of fuel introduced per stroke or per cycle into the power 30 cylinder at the different speeds of revolution in dependence on the quantity of air introduced into the motor cylinder at the speed of revolution at any particular time. In such a manner the maximum quantity of fuel at smaller speeds cl 3.; revolution is increased to correspond to'the greater quantity of air entering the cylinder during a cycle and vice versa. In other words, the maxi-' mum quantity of fuel introduced per stroke into the cylinder is varied each time in accordance ill with the change of the volumetric emciency, that is, in each case in accordance with the change in the quantity of air drawn in, as for instance by a suction stroke.
Such a method, which is based substantially 45 on a regulation of the maximum power of the engine at smaller speeds of revolution, also enables (this forming a further feature of the in-.- vention) the second of the factors mentioned above to be correspondingly enlarged in considerto ably reducing the smaller speed of revolution at which the engine can still be operated. The result is that as a vehicle engine the Diesel engine is at least equivalent to the mixture engine as to its elasticity. The minimum speed of revolution 55 of a motor is limited in that it must in any case be so great that the live force stored in the flywheel can overcome the work of compression without the motor experiencing a drop in the speed of revolution of the engine, which would detrimentally affect the proper running of the engine. Now as the work of compression depends on the final compression pressure, this final pressure is determined in the case of Diesel engines by the requirement of the self-ignition of the introduced fuel, and, therefore, amounts to a multiple of the final compression pressure of the mixture motors. The fly-wheel must also be made several times larger and heavier than that of mixture motors, if the smallest speed of revolution, at which the engine can still be operated, is to be the same. With the known Diesel engines for vehicles, a separate centrifugal governor is mostly provided, which prevents a drop below the speed of revolution determined by the mass of the fly-wheel and the work of compression.
An object of the present invention is to reduce this minimum speed of revolution, at which the engine can still operate properly. The invention makes use of the fact that by diminishing the quantity of air entering the cylinder (for instance by throttling) the work of compression in the cylinder can be reduced without the final temperature of the compression being lowered, so that such a diminution of the quantity of air is also a means for reducing the speed of revolution at which the engine can still operate properly. The compression temperature is dependent both on the initial temperature (temperature before the compression) and on the degree of compression. Now, as is known, a throttling in no way influences the initial temperature. The initial temperature of the compression thus remains the same and, as the degree of compression (that is to say, the ratio of the stroke volume to the 'volume of the compression space) remains the same, the compression temperature corresponding to normal operation is also reached at the compression pressure reduced by throttling. Hence according to the invention at loads or at powers lying below the maximum powers the quantity of air also is reduced in accordance with the quantity of fuel reduced in accordance with the smaller power, with the result that the final pressure of the compression can be reduced to nearly the final pressure of the mixture motors and thereby also the speed of revolution, at which the engine can still operate properly can be reduced in the same ratio.
' flihus, according to the inventionthe elasticity of Diesel engines is raised on the one hand by increasing the maximum power at smaller speeds of revolution, this being eifected by increasing the maximum fuel supply at smaller speeds of revolutlon in dependence on the excess of air at the smaller speeds of revolution and on the other hand by reducing the minimum speed of revolution at which the engine can still operate, in reducing, at the smaller powers which are obtained by reducing the quantity of fuel, the quantity of air along with the quantity .of fuel.
In the drawings, Fig. 1 is a view of a device showing the improvements in accordance with the invention for raising the maximum torque and reducing the minimum speed of revolution.
Fig. 2 is a view partly in section and partly in diagram of a device embodying another form of improvements for raising the maximum torque.
Fig. 3 is a view partly in section and partly in armies another form of improvements for raising the maximum torque and. reducing the minimum speed of revolution.
According to Fig. 1. a centrifugal governor is used for regulating the quantity of fuel for increasing the maximum power at smaller speeds of revolution. Member J is a lever'which can be swung downwards by hand or bypedal and which is arranged to pivot about the fixed shaft K and is connected by means of a rod Q to themember for regulating the fuel pump indicated generally at P. A suitable means for raising and lowering the rod B, such as the cam or eccentric is shown. The lever J, which is a bell crank, is influenced by the spring R which draws the lever upwards, the arrangement being such that, when the lever under the action of the spring R bears against the stop F, the fuel pump delivers the minimum quantity of fuel. The maximum quantity delivered by the fuel pump is limited by the contact surface T of a wedge 0, against which the stop P of the lever J strikes. The wedge O is guided in a guide S, but so as to be capable of moving freely upwards and downwards.
