79476A 7 Mercruiser FLANGE ASSEMBLY (2")


79476A 7 FLANGE ASSEMBLY (2") Mercruiser 02297343, 428B116KD, 442B110GD, 442B115KD, 4A72040ND, 4C72040TD, 4C8204DLD, 4CJ2040ND FLANGE
79476A 7 FLANGE ASSEMBLY (2") Mercruiser
Rating:
78

Buy FLANGE ASSEMBLY (2") 79476A 7 Mercruiser genuine, new aftermarket parts with delivery
Number on catalog scheme: 6
 

Mercruiser entire parts catalog list:

02297343 1983,1985,1986
428B116KD 1997,1998
442B110GD 1994,1995,1996,1998
442B115KD 1997
4A72040ND 1998
4C72040TD 1998
4C8204DLD 1998
4CJ2040ND 1998

Information:


Illustration 1 g01442708The fuel flows from the main gas supply through a knock-down regulator. A knock-down regulator is a second regulator that is needed when the gas supply pressure is too high for a single regulator to manage.From knock-down regulator, the fuel flows to the fuel filter. Usually, the fuel filter is a component of the design at the particular site. The customer is responsible for supplying clean, dry fuel to the engine. The fuel filter may be supplied by Caterpillar or by the customer. To prevent particles from entering the engine, a 1 micron filter is recommended. Use a filter that is properly sized for the required gas pressure.For installation of the fuel filter, the recommended location is close to the engine before the engine gas pressure regulator. Pressure gauges in the gas lines on each side of the fuel filter are recommended to monitor the filter differential pressure. A manual shutoff valve in the gas line before the fuel filter will facilitate servicing of the filter.The filtered fuel flows to the Gas Shutoff Valve (GSOV). The GSOV may be supplied by Caterpillar or by the customer. The solenoid for the GSOV may be connected to engine wiring harness or to a harness that is supplied by the customer. In either case, the customer may install a switch that can interrupt the circuit.The control system is configured for a GSOV that is energize-to-run. This means that the GSOV must be energized in order for the engine to run. The GSOV may be energized by the customer equipment or by the ECM. When the GSOV is energized, the valve opens and the fuel flows to the engine. When the control system shuts down the engine, the voltage is removed from the solenoid. The valve closes and the fuel is shut off.The fuel flows through the GSOV to the gas pressure regulator.The regulator may be supplied by Caterpillar or by the customer.For parallel to utility applications, the required fuel pressure stability is 1.7237 kPa ( 0.25 psi).A regulated pressure of 7 to 35 kPa (1 to 5 psi) is recommended.For island mode applications, the minimum fuel pressure is 20 kPa (2.9 psi). Steady state fuel pressure stability requirement of 6.9 mbar/sec (0.10 psi/sec). Transient fuel pressure stability requirement of 48.2 mbar/sec (0.70 psi/sec).For the Lean Coal Mine Methane (LCMM) application, the recommended fuel pressure range is 5 kPa (0.7psi) to 35 kPa (5 psi).Less gas pressure may result in reduced power. More gas pressure may result in instability.
Illustration 2 g00925714
Top view
Fuel flow through the single turbocharger arrangement
(1) Fuel metering valve
Illustration 3 g00925717
Top view
Fuel flow through the twin turbocharger arrangement.
(1) Fuel metering valve
Illustration 4 g06447735
Top view for the Lean Coal Mine Methane (LCMM) application
Fuel flows through a twin turbocharger arrangement.
(1) Fuel metering valves (TecJet)
Illustration 5 g01442860
Fuel flow through a low BTU arrangement
(1) Fuel metering valveThe fuel flows to the electronically controlled fuel metering valve (1). The ECM issues a command signal to the fuel metering valve via the CAN data link. The fuel metering valve regulates the flow of fuel to the engine.
Illustration 6 g00925730
Right view
Flow of fuel and of air through the single turbocharger arrangement
(2) Air inlet elbow adapter
(3) Turbocharger compressor
Illustration 7 g00925767
Right view
Flow of fuel and of air through the twin turbocharger arrangement
(2) Air inlet elbow adapter
(3) Turbocharger compressorThe fuel metering valve controls the volume of fuel that flows to adapter (2) for the air inlet elbow. The inlet air that is necessary for combustion also enters the adapter. The air/fuel mixture enters turbocharger compressor (3).
Illustration 8 g00925773
Right view
Flow of fuel and of air through the single turbocharger arrangement
(4) Throttle
(5) Aftercooler
Illustration 9 g00925776
Right view
Flow of fuel and of air through the twin turbocharger arrangement
(4) Throttle
(5) AftercoolerThe compressed air/fuel mixture flows to the electronically controlled throttle (4). The ECM issues a command signal to the throttle actuator via the CAN data link. The signal is based on the desired engine speed. The throttle controls the volume of the air/fuel mixture that flows through aftercooler (5).The temperature of the compressed air/fuel mixture is reduced in the aftercooler. The cooler temperature increases the density of the air/fuel mixture, which results in more efficient combustion.


Parts flange Mercruiser:

87917A 1
 
87917A 1 FLANGE ASSEMBLY (1")
02297343, 04706002, 04707333
87917A 2
 
87917A 2 FLANGE ASSEMBLY (1 1/8")
02297343, 04706002, 04707333
87917A 3
 
87917A 3 FLANGE ASSEMBLY (1 1/4")
02297343, 04706002, 04707333
87917A 4
 
87917A 4 FLANGE ASSEMBLY (1 3/8")
02297343, 04706002, 04707333
87917A 5
 
87917A 5 FLANGE ASSEMBLY (1 1/2")
02297343, 04706002, 04707333
854094
FLANGE ASSEMBLY-REAR
854094 FLANGE ASSEMBLY-REAR
428B116KD, 442B115KD, 4A72040ND
811379001
FLANGE ASSEMBLY, Front
811379001 FLANGE ASSEMBLY, Front
40280001D, 40280002D, 40420002D, 4C72040TD
884011002
 
884011002 FLANGE ASSEMBLY, Rear-Without Bushing
40280001D, 40280002D, 40420002D, 4C72040TD
Back to top