c18-diesel-elec-map

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Shutdown SIS Previous Screen Product: GENERATOR SET Model: C18 GENERATOR SET LXK01006 Configuration: C18 Generator Set LXK00001-UP Systems Operation C13, C15, and C18 Generator Set Engines Media Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014 i03522261 General Information SMCS - 1000 These engines are in-line six cylinder engines. The engines have a firing order sequence of 1, 5, 3, 6, 2, 4. The rotation of these engines is counterclockwise when the engine is viewed from the flywheel end. These engines utilize two turbochargers and an air-to-air aftercooler. The Electronic Unit Injector system (EUI) eliminates many of the mechanical components that are traditionally used in the fuel injector assembly. The EUI also provides increased control of the timing and increased control of the fuel air mixture. The timing advance is achieved by precise control of the fuel injection timing. Engine speed is controlled by adjusting the injection duration. The engine has built-in diagnostics in order to ensure that all of the components are operating properly. In the event of a system component failure, the operator will be alerted to the condition by a check engine light. The check engine light is located on the control panel. An electronic service tool can be used to read the numerical code of the faulty component or condition. Intermittent faults are logged and stored in memory. Starting The Engine The engine's Electronic Control Module (ECM) will automatically provide the correct amount of fuel in order to start the engine. Do not hold the throttle down while the engine is cranking. If the engine fails to start in 30 seconds, release the starting switch. Allow the starting motor to cool for two minutes before the starting motor is used again. NOTICE Excessive ether (starting fluid) can cause piston and ring damage. Use ether for cold weather starting purposes only. Page 1 of 2 C18 Generator Set LXK00001-UP(SEBP6165 - 04) - Documentation 5/20/2015 https://127.0.0.1:449/sisweb/sisweb/techdoc/techdoc_print_page.jsp?returnurl=/sisweb/...

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C18 with emcp4

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i03522261

    General InformationSMCS - 1000

    These engines are in-line six cylinder engines. The engines have a firing order sequence of 1, 5, 3,6, 2, 4. The rotation of these engines is counterclockwise when the engine is viewed from theflywheel end. These engines utilize two turbochargers and an air-to-air aftercooler.

    The Electronic Unit Injector system (EUI) eliminates many of the mechanical components that aretraditionally used in the fuel injector assembly. The EUI also provides increased control of thetiming and increased control of the fuel air mixture. The timing advance is achieved by precisecontrol of the fuel injection timing. Engine speed is controlled by adjusting the injection duration.The engine has built-in diagnostics in order to ensure that all of the components are operatingproperly. In the event of a system component failure, the operator will be alerted to the conditionby a check engine light. The check engine light is located on the control panel. An electronicservice tool can be used to read the numerical code of the faulty component or condition.Intermittent faults are logged and stored in memory.

    Starting The EngineThe engine's Electronic Control Module (ECM) will automatically provide the correct amount offuel in order to start the engine. Do not hold the throttle down while the engine is cranking. If theengine fails to start in 30 seconds, release the starting switch. Allow the starting motor to cool fortwo minutes before the starting motor is used again.

    NOTICE

    Excessive ether (starting fluid) can cause piston and ring damage. Useether for cold weather starting purposes only.

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  • Cold Mode OperationThe ECM will set cold mode when the coolant temperature is below 18 C (64 F).Cold mode is activated five seconds after the start of the engine. During cold mode, low idle speedwill be increased to 800 rpm. After 60 seconds, the engine speed is reduced to 600 rpm. Enginepower will be limited until cold mode is deactivated.

    Cold mode will be deactivated when the coolant temperature reaches 18 C (64 F).Cold mode varies the amount of fuel that is injected for white smoke cleanup. Cold mode alsovaries the timing for white smoke cleanup. The engine operating temperature is usually reachedbefore the walk-around inspection is completed.

    After cold mode is completed, the engine should be operated at low speed until normal operatingtemperature is reached. The engine will reach normal operating temperature faster when theengine is operated at low speed and low power demand.

    Copyright 1993 - 2015 Caterpillar Inc.

    All Rights Reserved.

    Private Network For SIS Licensees.

    Wed May 20 16:27:59 UTC+0430 2015

    Page 2 of 2C18 Generator Set LXK00001-UP(SEBP6165 - 04) - Documentation

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i03267842

    Electronic Control System ComponentsSMCS - 1900

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  • Illustration 1 g01666193

    Left Side View

    (1) Turbocharger Outlet Pressure Sensor(2) Inlet Air Temperature Sensor(3) Fuel Pressure Sensor(4) Fuel Temperature Sensor(5) Electronics Ground Stud(6) Speed and Timing Sensor for the Camshaft(7) Speed and Timing Sensor for the Crankshaft(8) Atmospheric Pressure Sensor(9) Engine Oil Pressure Sensor

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  • (10) ECM connector J2/P2(11) ECM connector J1/P1(12) Engine Coolant Temperature Sensor

    Illustration 2 g01481339

    Right side view of engine

    (13) Engine Oil Temperature Sensor (If Equipped)

