The fuel supply system ensures the filtration of fuel and its uniform distribution across the engine cylinders in metered portions at strictly defined moments

The engine uses a split-type fuel supply system consisting of a fuel tank, low-pressure fuel lines, coarse and fine fuel filters, fuel pumping and fuel pumping pumps, a high-pressure fuel pump, high-pressure fuel lines, injectors, an electromagnetic valve and pin candles of an electric flare device (EFU).

The fuel tank, the coarse fuel filter and the fuel pump must be installed on the product on which the engine is used, all other elements of the power system are installed directly on the engine.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The diagram of the engine fuel supply system is shown in Figure 1.

Fuel from the fuel tank 26 through the coarse filter 29 and the fuel pump 30 is supplied by the fuel pump 18, through the fuel tube 13 to the fine filter 16.

From a fine filter, through a low-pressure fuel tube 14, fuel enters the fuel injection pump 21, which, in accordance with the order of operation of the cylinders, distributes fuel through high-pressure fuel lines 1-8 to the injectors 10.

Injectors inject fuel into the combustion chambers.

Excess fuel, and with it the air entering the system through the bypass valve 24 and the valve 23 is discharged into the fuel tank.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The nozzle of the model 273-20 or 273-50 of a closed design, with five spraying holes and hydraulic control of the lifting of the spray needle is shown in Figure 2.

All parts of the nozzle are assembled in the housing 6. The nozzle housing 1 is pressed against the lower end of the nozzle housing with a nut 2 through a spacer 3, inside which there is a needle 12. The housing and the nozzle needle make up a precision pair.

Angular fixation of the sprayer body relative to the spacer and spacer relative to the nozzle body is carried out by pins 4. A spring 11 exerts pressure on the upper end of the sprayer needle through the rod 5.

The necessary tension of this spring is carried out by a set of adjusting washers 9, 10, installed between the spring and the end of the inner cavity of the nozzle body.

Fuel is supplied to the nozzle under high pressure through a nozzle 8 with a slot filter 13 built into it, then through the channels of the housing 6, spacer 3 and the atomizer housing 1 - into the cavity between the atomizer housing and the needle 12 and, lifting it, is injected into the engine cylinder.

The fuel that has leaked through the gap between the needle and the atomizer body is diverted through channels in the nozzle body and drained into the tank through drainage tubes 9 and 11, shown in Figure 1.

The nozzle is installed in the cylinder head, fixed with brackets, which are fixed with a nut. The end of the sprayer nut is sealed against gas breakthrough with a corrugated copper gasket.

O-ring 7 (Figure 2) eliminates dust ingress

and liquids into the cavity between the nozzle and the cylinder head.

It is strictly forbidden to install injectors of other models

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The high-pressure fuel pump (Figure 3) is designed to supply strictly metered portions of high-pressure fuel to the engine cylinders at certain moments.

A fuel injection pump with an all-mode regulator is installed on the engine of the automotive configuration.

Characteristics of the fuel pump

Type 337

The order of the sections 8 - 4 - 5 - 7 - 3 - 6 - 2 - 1

The direction of rotation of the cam shaft (from the drive side) is right

Plunger diameter, mm 11

Plunger stroke, mm 13

Nominal speed of rotation of the cam shaft, min-1 1100

The speed of rotation of the cam shaft of the pump when the control lever of the regulator stops in the bolt of the maximum speed limit, min-1:

- when the fuel supply regulator is completely turned off after 1280

nozzles, no more

- at the beginning of the shutdown by the fuel supply regulator after 1140-1160

injectors

Preliminary stroke of the plunger (from the beginning of its movement to the geometric beginning of injection in the eighth section), mm: 5.65± 0.05

Alternation of the beginning of the fuel supply by the angle of rotation of the cam shaft, deg: - 0 - 45 - 90 - 135 - 180 - 225 - 270 - 315

The maximum force on the control lever of the regulator at the nominal operating mode of the pump on the shoulder is 50 mm, N (kgf) 127.5 (13)

Nominal cyclic feed, mm3/cycle:

- for FUEL INJECTION PUMP MODELS 337-20.03 132-137

- for FUEL INJECTION PUMP MODELS 337-20.04 147-152

Eight sections are installed in the fuel pump housing 1 (Figure 3), each of which consists of a housing 6, a plunger sleeve 8, a plunger 7, a rotary sleeve 4, a discharge valve 11, the seat of which is pressed against the plunger sleeve 8 by a fitting 12.