In Fig. 1 the wedge is shown approximately in its middle position. The position of the wedge O is determined by the centrifugal governor L, to
which it is connected by the lever N.
As the speed of revolution increases the sleeve M of the governor moves upwards and the wedge O downwards, the maximum quantity of fuel thus being reduced. With the motion in the opposite direction the maximum quantity of fuel which can be delivered by the pump is increased. The back T of the wedge is so shaped that the regulation of the maximum quantity of fuel corresponds to the quantity of air drawn by suction in each case at this position of the regulator or at this speed of revolution. This quantity of air can be determined for each speed of revolution by a single test for each type of engine, for instance by measuring the final pressure of the suction or the compression.
In the constructional example of the invention shown in Fig. 2, the regulation is effected by the vacuum created in the suction pipe. At greater speeds of revolution the air flows through the suction pipe at greater velocity and therefore produces a greater vacuum in the same. By transmitting this vacuum to the member for limiting the maximum quantity of fuel an automatic regulation of the limiting is obtained.
In Fig. 2 J is the lever which is acted on by a tension spring R and according to its position regulates the output of the fuel'pump P. The wedge is in this case connected to the piston Z which is capable of moving freely upwards and downwards in the cylinder Y. The piston Z is forced downwards by the spring X. The cylinder Y is connected through the pipe W with the sucthe cylinder as possible. As the speed of revolution of the engine increases the vacuum at V becomes greater. By this -means the piston Z is moved upwards in opposition to the spring X and the limiting of the lever motion and with it the maximum fuel pump qitput is altered.
This mode of regulation is particularly suitable in cases in which, when regulating the maximum power of the Diesel engine for the different speeds of revolution, at the same time at smaller powersthe quantity of air is also varied in accordance with the quantity of fuel introduced in each case. For enabling both regulations to be effected -tion pipe U at V. This point V should be as near simultaneously, the arrangement may be made such, when a centrifugal governor in accordance with Fig. 1 is employed, that the member which serves the purpose of displacing the throttle for the purpose of reducing the power displaces the limiting of the stop for the lever J, for instance, through the fulcrum K of this lever being moved upwards when throttling, as is indicated in Fig. 1 by broken lines, the quantity of air thus being regulated with the quantity of fuel. The throttle D is moved by means of the lever A which is connected by the rod B to the fulcrum K, which latter can move freely upwards and downwards in a guide (not shown). 15
In the constructional example shown in Fig. 2, the connection of the pipe W must lie at a point V of the suction pipe, lying behindthe throttle D which is shown in broken lines.
In the constructional example shown in Fig. 3, a governor is used which acts on the air throttling member and the fuel pump. In this arrangement it is also sought to reduce the compressing work required for starting the engine, without however thereby diminishing the compression temperature. Use is made, in this case, of the above mentioned fact that the compression temperature is dependent on the one hand on the initial temperature (temperature before compression) and on the other hand on the degree of compression, whereby the compression temperature corresponding to normal operation can be reached even at the compression pressures reduced by throttling. In the example shown in Fig. 3, by means of a starting regulator, which acts on the air throttling member and the fuel pump, the quantity of air drawn in by suction is first reduced during the starting period to such an extent that it is only slightly greater than the quantity of air corresponding to the quantity of fuel required for maintaining the idle running of the engine. At thesame time, the fuel pump is adjusted so as to deliver a slightly greater quantity of fuel than the quantity of fuel required for idle running, the arrangement being such that, corresponding to the increasing acceleration of the'engine, the regulating member constantly reduces the throttling of the suction air and alters the delivery of the fuel pump in the manner required for reaching the full speed of revolution of the engine. In the example shown in the drawings such a regulator serves in place of the regulator L shown in Fig. 1 and also serves the further purpose of regulating the maximum power at different speeds of revolution.