    The electronic control system is integrally designed into the engine's fuel system and the engine's airinlet and exhaust system in order to electronically control the fuel delivery and the injection timing.The electronic control system provides increased timing control and fuel air ratio control incomparison to conventional mechanical engines. Injection timing is achieved by precisely controllingthe injector firing time. Engine rpm is controlled by adjusting the injection duration. The ElectronicControl Module (ECM) energizes the unit injector solenoids in order to start the injection of fuel.Also, the ECM de-energizes the unit injector solenoids in order to stop the injection of fuel.The personality module is used by the ECM to store all the rated information for a particularapplication. The personality module can not be replaced physically. The personality module must beprogrammed with the latest flash files by using a computer. Refer to Systems Operation/Testing AndAdjusting, "Fuel System" for a complete explanation of the fuel injection process.The engine uses the following three types of electronic components:

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  • Input component

    Control component

    Output component

    An input component is one that sends an electrical signal to the ECM of the system. The signal that issent varies in either of the following ways:

    Voltage

    Frequency

    Pulse width

    The variation of the signal is in response to a change in some specific system of the engine. Somespecific examples of an input component are the engine speed-timing sensors and the coolanttemperature sensor. The ECM interprets the signal from the input component as information aboutthe condition, environment, or operation of the engine.

    A control component (ECM) receives the input signals from the input components. Electronic circuitsinside the control component evaluate the signals from the input components. These electroniccircuits also supply electrical energy to the output components of the system. The electrical energythat is supplied to the output components is based on predetermined combinations of input signalvalues.

    An output component is one that is operated by a control module. The output component receiveselectrical energy from the control group. The output component uses that electrical energy in one oftwo ways. The output component can use that electrical energy in order to perform work. The outputcomponent can use that electrical energy in order to provide information.

    As an example, a moving solenoid plunger will perform work. By performing work, the componenthas functioned in order to regulate the engine.

    As an example, a dash panel light or an alarm will provide information to the operator of the engine.

    These electronic components provide the ability to electronically control the engine operation.Engines with electronic controls offer the following advantages:

    Improvement in performance

    Improvement in fuel consumption

    Reduction in emissions levels

    Copyright 1993 - 2015 Caterpillar Inc.

    All Rights Reserved.

    Private Network For SIS Licensees.

    Wed May 20 16:29:00 UTC+0430 2015

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i02963253

    Fuel SystemSMCS - 1250

    Illustration 1 g01061346

    Fuel system schematic

    (1) Fuel supply line(2) Electronic unit injectors(3) Fuel gallery(4) Electronic Control Module (ECM)(5) Fuel pressure sensor(6) Fuel temperature sensor

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  • (7) Pressure regulating valve(8) Secondary fuel filter(9) Fuel priming pump(10) Fuel transfer pump(11) Primary fuel filter(12) Fuel tank

    The fuel supply circuit is a conventional design for engines with electronic unit injection. A fuel tank(12) is used to store the fuel prior to use by the engine. A primary fuel filter/water separator (11) isplaced into the fuel supply circuit in order to remove large debris from the fuel. This debris may haveentered the fuel tank during fueling. The debris may have also entered the fuel tank through the ventfor the fuel tank. The primary filter element also separates water from the fuel. The water is collectedin the bowl at the bottom of the primary fuel filter/water separator.

    Fuel is drawn from the fuel tank by the fuel transfer pump (10) . The fuel transfer pump is a gearpump with fixed clearances. The fuel transfer pump incorporates an internal relief valve that protectsthe fuel system from extreme pressure. In the case of extreme pressure, fuel is redirected back to theinlet of the fuel transfer pump. There are internal check valves that are also incorporated into the fueltransfer pump. An inlet check valve prevents fuel from draining back to the fuel tank while the fueltransfer pump is not in operation. An outlet check valve is used in order to prevent pressurized fuelleakage back through the pump. The fuel transfer pump is located in the front of the engine. The fueltransfer pump is driven by the front gear train.

    Note: The inlet fuel temperature to the fuel transfer pump must not exceed 79 C (175 F) when theengine has reached normal operating temperature. Fuel temperatures above 79 C (175 F) willreduce the life of the fuel transfer pump check valves. The fuel efficiency and the engine poweroutput are reduced when the fuel temperature increases from 30 C (86 F) to 70 C (158 F). Thefuel heaters should be turned "OFF" during warm weather.

    Fuel from the fuel transfer pump flows to the fuel filter base. The fuel flows through cored passagesin the fuel filter base. The fuel priming pump (9) is mounted on the fuel filter base. The fuel primingpump is used in order to manually pump the fuel into the fuel system after the system, or parts of thesystem have been drained. The fuel priming pump is used in order to refill the fuel system after airhas been introduced into the system. For more information on priming the fuel system, refer toTesting and Adjusting, "Fuel System - Prime".As the fuel flows through cored passages in the fuel filter base, the fuel is directed into a 2 micronfuel filter (8) . The fuel is filtered in order to remove small abrasive particles that will causepremature wear to fuel system components. Fuel flows out of the fuel filter and returns to thepassages in the fuel filter base. Prior to exiting the fuel filter base, the fuel pressure and the fueltemperature is sampled by the fuel pressure sensor (5) and by the fuel temperature sensor (6) . Thesignals that are generated by the sensors are used by the engine control in order to monitor thecondition of the engine's components. This information is also used to adjust the fuel delivery of theengine in order to optimize efficiency.

    The fuel flows from the fuel filter base to the Electronic Control Module (ECM) (4) . The pressurizedfuel is used in order to cool the electronic components that are in the ECM. Excessive heat willdamage the electronic components in the ECM. The electronics are used to control engine operation.

