21089229 Volvo.Penta Rocker arm


21089229 Rocker arm Volvo.Penta D9A2A; D9A2A D9-425; D9A2A D9-500, D9A2A; D9A2A MG; D9A2A D9A-MG, TAD1340VE; TAD1341VE; TAD1342VE, TAD1341GE; TAD1342GE; TAD1343GE, TAD1350VE, TAD1360VE, TAD1361VE, TAD1363VE, TAD940GE; TAD941GE, TAD940VE; TAD941VE; TAD942VE Rocker
21089229 Rocker arm Volvo Penta
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27-05-2020

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Jeenda Power Rocker Arm 21089229 20999623 21154172 for Cummins QSX15 ISX15 X15 Volvo D12C D12D
Part Number:21089229 20999623 21154172 || Application:Volvo D12C D12D Cummins QSX15 ISX15 X15 || ✽100% Customer Satisfaction || ✽100% Tested Before Shipping to Ensure Product Safety, Stability and Durability || ✽Fast Shipping By Fedex/DHL,UPS
Number on catalog scheme: 10
 

Volvo Penta entire parts catalog list:

D9A2A; D9A2A D9-425; D9A2A D9-500; D9A2A D9-500 (R4); D9A2A D9-575; D9A2B D9-425; D9A2B D9-500 (R5); D9A2B D9-575; D9A2C D9-425; D9A2D D9
D9A2A; D9A2A MG; D9A2A D9A-MG
TAD1340VE; TAD1341VE; TAD1342VE; TAD1343VE; TAD1344VE; TAD1345VE; TAD1360VE; TAD1361VE; TAD1362VE; TAD1363VE; TAD1364VE; TAD1365VE; TAD1360-
TAD1341GE; TAD1342GE; TAD1343GE; TAD1344GE; TAD1345GE; TAD1350GE; TAD1351GE; TAD1352GE; TAD1353GE; TAD1354GE; TAD1355GE
TAD1350VE
TAD1360VE
TAD1361VE
TAD1363VE
TAD940GE; TAD941GE
TAD940VE; TAD941VE; TAD942VE; TAD943VE; TAD950VE; TAD951VE; TAD952VE

Information:


Illustration 1 g01122516
Air flow through the engine
(1) Exhaust outlet
(2) Air inlet
(3) Turbocharger
(4) Air cleaner
(5) Exhaust manifold
(6) Exhaust valves
(7) Inlet valves
(8) Sea water inlet to aftercooler
(9) Sea water outlet from aftercooler
(10) Aftercooler
(11) Cylinder head Clean inlet air from the air cleaner (4) is pulled through the air inlet of the turbocharger (3) by the turning of the compressor wheel. The compressor wheel causes a compression of the air. The turbocharger compresses the inlet air so that a larger volume of air can be drawn into the cylinders. This compressing of the inlet air is referred to as boost. The compression of the inlet air causes the temperature of the air to increase. The air then flows to the aftercooler (10). The aftercooler utilized cool sea water in order to cool the inlet air. Cooling of the inlet air causes the air to become more dense. This increases the combustion efficiency and the horsepower output of the engine. The air then flows from the aftercooler to the inlet manifold of the engine. When the inlet valves (7) open, the air flows into the engine cylinders. The air is mixed with the fuel for combustion. When the exhaust valves (6) open, the exhaust gases go out of the engine cylinders and into exhaust manifold (5). From the exhaust manifold, the exhaust gases flow through the blades of the turbine wheel in the turbocharger (3). This causes the turbine wheel to spin. The exhaust gases then flow out of exhaust outlet (1) of the turbocharger.Turbocharger
Two turbochargers are mounted on the rear of the engine. All of the exhaust gases from the left exhaust manifold goes through the left turbocharger, and the right turbocharger uses the exhaust from the right exhaust manifold.
Illustration 2 g01385582
Turbocharger
(12) Air inlet
(13) Compressor housing
(14) Compressor wheel
(15) Bearing
(16) Oil Inlet port
(17) Bearing
(18) Turbine housing
(19) Turbine wheel
(20) Exhaust outlet
(21) Oil outlet port
(22) Exhaust inlet All of the air that enters the engine passes through the turbocharger. All of the exhaust gases from the engine pass through the turbocharger.The exhaust gases enter turbine housing (18) through exhaust inlet (22). The exhaust gas pushes on the blades of the turbine wheel (19). The turbine wheel is connected by a shaft to the compressor wheel (14).Air that passes through the air filters enters the compressor housing air inlet (12) by the rotation of compressor wheel (14). The compressor wheel causes the inlet air to be pushed into the inlet side of the engine. Boost pressure is caused when the compressor wheel pushes more air into the inlet side 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 produces more power.When the throttle is opened, more fuel is injected into the cylinders. The combustion of this additional fuel produces greater exhaust temperature. The additional exhaust temperature causes the turbine and the compressor wheels of the turbocharger to turn faster. As the compressor wheel turns faster, more air is forced into the cylinders. The increased flow of air gives the engine more power by allowing the engine to burn the additional fuel with greater efficiency.Bearings (15) and (17) for the turbocharger use engine oil under pressure for lubrication and cooling. The oil comes in through oil inlet port (16). The oil then goes through passages in the center section in order to lubricate the bearings. This oil also cools the bearings. Oil from the turbocharger goes out through oil outlet port (21) in the bottom of the center section. The oil then goes back to the engine oil pan. Aftercooler
The C32 has a sea water aftercooler. The aftercooler is installed above the inlet manifold.
Illustration 3 g01385585
Air inlet system (typical example)
(23) Turbocharger
(24) Aftercooler
(25) Elbow on the front bonnet of the oil cooler The inlet air from the compressor side of the turbocharger flows into the aftercooler. The air passes through the core assembly which lowers the temperature as much as 38°C to 93°C (100°F to 200°F). The cooler air flows out of the bottom of the aftercooler and into the air chamber. The cooler air then flows through the inlet ports (passages) in the cylinder heads. Cooling the inlet air causes the air to become more dense. Dense air will help the engine burn the fuel more efficiently. This gives the engine more power.Valve System Components
Illustration 4 g01385586
Valve system components
(26) Rocker arm
(27) Locknut
(28) Rocker arm shaft
(29) Camshaft
(30) Valve bridge The valve train controls the flow of inlet air and exhaust gases into the cylinders and out of the cylinders during engine operation. The camshaft (29) controls the timing of the valves 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 position and the valve position.The camshaft has three camshaft lobes for each cylinder. One camshaft lobe operates the inlet valves. One camshaft lobe operates the exhaust valves. One camshaft lobe operates the unit injector. The camshaft lobes cause the follower on the rocker arm in order to actuate the valves and the unit injector.Each cylinder has two inlet valves and two exhaust valves. Valve springs hold the valves closed and the valve springs resist the opening of the valves. This ensures that the valves will close at high rpm and under high boost pressures. Valve rotators cause the valves to rotate while the engine is running. The rotation of the valves prevents the valves from burning by constantly changing the contact area of the valve face and the valve seat. This rotation gives the valves longer service life.


Parts rocker Volvo Penta:

21301512
 
21301512 Rocker arm, fuel injector
D11A-A; D11A-B; D11A-C, D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D13B-E MG (FE), D9A2A; D9A2A D9-425; D9A2A D9-500, D9A2A; D9A2A MG; D9A2A D9A-MG, TAD940GE; TAD941GE, TAD940VE; TAD941VE; TAD942VE
21654344
 
21654344 Rocker arm
D11A-A; D11A-B; D11A-C, D9A2A; D9A2A D9-425; D9A2A D9-500, D9A2A; D9A2A MG; D9A2A D9A-MG, TAD940GE; TAD941GE, TAD940VE; TAD941VE; TAD942VE
20742703
 
20742703 Rocker arm, exhaust
D12D-A MG; D12D-E MG, D12D-A MH; D12D-B MH; D12D-C MH, D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D13B-E MG (FE), TAD1240GE; TAD1241GE; TAD1242GE, TAD1340VE; TAD1341VE; TAD1342VE, TAD1341GE; TAD1342GE; TAD1343GE, TAD1350VE, TAD1360VE
20510623
 
20510623 Rocker arm shaft
D13B-A MP; D13B-B MP; D13B-C MP, D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D13B-E MG (FE), D13B-J MP; D13B-M MP, TAD1340VE; TAD1341VE; TAD1342VE, TAD1341GE; TAD1342GE; TAD1343GE, TAD1350VE, TAD1360VE, TAD1361VE, TAD1363VE, TAD1371VE
21260905
Rocker arm, intake
21260905 Rocker arm, intake
D13B-E MH; D13B-E MH (FE); D13B-N MH, D13B-F MG; D13B-E MG; D13B-E MG (FE), TAD1340VE; TAD1341VE; TAD1342VE, TAD1341GE; TAD1342GE; TAD1343GE, TAD1350VE, TAD1360VE, TAD1361VE, TAD1363VE
1360_101
1361_100
1363_101
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