The plunger performs a reciprocating motion under the action of the cam shaft 46 and the spring 3 of the pusher.

The pusher from turning in the housing is fixed with a cracker 14. The cam shaft rotates in roller bearings 45 mounted in steel rings pressed into the pump housing and pressed with covers.

The tension of the cam shaft bearings should be 0.05-0.15 mm and is regulated by gaskets 44.

To change the fuel supply, the plunger 7 is rotated using a sleeve 4 connected through the leash axis to the pump rail 5. The rail moves in the guide bushings 40.

The holes for the guide bushings in the fuel pump housing on the drive side are closed with plugs 39. On the opposite side of the pump there is a fuel supply corrector according to the charge air pressure 24.

At the front end of the housing, at the place where the fuel exits the pump, a bypass valve 38 is installed, which provides pressure in front of the intake ports of the plungers at operating modes 0.13-0.19 MPa (1.3-1.9 kgf / cm2).

The lubrication of the pump is circulating, under pressure from the general lubrication system.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The fuel pump speed controller (Figure 4) is all-speed, direct acting, changes the amount of fuel supplied to the cylinders depending on the load, maintaining the set speed of the crankshaft.

The regulator is installed in the collapse of the fuel pump housing. On the cam shaft of the pump there is a driving regulator gear 16 (Figure 39), the rotation of which is transmitted through rubber crackers 17.

The driven gear is made at the same time with a holder of 28 loads rotating on two ball bearings.

When the holder rotates, the loads 31 swinging on the axes 29 diverge under the action of centrifugal forces and move the regulator coupling 32 through the thrust bearing 30, which, resting against the finger 34, in turn moves the levers 2, 8 and 9 of the regulator (Figure 4), overcoming the spring force 5.

Lever 2 is connected via a pin to the right rail 3 of the fuel pump. The right rail is connected to the left rail 11 through the lever of the rails 7.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The operation scheme of the speed controller is shown in Figure 5.

The control lever 16 of the regulator is rigidly connected to the lever 12. A regulator spring 13 is attached to the lever 12, and a starting spring 15 is attached to the levers 14 and 11.

During the operation of the regulator, the centrifugal forces of the loads are balanced by the force of the spring 13.

With an increase in the speed of rotation of the crankshaft, the loads, overcoming the resistance of the spring 13, move the levers 2,4 and 9, and with them the fuel pump rails - the fuel supply decreases.

When the speed of the crankshaft decreases, the centrifugal force of the loads decreases, and the levers with the fuel pump rail move in the opposite direction under the action of the spring force - the fuel supply and the speed of the crankshaft increase.

When the regulator lever 9 stops in the bolt 6 and the crankshaft rotation speed is less than 1800 min-1, the spring 10 of the direct corrector moves the pump rails (through levers 2 and 4) in the direction of increasing the fuel supply, providing the required amount of maximum engine torque.

The spring 3 of the reverse corrector at a speed of less than 1400 min‑1 moves the lever 4 with rails in the direction of reducing the fuel supply, limiting the maximum smokiness of the exhaust gases of the engine.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The fuel supply is stopped by turning the lever 3 (Figure 6) to stop the engine all the way into the bolt 5.

In this case, the lever 3, overcoming the force of the spring of the lever 33 (Figure 3) and the spring 5 (Figure 4), will turn the levers 2, 8 and 9 through the pin 14, the rails will move until the fuel supply is completely stopped.