    The fuel is then directed through the fuel supply line (1) to fuel manifold (3) that runs the length ofthe cylinder head. The fuel enters the cylinder head at the front of the engine. A continuous flow offuel is supplied to the electronic unit injectors (2) in order to perform the following tasks:

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  • Supply fuel for injectionRemove excessive heat from the injectors.Remove air that may accumulate in the fuel system.

    The excess fuel flow that pumped through the system exits the cylinder head near the rear of theengine.

    The fuel exits the fuel gallery and returns to the fuel filter base. A pressure regulating valve (7) that islocated in the fuel filter base regulates the pressure for the fuel system. A sufficient amount of backpressure is maintained in the system in order to ensure a continuous availability of fuel to theelectronic unit injectors.

    Fuel HeatersFuel heaters prevent the waxing of the fuel in cold weather. The engine does not dissipate enoughheat in order to prevent waxing during cold weather conditions. Heaters that are not thermostaticallycontrolled can heat the fuel in excess of 65 C (149 F). High fuel temperatures can have thefollowing effects:

    Reduced engine efficiency

    Fuel pump damage

    Premature wear

    Note: Fuel heaters without thermostatic controls must never be used.

    The two types of fuel heaters that can be used: thermostatically controlled and self-adjusting.

    Electronic ControlsThere are two major components of the electronic control system that are necessary in order toprovide control of the mechanical electronic unit injectors:

    ECM

    Personality module (storage for the ECM flash file)The ECM is the computer that is used to provide control for all aspects of engine operation. Thepersonality module contains the software that defines the characteristics of the engine control. Thepersonality module contains the operating maps. The operating maps define the followingcharacteristics of the engine:

    Horsepower

    Torque curves

    Engine speed (rpm)Other characteristics

    The ECM, the personality module, the engine sensors, and the unit injectors work together in order tocontrol the engine. Neither of the four can control the engine alone.

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  • The ECM maintains the desired engine speed by sensing the actual engine speed. The ECMcalculates the amount of fuel that needs to be injected in order to achieve the desired engine speed.

    Fuel InjectionThe ECM controls the amount of fuel that is injected by varying the signal to each of the unitinjectors. The unit injectors will inject fuel only while the unit injector solenoid is energized. TheECM sends a 105 volt signal to the solenoid in order to energize the injector solenoid. By controllingthe timing of the 105 volt signal, the ECM controls injection timing. By controlling the duration ofthe 105 volt signal, the ECM controls the amount of fuel that is injected.The ECM sets certain limits on the amount of fuel that can be injected. The FRC fuel position is alimit that is based on boost pressure in order to control the fuel air mixture for the emission control.When the ECM senses an increase in the boost pressure, the ECM increases the FRC fuel position.The rated fuel position is a limit that is based on the horsepower rating of the engine. The rated fuelposition is similar to the rack stops and the torque spring on a mechanically governed engine. Therated fuel position provides the horsepower and the torque curves for a specific engine family. Therated fuel position provides the horsepower and the torque curves for a specific horsepower rating.The limits are programmed by the factory into the personality module. The limits are notprogrammable in the field.

    The injection timing relies on the following engine parameters: engine speed, engine load and otherengine data. The ECM senses the top center position of number one cylinder from the signal that isprovided by the engine speed/timing sensors. The ECM decides when the injection should occurrelative to this top center position. The ECM provides the signal to the unit injector at the desiredtime.

    Unit Injector Mechanism

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  • Illustration 2 g01484615

    Typical unit injector mechanism(13) Unit injector(14) Adjusting nut(15) Rocker arm assembly(16) Camshaft

    The unit injector mechanism provides the downward force that is required to pressurize the fuel in theunit injector. When a signal is received from the ECM, the unit injector (13) injects the pressurizedfuel into the combustion chamber. The camshaft gear is driven by an idler gear which is driventhrough the front gear train by the crankshaft gear. The gears of the front gear train that are timedmust be aligned in order to provide the correct relationship between the piston and valve movement.During assembly of the front gear train, care must be taken in order to correctly align the timingmarks of the gears. The camshaft has three camshaft lobes for each cylinder. Two lobes operate theinlet and exhaust valves, and one operates the unit injector mechanism. Force is transferred from theunit injector lobe on camshaft (16) through rocker arm assembly (15) to the top of the unit injector.The adjusting nut (14) allows setting of the unit injector adjustment. Refer to the section onadjustment of the injector in Testing and Adjusting for the proper setting of the unit injector.

    Electronic Unit Injector

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  • Illustration 3 g01484734

    Electronic unit injector(17) Spring(18) Solenoid connection to the Electronic Control Module (ECM)(19) Solenoid valve assembly(20) Plunger assembly(21) Barrel(22) Seal(23) Seal(24) Spring(25) Spacer(26) Body(27) Check valve

    Fuel at low pressure from the fuel supply manifold enters the electronic unit injector at the fill portthrough drilled passages in the cylinder head.

