Model | 963 |
with code G3Y (Turbo retarder clutch) | |
with code V2B (Actros model generation 5) | |
Model | 963 |
with code G3Y (Turbo retarder clutch) | |
with code V2F (Actros S/M cab, model generation 5) | |
Model | 964 |
with code G3Y (Turbo retarder clutch) | |
with code V2J (Arocs model generation 5) | |
Model | 964 |
with code G3Y (Turbo retarder clutch) | |
with code V3L (Actros BM964 model generation 5) |
Power flow diagram when driving off or when maneuvering |
1 | Flywheel |
2 | Dry clutch |
3 | Clutch pressure plate (with support for power take-off) |
4 | Hollow shaft |
5 | Turbo retarder clutch |
6 | Impeller |
7 | Turbine wheel |
8 | Turbine wheel brake |
9 | Sprag clutch |
10 | Transmission input shaft |
W25.50-1070-76
Starting-off function
To drive off, the engine output is transferred hydrodynamically, but without increasing torque in the turbo-retarder clutch (5), from the impeller (6) to the turbine wheel (7). Output is transferred to the transmission input shaft (10) through the blocked sprag clutch (9) in the turbine wheel (7). Under normal driving conditions the turbo retarder clutch (5) is not filled with oil. When starting off, it is charged with the amount of oil to match the accelerator pedal position. The fast change in its volumetric efficiency enables the fluid coupling (5) to achieve short reaction times to changing torque requests. It converts the engine torque into traction swiftly and tangibly. As soon as the slip between the impeller (6) and turbine wheel (7) has been sufficiently reduced, the clutch actuator closes the dry clutch (2). During this closing procedure, this acts as a lockup clutch for the fluid coupling (5). Once the dry clutch (2) has been completely closed, the oil is completely drained from the fluid coupling's (5) working chamber. The sprag clutch (9) is decoupled, and the turbine wheel (7) then rotates loosely only on the transmission input shaft (10). During the starting-off procedure, the fluid coupling (5) actuation is indicated by a symbol in the multifunction display or the instrument cluster control unit screen. The handling characteristics are equivalent to that of a conventional clutch/transmission combination. If the accelerator pedal is not pressed, the vehicle will not roll-start on a level piece of ground.
Maneuvering function
After operating the maneuvering switch, the working chamber in the fluid coupling (5) is partially filled with oil. In the lower start-off gears an intended crawling of the vehicle is made possible by releasing the service brake. In the maneuvering mode, the turbo-retarder clutch (5) responds extremely sensitively to any changes in the accelerator pedal position. At the same time, the signal range of the accelerator pedal travel is spread apart and the engine speed is limited to a maximum 1300 rpm. The actuated maneuvering mode is visually indicated by an indicator lamp on the maneuvering switch. In the maneuvering mode any closing of the dry clutch (2) is suppressed.
