3581542 Volvo.Penta Fuel filter


3581542 Fuel filter Volvo.Penta AD31L-A; AD31P-A; AD41L-A, KAD32P; TAMD42WJ-A; KAD43P-A, KAD42P-A; KAMD42P-A; HS1A Fuel
3581542 Fuel filter Volvo Penta
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$254.49
 

11-12-2023

LT: Roberto Parts LTD
Front Bumper Left Grille Air Duct Scoop 51747330891
Namz Custom Cycle Compatible with MINI || Replacement for R56 JCW model(-s) || OEM part number reference: 51747330891 7330891 || If you are unsure if this is correct item for your vehicle, please contact us via seller message and indicate that you are reffering to the item no: 51747330891 7330891 Need other item, but are unable to find it? You can also contact seller asking for help, please indicate what kind of item you are looking for.
Number on catalog scheme: 14
 

Volvo Penta entire parts catalog list:

AD31L-A; AD31P-A; AD41L-A; AD41P-A; D41L-A; TAMD31L-A; TAMD31M-A; TAMD31P-A; TAMD31S-A; TAMD41H-A; TAMD41H-B; TAMD41P-A; TAMD41L-A; TAMD41M-A
KAD32P; TAMD42WJ-A; KAD43P-A; KAMD43P; KAMD43P-A; KAMD43P-B; KAD44P; KAD44P-B; KAD44P-C; KAMD44P-A; KAMD44P-C; KAD300-A; KAMD300-A; HS1A; HS1E
KAD42P-A; KAMD42P-A; HS1A

Information:


Illustration 1 g01205681
Air inlet and exhaust system
(1) Exhaust manifold
(2) Fuel injector
(3) Glow plug
(4) Inlet manifold
(5) Aftercooler core
(6) Exhaust outlet
(7) Turbine side of turbocharger
(8) Compressor side of turbocharger
(9) Air inlet from the air cleaner
(10) Inlet valve
(11) Exhaust valve The components of the air inlet and exhaust system control the quality of air and the amount of air that is available for combustion. The air inlet and exhaust system consists of the following components:
Air cleaner
Turbocharger
Aftercooler
Inlet manifold
Cylinder head, injectors, and glow plugs
Valves and valve system components
Piston and cylinder
Exhaust manifoldAir is drawn in through the air cleaner into the air inlet of the turbocharger (9) by the turbocharger compressor wheel (8). The air is compressed and heated to about 150 °C (300 °F) before the air is forced to the aftercooler (5). As the air flows through the aftercooler the temperature of the compressed air lowers to about 50 °C (120 °F). Cooling of the inlet air increases combustion efficiency. Increased combustion efficiency helps achieve the following benefits:
Lower fuel consumption
Increased power output
Reduced particulate emissionFrom the aftercooler, air is forced into the inlet manifold (4). Air flow from the inlet manifold to the cylinders is controlled by inlet valves (10). There is one inlet valve and one exhaust valve for each cylinder. The inlet valves open when the piston moves down on the intake stroke. When the inlet valves open, cooled compressed air from the inlet port is forced into the cylinder. The complete cycle consists of four strokes:
Inlet
Compression
Power
ExhaustOn the compression stroke, the piston moves back up the cylinder and the inlet valves (10) close. The cool compressed air is compressed further. This additional compression generates more heat.Note: If the cold starting system is operating, the glow plugs (3) will also heat the air in the cylinder.Just before the piston reaches the Top Center (TC) position, fuel is injected into the cylinder. The air/fuel mixture ignites. The ignition of the gases initiates the power stroke. Both the inlet and the exhaust valves are closed and the expanding gases force the piston downward toward the Bottom Center (BC) position.From the BC position, the piston moves upward. This initiates the exhaust stroke. The exhaust valves open. The exhaust gases are forced through the open exhaust valves into the exhaust manifold.Exhaust gases from exhaust manifold (1) enter the turbine side of the turbocharger in order to turn turbocharger turbine wheel (7). The turbine wheel is connected to the shaft that drives the compressor wheel. Exhaust gases from the turbocharger pass through exhaust outlet (6), a silencer, and an exhaust pipe.Turbocharger
Illustration 2 g00302786
Turbocharger
(1) Air intake
(2) Compressor housing
(3) Compressor wheel
(4) Bearing
(5) Oil inlet port
(6) Bearing
(7) Turbine housing
(8) Turbine wheel
(9) Exhaust outlet
(10) Oil outlet port
(11) Exhaust inlet The turbocharger is mounted on the outlet of the exhaust manifold in one of two positions on the right side of the engine, toward the top of the engine or to the side of the engine. The exhaust gas from the exhaust manifold enters the exhaust inlet (11) and passes through the turbine housing (7) of the turbocharger. Energy from the exhaust gas causes the turbine wheel (8) to rotate. The turbine wheel is connected by a shaft to the compressor wheel (3).As the turbine wheel rotates, the compressor wheel is rotated. This causes the intake air to be pressurized through the compressor housing (2) of the turbocharger.
Illustration 3 g02269817
Turbocharger with the wastegate (if equipped)
(12) Actuating lever
(13) Wastegate actuator
(14) Line (boost pressure) When the load on the engine increases, more fuel is injected into the cylinders. The combustion of this additional fuel produces more exhaust gases. The additional exhaust gases cause the turbine and the compressor wheels of the turbocharger to turn faster. As the compressor wheel turns faster, air is compressed to a higher pressure and more air is forced into the cylinders. The increased flow of air into the cylinders allows the fuel to be burnt with greater efficiency. This produces more power.A wastegate may be installed on the turbine housing of the turbocharger. The wastegate is a valve that allows exhaust gas to bypass the turbine wheel of the turbocharger. The operation of the wastegate is dependent on the pressurized air (boost pressure) from the turbocharger compressor. The boost pressure acts on a diaphragm that is spring loaded in the wastegate actuator which varies the amount of exhaust gas that flows into the turbine.The shaft that connects the turbine to the compressor wheel rotates in bearings (4) and (6). The bearings require oil under pressure for lubrication and cooling. The oil that flows to the lubricating oil inlet port (5) passes through the center of the turbocharger which retains the bearings. The oil exits the turbocharger from the lubricating oil outlet port (10) and returns to the oil pan.Valve System Components
Illustration 4 g02263874
Valve system components
(1) Rocker arm
(2) Spring
(3) Valve
(4) Pushrod
(5) Lifter The valve system components control the flow of inlet air into the cylinders during engine operation. The valve system components also control the flow of exhaust gases out of the cylinders during engine operation.The crankshaft gear drives the camshaft gear through an idler gear. The camshaft must be timed to the crankshaft in order to get the correct relation between the piston movement and the valve movement.The camshaft has two camshaft lobes for each cylinder. The lobes operate the inlet and exhaust valves. As the camshaft turns, lobes on the camshaft cause the lifter (5) to move the pushrod (4) up and down. Upward movement of the pushrod against rocker arm (1) results in downward movement (opening) of valve (3). The opening of valve (3) compresses the valve spring (2). When the camshaft has rotated to the peak of the lobe, the valve is fully open. When the camshaft rotates further, the valve spring (2) under compression start to expand. The valve stems are under tension of the spring. The continued rotation of the camshaft causes the rocker arm (1), the pushrods (4) and the lifters (5) to move downward until the lifter reaches the bottom of the lobe. The valve (3)