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  • As the electronic unit injector mechanism transfers the force to the top of the electronic unit injector,spring (17) is compressed and plunger (20) is driven downward. This action displaces fuel throughthe valve in solenoid valve assembly (19) , and into the return manifold to the fuel tank. As theplunger travels downward, the passage in barrel (21) is closed by the outside diameter of the plunger.The passages within body (26) and along check valve (27) to the injector tip already contain fuel forinjection. After the passage in the plunger barrel is closed, the injector is ready for injection at anytime. The start of injection relies on the software in the Electronic Control Module (ECM).When the solenoid valve assembly is energized from a signal across solenoid connection (18) , thevalve closes and fuel pressure is elevated in the injector tip. Injection begins at 34500 1900 kPa(5000 275 psi) as the force of spring (24) above spacer (25) is overcome. The check valve begins tolift from the valve seat. The pressure continues to rise as the plunger cycles through a full stroke.After the correct amount of fuel has been discharged into the cylinder, the ECM removes the signal tothe solenoid connection. The solenoid valve assembly is de-energized and the valve in the solenoidvalve assembly is opened. The high pressure fuel is then dumped through the spill port and into thefuel return manifold. The fuel is then returned to the fuel tank. The check valve in the injector tipseats as the pressure in the tip decreases.

    The duration of injection meters the fuel that is consumed during the fuel injection process. Injectionduration is controlled by the governor logic that is programmed into the ECM.

    As the camshaft lobe rotates past the point of maximum lobe lift, the force on top of the electronicunit injector is removed and the spring for the injector mechanism is allowed to expand. The plungerreturns to the original position. This uncovers the fuel supply passage into the plunger barrel in orderto refill the injector pump body. The fuel at low pressure is again allowed to circulate through the fuelinjector body. After circulating through the fuel injector body, the fuel flows out of the spill port. Thiscontinues until the solenoid valve assembly is re-energized for another injection cycle.

    Copyright 1993 - 2015 Caterpillar Inc.

    All Rights Reserved.

    Private Network For SIS Licensees.

    Wed May 20 16:29:42 UTC+0430 2015

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i02963595

    Air Inlet and Exhaust SystemSMCS - 1050

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  • Illustration 1 g01051217

    Air inlet and exhaust system

    (1) Inlet valves(2) Exhaust valves(3) Exhaust manifold(4) Air-to-air Aftercooler(5) Air inlet(6) Exhaust outlet(7) Turbocharger(8) Inlet manifold

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  • The components of the air inlet and exhaust system control the quality of air and the amount of airthat is available for combustion. The components of the air inlet and exhaust system are thefollowing components:

    Air cleaner

    Turbocharger

    Aftercooler

    Cylinder head

    Valves and valve system components

    Piston and cylinder

    Inlet manifold

    Exhaust manifold

    Note: The following description of the operation of the air inlet and exhaust system assumes thatthe engine is developing boost pressure.

    Inlet air passes through the air cleaner into the air inlet (5) of the turbocharger compressor wheel.The turbocharger (7) will supply more volume of air into the engine. This compressing of the air isreferred to as boost. The compressing of air causes the air temperature to rise to about 204 C (400F). As the air flows through the aftercooler (4) the temperature of the compressed air lowers toabout 46 C (115 F). Cooling of the inlet air causes the air to become more dense. This increasescombustion efficiency and this increases horsepower output.

    From the aftercooler (4) , air enters the inlet manifold (8) . Air flow from the inlet manifold (8)into the cylinders is controlled by inlet valves (1) . There are two inlet valves and two exhaustvalves (2) for each cylinder. The inlet valves (1) open at the top center position before the pistonmoves toward the bottom center position. This is called the inlet stroke. When the inlet valves (1)open, cooled compressed air from the inlet port enters the cylinder. The inlet valves (1) close asthe piston reaches the bottom center position. The piston begins to travel back to the top centerposition on the compression stroke. The air in the cylinder is compressed to a very hightemperature. When the piston is near the end of the compression stroke, fuel is injected into thecylinder and mixes with the air. This causes combustion to start in the cylinder. Once combustionstarts, the combustion force pushes the piston toward the bottom center position. This is called thepower stroke. The exhaust valves (2) open when the piston moves toward the bottom centerposition and the exhaust gases are pushed through the exhaust port into exhaust manifold (3) asthe piston travels toward top center on the exhaust stroke. The exhaust valves (2) close and thecycle starts again. The complete cycle consists of four strokes:

    Inlet

    Compression

    Power

    Exhaust

    Exhaust gases from the exhaust manifold (3) enter the turbine side of the turbocharger (7) . Theexhaust gas temperature causes the turbine wheel in the turbocharger (7) to turn. The turbine

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  • wheel is connected to the shaft that drives the compressor wheel. Exhaust gases from the turbinewheel exit the turbocharger (7) .

    Turbocharger

    Illustration 2 g01485074

    Turbocharger

    (9) Air inlet(10) Compressor housing(11) Compressor wheel(12) Bearing(13) Oil Inlet port(14) Bearing(15) Turbine housing(16) Turbine wheel(17) Exhaust outlet(18) Oil outlet port

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  • (19) Exhaust inlet

    All of the air that enters the engine passes through the turbocharger. All of the exhaust gases fromthe engine pass through the turbocharger.