The inspection and adjustment of the injection pump, as well as the replacement of plunger pairs, sealing rings of the injection pump sections must be carried out in a specialized workshop by a qualified specialist.

It is STRICTLY FORBIDDEN to install on the engines 740.50-360 and 740.51-320 fuel injection pumps of other models other than the above, in order to avoid engine failure!

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

Fuel supply corrector by charge air pressure (Figure 7).

The charge air pressure corrector reduces the fuel supply when the charge air pressure drops below 40-45 kPa (0.4-0.45 kgf/cm2), thereby providing thermal protection of the engine and limiting the smokiness of exhaust gases.

A piston 26 with a spool 2 is installed in the housing of the corrector 1. A spring 27 acts on the piston, fixed by a plate 25 and a ring 3.

A stud 29 with a tip 31, which is a nominal stop in the regulator, is wrapped and secured in the piston with a nut 28.

The tip is secured with a nut 30. A spring 7 acts on the spool 2, the pre-tension of which can be changed by the adjusting screw 11.

The housing of the membrane 8 is attached to the body of the corrector 1 through the gasket 4. A membrane assembly with a rod is installed in it (parts 24,16,17,23, 22, 19,18). The membrane is clamped between the housing 8 and the cover 21.

In the membrane housing 8, a corrector lever 12 is installed on the axis of the lever 13, the rotation of which is limited by the adjusting screw 15.

The fuel supply corrector is not direct acting: when the pressure of the charge air in the membrane cavity changes, the position of the spool changes, which, in turn, determines the position of the corrector piston.

In the cavity "A" between the corrector housing 1 and the piston 26, oil is supplied under pressure from the engine lubrication system through a threaded hole and a 0.7 mm jet in the corrector housing (not shown in the figure).

The piston under the influence of this pressure, compressing the spring 27, moves to the left until the windows in the piston and spool open and the oil goes to drain. At the same time, a constant oil consumption is established through the corrector.

When the position of the spool changes, the piston moves after it (the tracking system).

Air from the intake manifold of the engine is supplied to the membrane cavity through the threaded hole of the cover 21.

When the air pressure drops below 0.05 MPa (0.5 kgf/cm2), the force of the corrector spring 7 acting on the spool becomes greater than the force created by the pressure of the charge air on the membrane and transmitted through the diaphragm rod and the corrector lever also to the spool.

The spool moves to the right until there is a balance of forces acting on it.

Following the spool, the piston with the stud 29 and the tip 31 moves to the right, moving the regulator lever 8 resting on it to the right (Figure 4).

Following the regulator lever, under the action of the centrifugal forces of the loads, the levers 9.2 and 7 with the pump rails move in the direction of reducing the fuel supply.

Adjusting the corrector

The corrector has two external adjustments - screws 11 and 15 (Figure 7).

The screw 11 changes the pre-tension of the spring of the corrector 7, while changing the start of the operation of the corrector.

If it is necessary to increase the value of the charge air pressure at which the corrector starts to work, then the screw 11 is turned, increasing the pre-tension of the spring 7.

The nominal cyclic fuel supply is regulated by the screw 15. When the screw 15 is turned out, the fuel supply increases.

If there is a need to remove the corrector, then it is first necessary to measure the protrusion of the tip of the stud 31 relative to the rear end of the fuel pump housing, and after installing the corrector in place, restore the size of this protrusion and wipe the tip with a nut 30.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The fuel pump drive is shown in Figure 8. It consists of a fuel pump drive shaft 6 with packages of front 7 and rear 8 compensating plates, driven coupling half 2, driven coupling half flange 3, centering flange 4, driving coupling half 9 and centering bushings 5.

Each package of compensating plates consists of 5 plates with a thickness of 0.5 mm each.

All bolts in the fuel pump drive, except the bolt pos. 10, must be of strength class R100 and be tightened by a torque of 65-75 Nm (6.5-7.5 kgf m).

The tightening of all bolts must be controlled with a torque wrench. Before installing the bolts, check for centering bushings.

