Function of exhaust gas turbocharger: - ra09006020050x(0050)
Engines 602.96, 603.96, 603.971 TURBO in Models 124, 126, 140, 201 (model 463.3 : for deviations see introductory notes)
| Engine | Designation | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| 602.96 | Garrett TB 025 KKK K14 (2) Garret T 025 (4)) |
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| 603.96 | Garrett TB 03 (1)(3) or T 03 (1)(3) KKK K24 (1)(3) KKK 24 (5) |
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| 603.971 | Garrett TB 03 | ||||||||||
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Engine 602.961, Garrett TB 025
Engine 603.96, Garrett TB 03
Garrett TB 03 with air recirculation valve
KKK-K24 with air recirculation valve
General
The exhaust gas turbocharger (ATL) is a turbine machine. The flow energy of the engine exhaust gas is used for driving the turbine, which in turn drives the compressor via a shaft. The ATL is installed between the exhaust manifold and the exhaust pipe. It is connected to the engine oil circuit for lubrication and cooling.
A charge pressure control valve, fitted to the turbine housing or separately, ensures that a charge pressure of 0.95 bar is not exceeded. If the boost pressure control valve is faulty, engine failure is prevented by means of an engine overload protection (pay attention to note).
The exhaust gases of the engine are passed through the exhaust manifold into the turbine housing (h) and impinge on the turbine wheel (i). The flow energy of the exhaust gases starts the turbine wheel (i) rotating. This causes the compressor wheel (d) which is connected via the shaft (n) to the turbine wheel (i) to be driven at the same speed. The maximum rotation speed is approx. 135 000 rpm. The fresh air drawn in by the compressor wheel (d) is precompressed and passed to the engine.
Discontinuation of engine overload protection.
| Model | Engine | Engine end no. Manual transmission | Engine end no. Automatic transmission |
|---|---|---|---|
| 124.128/188 | 602.962 | 027382 | - |
| 124.333/393 | 603.963 | - | 004004 |
| Model | Engine | Engine end no. Automatic transmission |
|---|---|---|
| 124.128/188 | 602.962 | 017181 |
| 124.133/193 | 603.960 | 046668 |
Functional diagram turbocharger KKK K24 (Engine 603.96)
Function diagram
Air Recirculation Valve
(refer also to EDS Operation No. 07.1-010).
In order to create more favorable combustion conditions for the trap oxidizer, the air recirculation valve is continuously opened or closed in accordance with the performance
characteristic map.
After the closing operation, a residual vacuum of approx. 30 mbar is retained at the air circulation valve.
Function diagram turbocharger KKK with air circulation valve
California
Model year 1986/87
Charge Pressure Control Valve (KKK)
To prevent the charge pressure rising above a certain level, a charge pressure control valve (a) is attached to the turbine housing (h). The charge pressure is tapped at the compressor housing and passed through the connecting hose (14) to the charge pressure control valve. When the charge pressure is reached, the charge pressure valve begins to open and allows the exhaust gas to flow along the bypass passage (C). Part of the exhaust gas is now flowing directly to the exhaust pipe, with the result that the charge pressure remains at a constant level.
Charge pressure diagram - full load
Boost pressure control by means of vacuum-controlled boost pressure control valve Engine 602.96 Model Year 1990
Function diagram
Boost pressure control by means of vacuum-controlled boost pressure control valve Engine 602.96 as of Model Year 1991,
as of Model Year 1992
Engine 603.971 as of Model Year 1992
Function diagram
Function diagram exhaust gas turbocharger
Boost pressure control valve vacuum unit
With the boost pressure control, the bypass flap (a) from the turbocharger is opened with the controlled vacuum from the boost pressure control/vacuum control flap vacuum transducer (Y31/5), engine 602.96, or from the boost pressure control vacuum transducer (Y31/4), engine 603.971. The flap is operated by the control linkage (b).
Idling and Lower Part Load
No compression occurs during idling and in the lower part load, the engine is operating as a naturally aspirated engine.
Upper Part Load and Full Load
As the engine load and speed increases, e.g. with an increase in the exhaust gas flow, the turbine wheel (i) is accelerated with the result that the compressor wheel (d) produces a charge pressure up to a certain value. The compressed charge air is passed through the charge air pipe to the individual cylinders. The charge pressure allows increased quantity of fuel to flow through the ALDA unit at the injection pump.
Although charge pressure exists in the deceleration mode, fuel injection is stopped as a result of the control rod position (decel fuel cutoff).