    The exhaust gases enter turbine housing (15) through exhaust inlet (19) . The exhaust gas pusheson the blades of the turbine wheel (16) . The turbine wheel is connected by a shaft to thecompressor wheel (11) .Air that passes through the air filters enters the compressor housing air inlet (9) by the rotation ofcompressor wheel (11) . The compressor wheel causes the inlet air to be pushed into the inlet sideof the engine. Boost pressure is caused when the compressor wheel pushes more air into the inletside of the engine. This results in an inlet manifold pressure that exceeds atmospheric pressure.This allows the engine to burn more fuel. When the engine burns more fuel the engine producesmore power.

    When the throttle is opened, more fuel is injected into the cylinders. The combustion of thisadditional fuel produces greater exhaust temperature. The additional exhaust temperature causesthe turbine and the compressor wheels of the turbocharger to turn faster. As the compressor wheelturns faster, more air is forced into the cylinders. The increased flow of air gives the engine morepower by allowing the engine to burn the additional fuel with greater efficiency.

    Bearings (12) and (14) for the turbocharger use engine oil under pressure for lubrication andcooling. The oil comes in through oil inlet port (13) . The oil then goes through passages in thecenter section in order to lubricate the bearings. This oil also cools the bearings. Oil from theturbocharger goes out through oil outlet port (18) in the bottom of the center section. The oil thengoes back to the engine oil pan.

    Valve System Components

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  • Illustration 3 g01485193

    Valve system components

    (20) Rocker arm(21) Locknut for adjusting screw(22) Rocker arm shaft(23) Camshaft(24) Valve bridge

    The valve train controls the flow of inlet air and exhaust gases into the cylinders and out of thecylinders during engine operation. The camshaft (23) controls the timing of the valves duringengine operation.

    The crankshaft gear drives the camshaft gear through an idler gear. The camshaft must be timed tothe crankshaft in order to get the correct relation between the piston position and the valveposition.

    The camshaft has three camshaft lobes for each cylinder. One camshaft lobe operates the inletvalves. One camshaft lobe operates the exhaust valves. One camshaft lobe operates the unitinjector. The camshaft lobes cause the follower on the rocker arm in order to actuate the valvesand the unit injector.Each cylinder has two inlet valves and two exhaust valves. Valve springs hold the valves closedand the valve springs resist the opening of the valves. This ensures that the valves will close at

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  • high rpm and under high boost pressures. Valve rotators cause the valves to rotate while theengine is running. The rotation of the valves prevents the valves from burning by constantlychanging the contact area of the valve face and the valve seat. This rotation gives the valves longerservice life.

    Copyright 1993 - 2015 Caterpillar Inc.

    All Rights Reserved.

    Private Network For SIS Licensees.

    Wed May 20 16:30:07 UTC+0430 2015

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i03267863

    Lubrication SystemSMCS - 1300

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  • Illustration 1 g01666216

    (1) Piston cooling jets(2) Camshaft journals(3) Main bearings(4) Oil passage(5) Turbocharger oil supply line(6) Oil filter bypass valve(7) Oil filter(8) Oil cooler bypass valve(9) High pressure bypass valve(10) Oil Cooler

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  • (11) Engine oil pump(12) Oil pump bypass valve(13) Secondary engine oil filter (if equipped)(14) Engine oil pan

    The lubrication system supplies filtered oil at approximately 275 kPa (40 psi) at rated engineoperating conditions. Oil pump bypass valve (12) is controlled by the engine oil manifold pressure.Oil cooler bypass valve (8) maintains the engine oil temperature to 110 C (230 F). High pressurebypass valve (9) , which is located in the filter base, protects the filters and other components duringcold starts. The opening pressure of the high pressure bypass valve is 695 kPa (100 psi). Secondaryoil filter (13) is a five micron filter which filters five percent of the oil flow before returning the oil tothe sump. The pressure differential of the oil filter bypass valve is 170 kPa (25 psi). The engine oilpressure sensor is part of the engine protection system.

    The turbocharger cartridge bearings are lubricated by oil supply line (5) from the main oil gallery,and the oil drain line returns the oil flow to the sump.

    Oil Flow Through The Lubrication System

    Illustration 2 g01091517

    Flow through oil filter base

    (6) Oil filter bypass valve(8) Oil cooler bypass valve(15) Flow from oil pan

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  • (16) Flow up to oil cooler(17) Flow from oil cooler(18) Flow into oil filters(19) Flow out of oil filters(20) Flow to engine

    The engine oil pump is mounted to the back of the front gear train. The engine oil pump is driven byan idler gear from the crankshaft gear. Oil is pulled from the sump through the oil pump on the wayto the engine oil cooler. The bypass valve controls the engine oil pressure. The engine oil pump iscapable of supplying excess oil for the lubricating system. When this situation is present, the oilpressure increases and the bypass valve opens. The open bypass valve allows the excess oil to returnto the sump.

    The oil then flows through the engine oil cooler. The engine oil cooler uses engine coolant in order tocool the oil. The oil cooler bypass valve (8) directs the oil flow through the engine oil cooleraccording to the temperature of the oil and the pressure of the oil.

    Oil cooler bypass valve (8) will close when the oil temperature exceeds the following temperatures100 C to 103 C (212 F to 217 F). Closing of the bypass valve will direct the oil through theengine oil cooler.