The governor l is connected by the lever 2;
which is pivoted at the point l8, and the bar 3 to a regulating body 4 for the quantity of fuel, this regulating body acting through a profile 5 which is determined by experiment. The regulating body 4 is connected on the one hand'by a bar 6 with a lever I and ion the other hand by lever II] in certain positions of the bell crank lever l.
The profile 5 coacts with a roller l'l mounted on a bar It, the bar llibeing connected in. a manner not shown in the figure with the member regulating the output of the fuel pump.
.This arrangement operates as follows:
When the engine is stationary the governor is in the position marked I. At the speed of revolution, at which the throttling action which is effective at starting ceases, that is, when the throttle is in its entirely open position (shown in the drawing by heavy lines), the governor is in the position marked II. (In this position all parts are shown in the drawing in heavy lines.) During the change of position from -I to II the throttle valve is displaced from its closed position I, which corresponds to the smallest speed of revolution, by the bar l3 ,or the spring l5 into the entirely open position II.
For the better understanding of the invention let it be assumed that the engine is running at 1000 revolutions per minute. The position 11 is assumed as occuring for instance at 300 revolutions, that is, at that speed of revolution at which the fiy-wheel already overcomes the entire compression work.
The position III of the governor corresponds to the maximum speed of revolution 1000.
While the governor is swinging from the position II into the position III only the regulating body 4 for the quantity of fuel is displaced and by means of the profile 5 the maximum quantity of fuel for the particular speed of revolution is correspondingly regulated.
The position II of the throttle valve coincides with the position III, when the lever in resting on the head 9 cannot be further displaced by the spring l5.
On the speed of revolution of the engine tending to increase because the load becomes smaller, the governor will swing from the position III towards the position IV and the fuel regulating body 4 will diminish the quantity of fuel, while the lever l displaces the bar 8 upwards and closes the throttle valve. i
I'claim:
1. A fuel regulating apparatus comprising a governor, a fuel pump, an air supply pipe with a throttle therein, a bar operatively connected to the governor, a movable member connected to the bar having a profile surface thereon, said profile surface being formed to vary the adjustment of the fuel pump, means connecting said surface to said pump and means of connection between said profile member and the throttle, said latter means consisting of a bar connected to the profile member, a bell crank lever connected to said bar, a second bar connected to said profile member, a lever connected to said second bar, said latter lever being operatively connected to the throttle and a floating bar interposed between said bell crank lever and said latter lever for actuating the same whereby the position of said throttle is simultaneously adjusted by said profile member. 1
2. A fuel regulating apparatus as claimed in claim 1 characterized by means for guiding the movement of the floating bar.
mam scmmusx.
US17758A 1934-07-13 1935-04-23 Device for regulating the running of injection engines at different speeds of revolution Expired - Lifetime US2117105A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2530741A (en) * 1946-02-11 1950-11-21 Diesel Power Inc Diesel engine idling control
US2865164A (en) * 1954-04-14 1958-12-23 Worthington Corp Air fuel control for two-cycle turbocharged spark ignition gas engines
US3074472A (en) * 1960-08-29 1963-01-22 Bendix Corp Fuel feeding system for gas turbine engines
US3269378A (en) * 1964-09-26 1966-08-30 Bosch Gmbh Robert Apparatus in controlling the supply of fuel to a combustion engine
US4221192A (en) * 1978-06-26 1980-09-09 Cummins Engine Company, Inc. Fuel injector and common rail fuel supply system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2530741A (en) * 1946-02-11 1950-11-21 Diesel Power Inc Diesel engine idling control
US2865164A (en) * 1954-04-14 1958-12-23 Worthington Corp Air fuel control for two-cycle turbocharged spark ignition gas engines
US3074472A (en) * 1960-08-29 1963-01-22 Bendix Corp Fuel feeding system for gas turbine engines
US3269378A (en) * 1964-09-26 1966-08-30 Bosch Gmbh Robert Apparatus in controlling the supply of fuel to a combustion engine
US4221192A (en) * 1978-06-26 1980-09-09 Cummins Engine Company, Inc. Fuel injector and common rail fuel supply system

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