G3406 Engine Caterpillar


Air Inlet and Exhaust System Components

Usage:

G3406 1RK
The engine can have a system that uses high pressure gas or low pressure gas.


Illustration 1g00776843
Diagram for a turbocharged air inlet and exhaust system with high pressure gas
(1) Gas pressure regulator
(2) Balance line
(3) Carburetor
(4) Air cleaner
(5) Turbocharger
(6) Gas supply
(7) Governor
(8) Aftercooler
(9) Air inlet manifold
(10) Cylinder
(11) Exhaust bypass valve
(12) Exhaust manifold


Illustration 2g00830515
Diagram for a turbocharged air inlet and exhaust system with low pressure gas
(AA) Exhaust gas
(BB) Air and gas to cylinders
(CC) Gas supply
(DD) Low pressure gas
(EE) Air inlet
(1) Gas pressure regulator
(2) Balance line
(3) Carburetor
(4) Air cleaner
(5) Turbocharger
(6) Gas supply
(7) Governor
(8) Aftercooler
(9) Air inlet manifold
(10) Cylinder
(11) Exhaust bypass valve
(12) Exhaust manifold

Fuel from gas supply (6) goes to gas pressure regulator (1). After the gas is reduced to the desired pressure by the regulator, the gas goes to carburetor (3).

Inlet air is filtered by air cleaner (4).

On high pressure gas fuel systems (Illustration 1), turbocharger (5) delivers compressed air to the carburetor. Boost pressure is delivered to the gas pressure regulator through balance line (2) in order for the regulator to maintain the differential pressure between the gas and the inlet air.

With low pressure gas (Illustration 2), the air and the fuel are mixed in the carburetor and the mixture is compressed by the turbocharger.

Governor (7) controls the opening of the throttle. The air and fuel is cooled in aftercooler (8) before entering air inlet manifold (9) and cylinders (10).

Exhaust gas travels to exhaust manifold (12). Some of the exhaust gas drives turbocharger (5) before the exhaust gas exits through the exhaust outlet. If the boost pressure is excessive, some of the exhaust gas is diverted by exhaust bypass valve (11) to the exhaust outlet.

Some systems have a gas shutoff valve in the supply line. This valve may be electrically operated from the ignition system. The valve can be operated manually in order to stop the engine. Manual resetting of the valve is needed in order to restart the engine.

Engine installations that use dual fuel systems have components that are similar to the components in the above illustrations. However, an engine that uses a dual fuel system requires two gas pressure regulators. When the gas is changed, adjustments must be made for differences in the BTU content of the gas. An engine that has a dual fuel system can change fuels automatically. For optimum operation, the engine timing must be adjusted when the fuel is switched.

Caterpillar Information System:

Electronic Modular Control Panel II (EMCP II) Fault Log Clearing OP4
Electronic Modular Control Panel II (EMCP II) Normal Mode
Electronic Modular Control Panel II (EMCP II) Display of Voltage or Current Is Zero
Electronic Modular Control Panel II (EMCP II) GSC Operation Is Erratic
Electronic Modular Control Panel II (EMCP II) Engine Does Not Shutdown (for PEEC Engines)
Electronic Modular Control Panel II (EMCP II) AC Offset Adjustment OP10
Electronic Modular Control Panel II (EMCP II) Engine Does Not Shutdown (for MUI 3412C, 3508,3512, 3516 Engines)
Electronic Modular Control Panel II (EMCP II) Engine Does Not Shutdown (for MUI 3306B, 3406C Engines)
Electronic Modular Control Panel II (EMCP II) Engine Does Not Shutdown (for EUI Engines)
Electronic Modular Control Panel II (EMCP II) Starting Motor Remains Engaged (for MUI 3412C, 3508, 3512, 3516 Engines)
G3304 and G3306 Engines General Information (Cooling System)
Electronic Modular Control Panel II (EMCP II) Starting Motor Remains Engaged (for EUI and PEEC Engines)
G3406 Engine Finding the Top Center Position for the No. 1 Piston
Electronic Modular Control Panel II (EMCP II) SP Fault Codes
Electronic Modular Control Panel II (EMCP II) Indicators of Alarm Module or Remote Annunciator Are Constantly Flashing
Electronic Modular Control Panel II (EMCP II) Alarm Module Control (Custom)
Electronic Modular Control Panel II (EMCP II) GSC CID 0100 - FMI 02 (for EUI Engines)
Electronic Modular Control Panel II (EMCP II) GSC CID 0100 - FMI 02 (for MUI and PEEC Engines)
Electronic Modular Control Panel II (EMCP II) GSC CID 0100 - FMI 03
Electronic Modular Control Panel II (EMCP II) GSC CID 0100 - FMI 04
Electronic Modular Control Panel II (EMCP II) GSC CID 0110 - FMI 02 (for EUI Engines)
Electronic Modular Control Panel II (EMCP II) GSC CID 0110 - FMI 02 (for MUI and PEEC Engines)
Electronic Modular Control Panel II (EMCP II) Fault Identification
Electronic Modular Control Panel II (EMCP II) GSC CID 0110 - FMI 03
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