    The oil cooler bypass valve (8) is normally closed if the pressure differential across the engine oilcooler is less than 155 17 kPa (22 3 psi). This will direct the oil through the engine oil cooler.When the oil returns from the engine oil cooler, the oil flows to the two engine oil filters. When theoil pressure differential across oil filter bypass valve (6) reaches 170 kPa (25 psi), the valve allowsthe oil flow to bypass the primary engine oil filter in order to lubricate the engine parts. The bypassvalve provides immediate lubrication to the engine components when there is a restriction in theprimary engine oil filter due to the following conditions:

    Cold oil with high viscosity

    Plugged primary engine oil filter

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  • Illustration 3 g01095134

    (21) Piston cooling jet(22) Piston(23) Connecting rodFiltered oil flows through the main oil gallery in the cylinder block to the following components:

    Piston cooling jets (21)Valve mechanism

    Camshaft bearings

    Crankshaft bearings

    Turbocharger

    An oil cooling chamber is formed by the following pieces: the lip forge at the top of the skirt of thepiston (22) and the cavity behind the ring grooves in the crown. Oil flow from the piston cooling jetenters the cooling chamber through a drilled passage in the skirt. The oil then returns to the sumpthrough the clearance gap between the crown and the skirt. Four holes that are drilled from the pistonoil ring groove to the interior of the piston drain excess oil from the oil ring.

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i02166213

    Cooling SystemSMCS - 1350

    This engine has a pressure type cooling system that is equipped with a shunt line.

    A pressure type cooling system gives two advantages. First, the cooling system can be operatedsafely at a temperature that is higher than the boiling point of water. Also, cavitation in the waterpump is prevented. It is more difficult for air or steam pockets to be made in the cooling system.

    Note: A 30 percent mixture of ethylene glycol base antifreeze must be used for efficient waterpump performance on engines that are equipped with an air-to-air aftercooler. This mixture keepsthe cavitation temperature range of the coolant high enough for efficient performance. Refer toOperation and Maintenance Manual, "Refill Capacities and Recommendations".

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  • Illustration 1 g01096647

    Cooling system for a warm engine

    (1) Cylinder head(2) Water temperature regulators(3) Outlet hose(4) Vent line(5) Vent tube(6) Shunt line(7) Elbow(8) Water pump(9) Cylinder block(10) Oil cooler(11) Inlet hose(12) Radiator

    During operation, water pump (8) sends most of the coolant from radiator (12) to oil cooler (10) .The coolant from oil cooler (10) goes into cylinder block (9) through a bonnet and an elbow. Thecoolant flows around the cylinder liners into the cylinder head.

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  • The flow of coolant goes around the valves and the passages for exhaust gases in the cylinderhead. The coolant then goes to the front of the cylinder head. At this point, two water temperatureregulators (2) control the direction of coolant flow.Water temperature regulators (2) are closed when the engine is cold. The coolant flows throughthe regulator housing and elbow (7) back to water pump (8) .If the coolant is at normal operating temperature, water temperature regulators (2) open and thecoolant flows to radiator (12) through the outlet hose (3). The coolant becomes cooler as thecoolant moves through the radiator. When the coolant gets to the bottom of the radiator, thecoolant goes through inlet hose (11) and into water pump (8) .Note: Water temperature regulators (2) are an important part of the cooling system. Watertemperature regulator (2) divides the coolant flow between radiator (12) and bypass elbow (7).This will maintain the correct temperature.

    Shunt line (6) gives several advantages to the cooling system. The shunt line gives a positivecoolant pressure at the water pump inlet that prevents pump cavitation. A small flow of coolantconstantly goes through shunt line (6) to the inlet of water pump (8). This causes a small amountof coolant to move constantly through vent tube (5). The flow through the vent tube is small andthe volume of the upper compartment is large. Air in the coolant is removed as the coolant goesinto the upper compartment.

    The vent line is used to fill the cooling system with coolant for the first time. This will purge anyair out of the top of a bottom filled system.

    A surge tank may be installed into the system. The tank can be mounted on the radiator or the tankcan be mounted on a remote location. The coolant that expands past the radiator cap is retained inthe surge tank. The coolant contracts as the temperature drops and the coolant is drawn back intothe radiator.

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i02072920

    Basic EngineSMCS - 1200

    Cylinder Block AssemblyThe cylinder block is of a skirted design that is made from cast iron. Drilled passageways allow oilto supply the oil for the crankshaft bearings and the pistons. Cooling passages are cast into theblock. This engine utilizes wet cylinder liners that are serviceable. The configuration providesimproved rigidity.

    The cylinder liner is a compacted graphite liner that is induction hardened. A steel spacer plateprovides improved reusability and durability.

    Cylinder Head AssemblyThe cylinder head is a one-piece cast iron head. The camshaft is contained within the cylinderhead. This improves the rigidity of the valve train. Steel reinforced aluminum bearings are pressedinto each journal. The bearings are lubricated under pressure. Bridge dowels have been eliminatedas the valve train uses floating valve bridges.

    Thermal efficiency is enhanced by the use of stainless steel thermal sleeves in each exhaust port.The sleeves reduce the amount of heat rejection to the cooling system. The sleeves then transferthe thermal energy to the turbocharger.

    The electronic unit injector is mounted in a stainless steel sleeve. This sleeve has been pressed intothe cylinder head injector bore.