W25.50-A010-79
Shown on vehicle with code J6A (Classic cockpit) |
6 | Impeller | A1 | Instrument cluster (ICUC) control unit | Y23 | Proportioning valve | ||
7 | Turbine wheel | A1 p1 | Multifunction display | Y24 | Fast emptying solenoid valve | ||
8 | Turbine wheel brake | A3a | Drive control control unit (CPC5) | Y48 | Turbine wheel brake solenoid valve | ||
9 | Sprag clutch | A5 | Transmission control (TCM) control unit | A | Working chamber oil feed | ||
11 | Oil separator | A69 | Turbo retarder clutch control unit (CCM) | B | Working chamber oil return | ||
12 | Shaped breather | B88 | Oil reservoir pressure sensor | C | Air duct (for aeration and ventilation) | ||
13 | Filter | B89 | Ventilation pressure sensor | D | Coolant circuit | ||
14 | Outlet restrictor | B90 | Oil temperature sensor | E | Oil duct (oil supply for turbine wheel brake) | ||
15 | Heat exchanger | B91 | Coolant temperature sensor | F | Compressed air supply | ||
16 | Outlet check valve | B93 | Turbine wheel rpm sensor | G | Unpressurized line | ||
17 | Oil feed shutoff valve | CAN 3 | Frame CAN | a | Consumer circuit | ||
18 | Oil supply chamber | CAN 4 | Drive train CAN |
W25.50-A000-79
Shown on vehicle with code J6B (Multimedia cockpit) or code J6C (Multimedia cockpit, interactive) |
6 | Impeller | A3a | Drive control control unit (CPC5) | CAN 17 | User interface CAN | ||
7 | Turbine wheel | A5 | Transmission control (TCM) control unit | Y23 | Proportioning valve | ||
8 | Turbine wheel brake | A69 | Turbo retarder clutch control unit (CCM) | Y24 | Fast emptying solenoid valve | ||
9 | Sprag clutch | A151 | Instrument cluster (IC) control unit | Y48 | Turbine wheel brake solenoid valve | ||
11 | Oil separator | A153 | Instrument cluster screen (ICS) control unit | A | Working chamber oil feed | ||
12 | Shaped breather | B88 | Oil reservoir pressure sensor | B | Working chamber oil return | ||
13 | Filter | B89 | Ventilation pressure sensor | C | Air duct (for aeration and ventilation) | ||
14 | Outlet restrictor | B90 | Oil temperature sensor | D | Coolant circuit | ||
15 | Heat exchanger | B91 | Coolant temperature sensor | E | Oil duct (oil supply for turbine wheel brake) | ||
16 | Outlet check valve | B93 | Turbine wheel rpm sensor | F | Compressed air supply | ||
17 | Oil feed shutoff valve | CAN 3 | Frame CAN | G | Unpressurized line | ||
18 | Oil supply chamber | CAN 4 | Drive train CAN | a | Consumer circuit |
Actuation process
When driving off the required specified torque is forwarded by the transmission control unit to the fluid coupling control unit over the drive train CAN. The fluid coupling control unit sends an electrical signal with the required amperage to the proportional valve.
The proportional valve is connected to the consumer circuit (a) of the vehicle's compressed air system. As soon as the proportional valve receives an electrical input signal from the fluid coupling control unit, the signal is converted into pneumatic actuating pressure. This acts through the air duct (C) on the oil in the fluid reservoir (18).
The oil reservoir chamber pressure sensor records the pneumatic actuating pressure, and converts it into an electrical signal. This is then made available to the fluid coupling control unit to regulate the desired oil charging process of the working chamber between the impeller (6) and the turbine wheel (7), to therefore also regulate the starting torque.
The opened oil feed shutoff valve (17) and the working chamber oil feed (A) enable the oil to flow through intake ports in the impeller (6) into the working chamber between the turbine wheel (7) and the impeller (6).
The hollow shaft (4) driven and rotating impeller (6) accepts the oil into its rotary motion and accelerates it. The oil is diverted at the turbine wheel (7) and directed back to the impeller (6) at the inside diameter of the working chamber. This induces the turbine wheel (7) to rotate with the impeller (6), whereupon the outlet pressure is then generated.
The air in the working chamber is displaced by the oil and routed over the profile ventilation (12) and oil separator (11) to the atmosphere. The profile ventilation (12) is then closed in the maximum filling range.
The heated oil flows through the working chamber oil return (B) and the outlet restrictor (14) into the heat exchanger (15), where it dissipates the absorbed thermal energy into the coolant circuit (D). Depending on the operating condition, the cooled-down oil is then routed back over the heat exchanger (15) and the outlet check valve (16) to the working chamber, or it flows back into the reservoir (18).
The rotary motion of the turbine wheel (7) is transferred through the sprag clutch (9) to the transmission input shaft (10) and the vehicle moves off.
Once the bypass point is reached, the proportional valve is deactivated. The actuating pressure in the reservoir (18) is reduced through the air duct (C) and the proportional valve. It is vented through a separate air duct in the housing gap between the fluid coupling (5) and the transmission.