Deformation (bending) of the front and rear compensating plates is not allowed. The bolt 10 of the half coupling of the leading one should be tightened last of all with a torque of 78.4-84.3 Nm (8-8.6 kgf m).

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The fuel fine filter is shown in Figure 9. It is designed for the final purification of fuel from fine particles before entering the fuel injection pump.

The filter is installed at the highest point of the fuel supply system to collect and remove air into the tank along with part of the fuel through a valve (Figure 10) installed at the bypass from the filter.

When replacing filter elements, it is necessary to strictly observe the rules for servicing the fuel supply system. Do not allow contamination to enter the system and use filter elements only of the following models 740.1117040-01, 740.1117040-02, 740.1117040-04.90

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The valve is shown in Figure 10. When the pressure in the cavity "A" of the fuel supply reaches 25-45 kPa (0.25-0.45 kgf / cm2), the ball 4 moves and the fuel flows from the cavity "A" into the cavity "B" through the valve nozzle 5.

The fuel pump 13 (Figure 3) of the piston type is designed to supply fuel from the tank through coarse and fine filters and a fuel pump to the intake cavity of the injection pump.

The pump is mounted on the back cover of the regulator, its drive is carried out from the eccentric 19, located at the rear end of the cam shaft of the injection pump.

The pump housing contains a piston, a piston spring, a rod sleeve 47 and a pusher rod 48, inlet and discharge valves with springs.

The eccentric 19 through the roller 49, the pusher 15 and the rod 48 communicates reciprocating motion to the piston of the fuel pump.

The pump operation scheme is shown in Figure 11. When the pusher 9 is lowered, the piston 1 moves downwards under the action of the spring 4. A vacuum is created in the cavity "A" and the intake valve 2, compressing the spring 3, passes fuel into the cavity "A".

At the same time, the fuel located in the discharge cavity "B" is forced into the main line "G", while the valve 5 is closed under the action of the spring 6, excluding the flow of fuel from the cavity "B" into the cavity "A".

When the piston 1 moves upwards, the fuel filling the cavity "A" enters the cavity "B" under the piston through the discharge valve 5, while the intake valve closes.

When the pressure in the discharge line increases, the piston does not make a full stroke after the pusher, but remains in a position that is determined by the equilibrium of the fuel pressure force on the one hand and the spring force on the other.

 Конструкция подачи топлива в дизель KAMA3-740.50-360, KAMA3-740.51-320

The piston-type fuel pump 10 (Figure 11) is used to fill the fuel system with fuel before starting the engine and removing air from it.

The pump consists of a housing, piston, cylinder, inlet and discharge valves.

The fuel system should be pumped using the pump piston, having previously opened it by turning counterclockwise.

When the piston 11 moves upwards, a vacuum is created in the space under it. The intake valve 12, squeezing the spring 14, opens and the fuel enters the cavity "D" of the pump.

When the piston moves down, the intake valve closes and the discharge valve 13 opens, the fuel enters the discharge line under pressure, ensuring the removal of air from the engine fuel system through the fuel fine filter valve and the bypass valve of the fuel injection pump.

After pumping the system, it is necessary to lower the piston and fix it by turning clockwise. In this case, the piston will press against the end of the cylinder through a rubber gasket, sealing the suction cavity of the fuel pump.

It is not allowed to start the engine with an unfixed piston due to the possibility of air suction through the piston seal.

Fuel lines are divided into fuel lines of low pressure - 0.4-2 MPa (4-20 kgf / cm2) and high pressure more than 20 MPa (200 kgf /cm2).

The low-pressure fuel lines are made of steel pipe with a cross section of 10 mm with soldered tips.

High-pressure fuel lines of equal length (1 = 595 mm) are made of steel tubes with an internal diameter of 2 +0.05 mm by landing at the ends of connecting cones with crimp washers and cap nuts for connection with fuel injection pump fittings and injectors.

In order to avoid damage from vibration, the fuel lines are fixed with brackets to the intake manifolds.