    Pistons, Rings And Connecting RodsThe piston is a one-piece design that is forged steel. An oil cooling chamber is formed by the lipthat is cast at the top of the piston and the cavity that is behind the ring grooves. The oil flow thenreturns to the sump through the clearance gap between the crown and the skirt. The pistons havethree rings that are located in grooves in the steel crown. The rings seal the combustion gas andthe rings provide control of the oil. The top ring has a barrel face. This ring is a KEYSTONE ringwith a nitrided coating. The second ring has a square face with a nitrided coating. The third ring is

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  • the oil ring. The ring is double railed and the ring is ground with a profile. This ring is coated withnitride. The oil ring has a coil spring expander. There are four holes that are drilled from the pistonoil ring groove to the interior of the piston. These holes drain excess oil from the oil ring.

    The cap of the connecting rod is attached to the shank by four bolts that are threaded into theshank. Each side of the small end of the connecting rod is machined at an angle of 12 degrees inorder to fit within the piston cavity.

    CrankshaftThe crankshaft converts the combustion force in the cylinder into rotating torque. The rotatingtorque powers the equipment. On this engine, a vibration damper is used at the front of thecrankshaft in order to reduce the torsional vibrations. The torsional vibrations can cause damage tothe engine.

    The crankshaft drives a group of gears (front gear train) on the front of the engine. The front geartrain provides power for the following components: camshaft, water pump, oil pump and transferpump.

    The crankcase has seven main bearings that support the crankshaft. The crankcase also has twobolts which hold each bearing cap to the block. The oil holes in the shell for the upper bearing arelocated at all of the main bearing journals. The grooves in the shell for the upper bearing are alsolocated at all of the main bearing journals. The holes and the grooves supply oil to the connectingrod bearings.

    To seal the crankcase, crankshaft seals are installed in the front timing gear housing and theflywheel housing.

    CamshaftThe camshaft has three lobes for each cylinder. These lobes allow the camshaft to operate theelectronic unit injectors, exhaust valves, and the inlet valves. The camshaft is supported in thecylinder head by seven journals which are fit with aluminum bearings. A bearing is pressed intoeach journal. The camshaft gear contains integral roller dampers that counteract the torsionalvibrations that are generated by the high pressure from operation of the electronic unit injectors.The design reduces gear train noise. This design also increases the life of the gear train. Thecamshaft is driven by an adjustable idler gear which is turned by a fixed idler gear which is turnedby a cluster idler gear in the front gear train. Each bearing journal is lubricated from the oilmanifold in the cylinder head. A thrust plate that is located at the front positions the camshaft.Timing of the camshaft is accomplished by aligning marks on the crankshaft gear and idler gear.

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  • Shutdown SIS

    Previous Screen

    Product: GENERATOR SET

    Model: C18 GENERATOR SET LXK01006

    Configuration: C18 Generator Set LXK00001-UP

    Systems OperationC13, C15, and C18 Generator Set EnginesMedia Number -SENR9708-15 Publication Date -01/08/2014 Date Updated -28/08/2014

    i02964450

    Electrical SystemSMCS - 1400; 1550; 1900

    ReferenceRefer to the Schematic and the Troubleshooting, "Electronic Troubleshooting" for additionalinformation on your engine.

    Grounding PracticesProper grounding for the electrical system is necessary for proper engine performance andreliability. Improper grounding will result in unreliable electrical circuit paths and in uncontrolledelectrical circuit paths.

    Uncontrolled engine electrical circuit paths can result in damage to the main bearings, to thecrankshaft bearing journal surfaces, and to the aluminum components.Uncontrolled electrical circuit paths can cause electrical noise which may degrade performance.

    In order to ensure proper functioning of the electrical system, an engine-to-frame ground strapwith a direct path to the battery must be used. This may be provided by the starting motor ground,by a frame to starting motor ground, or by a direct frame to engine ground. An engine-to-frameground strap must be run from the grounding stud of the engine to the frame and to the negativebattery post.

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  • Illustration 1 g01486733

    Typical example of grounding the battery and the cylinder head to the frame rail

    (1) Cylinder head ground stud(2) Optional engine ground stud(3) Frame rail

    Connect the battery negative post to frame rail (3) . From the frame rail, connect the ground wireto one of the following locations:

    Cylinder head ground stud (1)Optional engine ground stud connection (2)

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  • Illustration 2 g01096929

    Typical example of the alternate cylinder head to the battery ground

    (1) Cylinder head ground stud(2) Optional engine ground stud(3) Frame rail

    The engine must be grounded to frame rail (3) . Connect the battery negative post to one of thefollowing locations:

    Cylinder head ground stud (1)Optional engine ground stud connection (2)

    The engine must have a ground wire to the battery.

    Ground wires or ground straps should be combined at the studs that are only for ground use.

    All of the ground paths must be capable of carrying any potential currents. A wire that is AWG 0or more is recommended for the cylinder head ground strap.

    The engine alternator should be grounded to the battery with a wire size that is capable ofmanaging the full charging current of the alternator.

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  • NOTICE

    When jump starting an engine, the instructions in the Operation andMaintenance Manual, "Starting with Jump Start Cables" should be

    followed in order to properly start the engine.

    This engine may be equipped with a 12 volt starting system or with a24 volt starting system. Only equal voltage for boost starting should be

    used. The use of a welder or of a higher voltage will damage theelectrical system.

    The engine has several input components which are electronic. These components require anoperating voltage.