At the same time, the quick drain solenoid valve is activated and pressure is applied to the oil feed shutoff valve (17). This causes the oil feed shutoff valve (17) to close whereupon the oil flow to the working chamber is then interrupted. The "residual oil" in the working chamber is returned through the heat exchanger (15) and the outlet check valve (16) in the reservoir (18). Once the working chamber has been drained, the quick drain solenoid valve is deactivated, whereupon the oil feed shutoff valve (17) is opened through a return spring.
The profile ventilation (12) is now opened again, and the working chamber is connected through the oil separator (11) with the atmosphere. The outlet check valve (16) is closed again, to prevent the oil in the heat exchanger (15) draining into the reservoir (18).
The dry clutch (2) connected to the flywheel (1) is closed. The transmission input shaft speed is then sped up to match the engine rpm and thereby exceeds the speed of the turbine wheel (7). The sprag clutch (9) opens and the turbine wheel (7) is decoupled from the transmission input shaft (10).
Throughout the entire starting-up procedure oil flows to the turbine wheel brake (8) through the oil duct (E). This oil flow ensures that he required lubrication is provided.
Instrument cluster control unit (ICUC), component description | Only on vehicles with code J6A (Classic cockpit) | ||
Drive control (CPC) control unit, component description | A3a | ||
Transmission control unit (TCM), component description | Only on vehicles with transmission 715 with code G5G (Mercedes PowerShift 3) | ||
Component description for turbo retarder clutch (CCM) control unit | A69 | ||
Instrument cluster (IC) control unit component description | Only for vehicles with code J6B (Multimedia cockpit) or with code J6C (Multimedia cockpit, interactive) | ||
Instrument cluster (ICS) screen, component description | Only for vehicles with code J6B (Multimedia cockpit) or with code J6C (Multimedia cockpit, interactive) | ||
Pressure sensor for oil reservoir chamber component description | B88 | ||
Ventilation pressure sensor component description | B89 | ||
Oil temperature sensor component description | B90 | ||
Component description for coolant temperature sensor | B91 | ||
Turbine wheel rpm sensor, component description | B93 | ||
Proportional valve component description | Y23 | ||
Quick drain solenoid valve component description | Y24 | ||
Turbine wheel brake solenoid valve component description | Y48 | ||
Heat exchanger, component description | |||
Profile ventilation, component description | |||
Outlet check valve, component description | |||
Oil feed shutoff valve, component description | |||
Oil separator component description | |||
Turbine wheel component description | |||
Impeller component description | |||
Turbine wheel brake component description |
Referenced documents
- gf2550w1000h Turbine wheel brake component description
- gf2550w1001h Impeller component description
- gf2550w1002h Turbine wheel component description
- gf2550w1003h Proportional valve component description
- gf2550w1004h Pressure sensor for oil reservoir chamber component description
- gf2550w1005h Ventilation pressure sensor component description
- gf2550w1006h Oil separator component description
- gf2550w1007h Oil temperature sensor component description
- gf2550w1008h Component description for coolant temperature sensor
- gf2550w1009h Quick drain solenoid valve component description
- gf2550w1010h Turbine wheel brake solenoid valve component description
- gf2550w1012h Outlet check valve, component description
- gf2550w1014h Turbine wheel rpm sensor, component description
- gf2550w1015h Heat exchanger, component description
- gf2550w1017h Profile ventilation, component description
- gf2550w1018h Component description for turbo retarder clutch (CCM) control unit
- gf2550w1021h Oil feed shutoff valve, component description
- gf2621w3002h Transmission control unit (TCM), component description
- gf3035w4105h Drive control (CPC) control unit, component description
- gf5421w6004f Instrument cluster (IC) control unit component description
- gf5430w6001h Instrument cluster control unit (ICUC), component description
- gf5430w6006f Instrument cluster (ICS) screen, component description