Parts fuel Volvo Penta:

863940
Fuel gauge
863940 Fuel gauge
2001; 2001B; 2001AG, 230A; 230B; 250A, 251A, 430; 430A; 430B, 500; 500A; 501A, 571A, 740A; BB740A, AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, AD41D; D41D; TAMD41D, D1-13; D1-13B; D1-20, D2-55; D2-55B; D2-55C, D2-75; D2-75B; D2-75C, D4-180I-B;
840531
 
840531 Fuel filter
AD30A; AQAD30A; MD30A, AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, KAD32P; TAMD42WJ-A; KAD43P-A, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, MD6; MD6A; MD6B, TD30A; TD31ACE; TD40A
860320
Fuel pump
860320 Fuel pump
AD31D; AD31D-A; AD31XD, AD41D; D41D; TAMD41D, KAD42A; KAMD42A; HS1A, KAD42B; KAMD42B; TAMD42B, KAD42P-A; KAMD42P-A; HS1A, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, TD30A; TD31ACE; TD40A, TMD41A; TMD41B; D41A, TMD41B; D41B; TAMD41B
860447
 
860447 Fuel pipe
AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, KAD32P; TAMD42WJ-A; KAD43P-A, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, TD30A; TD31ACE; TD40A
838722
 
838722 Fuel pipe
AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, KAD32P; TAMD42WJ-A; KAD43P-A, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, TD30A; TD31ACE; TD40A
877763
Fuel filter
877763 Fuel filter
AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, AD41D; D41D; TAMD41D, D1-13; D1-13B; D1-20, D2-55; D2-55B; D2-55C, D2-75; D2-75B; D2-75C, D3-110I-A; D3-110I-B; D3-110I-C, D3-110I-D; D3-110I-E; D3-110I-F, D3-110I-G; D3-140A-G; D3-140I-G, D3-110I-H;
873808
 
873808 Fuel gauge
AD31D; AD31D-A; AD31XD, AD31L-A; AD31P-A; AD41L-A, AD41D; D41D; TAMD41D, D1-13; D1-13B; D1-20, D2-55; D2-55B; D2-55C, D2-75; D2-75B; D2-75C, D4-180I-B; D4-180I-C; D4-180I-D, D4-180I-F; D4-225A-F; D4-225I-F, D6-280A-A; D6-280A-B; D6-280A-C, D6-300A-F;
860873
 
860873 Fuel filter
AD31L-A; AD31P-A; AD41L-A, AD41D; D41D; TAMD41D, KAD32P; TAMD42WJ-A; KAD43P-A, KAD42A; KAMD42A; HS1A, KAD42B; KAMD42B; TAMD42B, KAD42P-A; KAMD42P-A; HS1A, TMD41B; D41B; TAMD41B
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