    This engine is tolerant to common external sources of electrical noise. Electromechanical buzzerscan cause disruptions in the power supply. If electromechanical buzzers are used near the system,the engine electronics should be powered directly from the battery system through a dedicatedrelay. The engine electronics should not be powered through a common power bus with otherdevices that are activated by the engine control switch (ECS).

    Engine Electrical SystemThe electrical system can have three separate circuits. The three circuits are the charging circuit,the starting circuit, and the low amperage circuit. Some of the electrical system components areused in more than one circuit.

    The charging circuit is in operation when the engine is running. An alternator creates electricityfor the charging circuit. A voltage regulator in the circuit controls the electrical output in order tomaintain the battery at full charge.

    The starting circuit is in operation when the start switch is activated.

    The low amperage circuit and the charging circuit are connected through the ammeter. Thestarting circuit is not connected through the ammeter.

    Charging System ComponentsAlternator

    The alternator is driven by the crankshaft pulley through a belt that is a Poly-vee type. Thisalternator is a three-phase self-rectifying charging unit. The regulator is part of the alternator.

    The alternator design has no need for slip rings or for brushes. The only part of this alternator thatmoves is the rotor assembly. All of the conductors that carry current are stationary. The followingcomponents are the conductors: the field winding, the stator windings, six rectifying diodes andthe regulator circuit.

    The rotor assembly has many magnetic poles with air space between each of the opposite poles.The poles have residual magnetism that produces a small amount of magnet-like lines of force(magnetic field). This magnetic field is produced between the poles. As the rotor assembly beginsto turn between the field winding and the stator windings, a small amount of alternating current

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  • (AC) is produced in the stator windings. The alternating current is produced from the smallmagnetic lines of force that are created by the residual magnetism of the poles. The AC is changedinto direct current (DC) when the current passes through the diodes of the rectifier bridge. Most ofthis current provides the battery charge and the supply for the low amperage circuit. Theremainder of current is sent to the field windings. The DC current flow through the field windings(wires around an iron core) increases the strength of the magnetic lines of force. These strongermagnetic lines of force increase the amount of AC that is produced in the stator windings. Theincreased speed of the rotor assembly also increases the current output of the alternator and thevoltage output of the alternator.

    The voltage regulator is a solid-state electronic switch. The voltage regulator senses the voltage ofthe system. The regulator then uses switches to control the current to the field windings. Thiscontrols the voltage output in order to meet the electrical demand of the system.

    NOTICE

    The alternator should never be operated without the battery in thecircuit. The making or the breaking of an alternator connection with a

    heavy load on the circuit can cause damage to the regulator.

    Illustration 3 g01486777

    Typical cross section of an alternator

    (4) Regulator(5) Roller bearing(6) Stator winding(7) Ball bearing(8) Rectifier bridge

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  • (9) Field winding(10) Rotor assembly(11) Fan

    Starting System ComponentsSolenoid

    Illustration 4 g00292316

    Typical cross section of a solenoid

    A solenoid is an electromagnetic switch that performs two basic functions:

    The solenoid closes the high current starting motor circuit with a low current start switchcircuit.

    The solenoid engages the starting motor pinion with the ring gear.

    The solenoid has windings (one set or two sets) around a hollow cylinder or a hollow housing. Aplunger that is spring loaded is located within the solenoid housing. The plunger can moveforward and backward. When the start switch is closed and electricity is sent through thewindings, a magnetic field is created. The magnetic field pulls the plunger forward in the solenoidhousing. This moves the shift lever in order for the pinion drive gear to engage with the ring gear.The front end of the plunger then makes contact across the battery and across the motor terminalsof the solenoid. The starting motor then begins to turn the flywheel of the engine.

    When the start switch is opened, current no longer flows through the windings. The spring nowreturns the plunger to the original position. At the same time, the spring moves the pinion gearaway from the flywheel.

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  • When two sets of windings in the solenoid are used, the windings are called the hold-in windingand the pull-in winding. Both of the windings wind around the cylinder for an equal amount oftimes. The pull-in winding uses a wire with a larger diameter in order to produce a strongermagnetic field. When the start switch is closed, part of the current flows from the battery throughthe hold-in winding. The remainder of the current flows through the pull-in windings, to the motorterminal, and then to the ground. When the solenoid is activated, the current is shut off through thepull-in windings. Only the smaller hold-in windings are in operation for the extended period oftime that is necessary for the engine to be started. The solenoid will now take a smaller amount ofcurrent from the battery. Heat that is created by the solenoid will be kept at an acceptable level.

    Starting Motor

    Illustration 5 g01486816

    Typical cross section of a starting motor

    (12) Field(13) Solenoid(14) Clutch(15) Pinion(16) Commutator(17) Brush assembly(18) Armature

    The starting motor rotates the engine flywheel at a rate that is fast enough to start the engine.

    The starting motor has a solenoid. When the start switch is activated, the solenoid will move thestarter pinion in order to engage the pinion and the ring gear on the engine flywheel. The starterpinion and the ring gear will engage before the circuit between the battery and the starting motoris closed by the electric contacts in the solenoid. When the circuit between the battery and the

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  • starting motor is complete, the pinion will rotate the engine flywheel. A clutch provides protectionfor the starting motor so that the engine cannot turn the starting motor too fast. When the switch isreleased, the starter pinion will move away from the ring gear.

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