838971 Volvo.Penta Coolant pipe


838971 Coolant pipe Volvo.Penta AD30A; AQAD30A; MD30A, MD31A; TMD31A; TMD31B, MD40A; TMD40A; TMD40B, TMD41A; TMD41B; D41A Coolant
838971 Coolant pipe Volvo Penta
Rating:
103

Buy Coolant pipe 838971 Volvo Penta genuine, new aftermarket parts with delivery
Number on catalog scheme: 12
 

Volvo Penta entire parts catalog list:

AD30A; AQAD30A; MD30A; TAMD30A; TMD30A; AD30; AQAD30; MD30; TAMD30; TMD30
MD31A; TMD31A; TMD31B; TAMD31A; TAMD31B; AD31; AQAD31A; AD31B; 290A; DP-A; DP-B; DP-A1; DP-B1; SP-A; SP-A1
MD40A; TMD40A; TMD40B; TMD40C; AQD40A; TAMD40A; TAMD40B; AD40B; AQAD40A; AQAD40B
TMD41A; TMD41B; D41A; D41B; TAMD41A; TAMD41B; AQAD41A; AD41A; AD41B; 290A; DP-A; DP-B; DP-A1; DP-B1; SP-A; SP-A1; AD41BJ; AD41; AD41P-B; D41; TAMD41

Information:

Engine Design
CYLINDER, VALVE AND INJECTION PUMP LOCATIONBore ... 137.2 mm (5.40 in.)Stroke ... 152.4 mm (6.00 in.)Number and Arrangement of Cylinders ... V-8Firing Order (Injection Sequence) ... 1, 8, 4, 3, 6, 5, 7, 2Rotation of Crankshaft (when seen from flywheel end) ... counterclockwiseRotation of Fuel Pump Camshaft (when seen from pump drive end) ... counterclockwise Front end of engine is opposite to flywheel end. Left side and right side of engine are as seen from flywheel end. No. 1 cylinder is the front cylinder on the left side. No. 2 cylinder is the front cylinder of the right side.Fuel System
This engine has a pressure type fuel system. There is one injection pump and one injection valve for each cylinder. The injection pumps are in injection pump housing (4) on the top of the engine. The injection valves are in the precombustion chambers or adapters (for engines with direct injection) under the valve covers.Fuel is pulled from fuel tank (6) through primary fuel filter (8) by fuel transfer pump (9). The transfer pump sends fuel through main fuel filter (11) to the manifold of the fuel injection pump housing.Fuel in the manifold of the injection pump housing is the supply for the injection pumps. Some of the fuel in the manifold is constantly sent through an orifice in the tee or fitting that connects the return line to the manifold. The orifice controls the pressure in the manifold and the amount of fuel that returns to the tank. The constant flow of fuel back to the tank removes air from the system.
FUEL SYSTEM SCHEMATIC
1. Fuel inlet line for the injection pump housing. 2. Damper. 3. Adapter with orifice. 4. Injection pump housing. 5. Fuel return line. 6. Fuel tank. 7. Fuel supply lines. 8. Primary fuel filter. 9. Fuel transfer pump. 10. Fuel priming pump. 11. Main fuel filter.
LOCATION OF FUEL SYSTEM COMPONENTS
1. Fuel inlet line for the injection pump housing. 2. Damper. 3. Adapter with orifice. 4. Injection pump housing. 5. Fuel return line. 7. Fuel supply line. 9. Fuel transfer pump. 12. Nut for a fuel injection line at the injection pump. 13. Fuel manifold across the injection pump housing. 14. Adapter through the valve cover base. 15. Governor.There is a surge damper (2) in the system to reduce shock loads on the fuel filter caused by high pressure from the injection pumps. On later engines, damper (2) is installed on the outlet side of fuel manifold (13). On earlier engines, damper (2) is installed on the inlet side of fuel manifold (13).The injection pumps are in time with the engine. They send fuel to the injection valves under high pressure. When the fuel pressure at the injection valve is high enough the valve opens and sends fuel into the precombustion chamber or directly into the cylinder on direct injection engines.Fuel transfer pump (9) has a bypass valve and a pressure relief valve. The bypass valve makes it possible for the priming pump to send fuel through the transfer pump. The pressure relief valve controls the maximum pressure of the fuel. When the pressure gets too high the valve opens and some of the fuel goes back to the inlet side of the pump.When there is air on the inlet side of the fuel system use priming pump (10). Operation of the priming pump fills the system with fuel. This forces the air back into the tank.Air can be removed from the fuel injection lines by loosening a fuel injection line nut (one at a time) at the valve cover base adapter. On PC Engines use the priming pump to remove the air. On DI Engines use the starter motor to turn the engine until fuel without air flows from the loosen nut. Tighten the nuts after air has been removed. Because of the check assemblies in the injection pump outlets for the DI engine, the priming pump will not give enough pressure to remove air from the fuel injection lines.
LOCATION OF FUEL SYSTEM COMPONENTS
1. Fuel inlet line to injection pump housing. 5. Fuel return line to tank. 7. Fuel supply line. 10. Fuel priming pump. 11. Main fuel filters. 16. Junction block. 17. Fuel outlet line from transfer pump and inlet line to main filters.Fuel Injection Pump
CROSS SECTION OF THE FUEL INJECTION PUMP HOUSING
1. Fuel manifold. 2. Inlet passage. 3. Check valve. 4. Pressure relief passage. 5. Pump plunger. 6. Spring. 7. Gear. 8. Fuel rack (left). 9. Lifter. 10. Link. 11. Lever. 12. Camshaft.The rotation of the cams on the camshaft (12) cause lifters (9) and pump plungers (5) to move up and down. The stroke of each pump plunger is always the same. The force of springs (6) hold lifters (9) against the cams of the camshaft.The pump housing is a "V" shape (similar to the engine cylinder block), with four pumps on each side.When the pump plunger is down, fuel from fuel manifold (1) goes through inlet passage (2) and fills the chamber above pump plunger (5). As the plunger moves up it closes the inlet passage.The pressure of the fuel in the chamber above the plunger increases until it is high enough to cause check valve (3) to open. Fuel under high pressure flows out of the check valve through the fuel line to the injection valve until the inlet passage opens into pressure relief passage (4) in the plunger. The pressure in the chamber decreases and check valve (3) closes.The longer the inlet passage is closed the larger the amount of fuel which will be forced through check valve (3). The period for which the inlet passage is closed is controlled by the pressure relief passage. The design of the passage makes it possible to change the inlet passage closed time by rotation of the plunger. When the governor moves fuel racks (8) they move gears (7) that are fastened to plungers (5). This causes a rotation of the plungers.The governor is connected to the left rack. The spring load


Parts coolant Volvo Penta:

846051
 
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852771
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852771 Coolant pipe
230A; 230B; 250A, 251A, 430; 430A; 430B, 500; 500A; 501A, 571A, AD30A; AQAD30A; MD30A, AQ131A; AQ131B; AQ131C, AQ145B, AQ151A; AQ151B; AQ151C, AQ171A; AQ171C, AQ175A, AQ200D; AQ200F; 280B, AQ205A; AQ205LB, AQ211A; DP-A; SP-A, AQ225D; AQ225E; AQ225F,
858297
 
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858482
 
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860280
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858038
 
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838798
 
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