Abstract: Integrated supercharger module having a low-pressure charging device (2) having a low-pressure compressor housing (4), a high-pressure charging device (3) having a high-pressure compressor housing (5), a turbine (9) and a cooler arrangement, wherein the low-pressure charging device (2), the high-pressure charging device (3), the turbine (9) and the cooler arrangement form a structural unit.

Abstract: A crankcase for an internal combustion engine with two side walls, an upper surface and a first end face, where the side walls, the upper surface, and the first end face are joined with one another as a single piece. The crankcase is open at the second end face, and an adapter flange detachably seals the second end face of the crankcase from the outside environment.

Abstract: Integrated supercharger module having a low-pressure charging device (2) having a low-pressure compressor housing (4), a high-pressure charging device (3) having a high-pressure compressor housing (5), a turbine (9) and a cooler arrangement, wherein the low-pressure charging device (2), the high-pressure charging device (3), the turbine (9) and the cooler arrangement form a structural unit.

Abstract: A crankcase for an internal combustion engine with two side walls, an upper surface and a first end face, where the side walls, the upper surface, and the first end face are joined with one another as a single piece. The crankcase is open at the second end face, and an adapter flange detachably seals the second end face of the crankcase from the outside environment.

Abstract: In a bottom plate for closing a crankcase of an internal combustion engine wherein the bottom plate includes openings and channels for collecting and conducting fluids, the bottom plate consists of a number of individual plates which are joined together after the channels and openings have been cut into the individual plates by laser beam cutting or water beam cutting.

Abstract: In a bottom plate for closing the crankcase of an internal combustion engine including coolant and lubricant flow channels integrated into the bottom plate which consists of individual plates stacked on top of one another, a heat exchanger, which consists of heat exchanger plates stacked on top of one another as disposed on the bottom plate so as to form at least one common chamber therewith for transferring at least one of coolant and lubricant between the bottom plate and the heat exchanger.

Abstract: In a bottom plate for closing a crankcase of an internal combustion engine wherein the bottom plate includes openings and channels for collecting and conducting fluids, the bottom plate consists of a number of individual plates which are joined together after the channels and openings have been cut into the individual plates by laser beam cutting or water beam cutting.

Abstract: A cover plate is provided for closing a crankcase of an internal-combustion engine on its underside. The cover plate has a suction point for collecting lubricant from the crankcase. With respect to the crankcase, the suction point is closed off by a screen plate. This screen plate comprises a first area with passage openings for the lubricant and a second area which is impervious to the lubricant. The screen plate has the effect that a reliable lubricant intake from the suction point is ensured even in the event of a tilt of the internal-combustion engine.

Abstract: In a bottom plate for closing the crankcase of an internal combustion engine including coolant and lubricant flow channels integrated into the bottom plate which consists of individual plates stacked on top of one another, a heat exchanger, which consists of heat exchanger plates stacked on top of one another as disposed on the bottom plate so as to form at least one common chamber therewith for transferring at least one of coolant and lubricant between the bottom plate and the heat exchanger.

Abstract: A method for plastic molding of a hub recess for a fast-running turbine component is provided. The plastic molding of the hub recess occurs by hydraulic expansion, by way of a hydraulic fluid introduced into the hub recess of the turbine component under high pressure.

Abstract: A cover plate is provided for closing a crankcase of an internal-combustion engine on its underside. The cover plate has a suction point for collecting lubricant from the crankcase. With respect to the crankcase, the suction point is closed off by a screen plate. This screen plate comprises a first area with passage openings for the lubricant and a second area which is impervious to the lubricant. The screen plate has the effect that a reliable lubricant intake from the suction point is ensured even in the event of a tilt of the internal-combustion engine.

Abstract: A method for plastic molding of a hub recess for a fast-running turbine component is provided. The plastic molding of the hub recess occurs by hydraulic expansion, by way of a hydraulic fluid introduced into the hub recess of the turbine component under high pressure.

Abstract: An exhaust system for a supercharged internal-combustion engine in which of the exhaust-gas-carrying components, the exhaust gas pipes leading from the cylinder outlets to the turbines, or the turbines, or the turbines and the exhaust gas pipes are arranged jointly in an exhaust-gas-tight housing. Openings in the exhaust-gas-carrying components cause the space formed between the exhaust-gas-carrying components and the housing to be filled with exhaust gas. By way of a bypass pipe which is connected with the space and leads to the turbine, exhaust gas can be blown off from the space. A blow-off valve is arranged in the bypass pipe.

Abstract: A throttle flap construction (12) is installed in an exhaust gas duct (11). For the installation the duct wall is provided with a radially facing, axially extending narrow slot (20) centrally provided with a circular opening so that a flap disk (14) may pass radially inwardly through the slot while a bearing portion (17) of the flap disk (14) may pass through the central circular opening. During installation, the flap disk (14) extends vertically when the throttle unit is inserted, a cover (16) is bolted to a flange (11A) surrounding the slot (20) and the central opening (21). Thus, the duct (11) can be properly sealed without cutting entirely through the duct in a radial plane.

Abstract: An exhaust gas turbocharger having rotor runners disposed in roller bearings protects the roller bearings from shocks and vibrations by a pressure-oil-filled oil film damper. By a shut-off device arranged in the main lubricating oil duct, the lubricating oil supply of the roller bearings is shut off when the rotor runners are stopped. However, the pressure oil supply of the oil film damper remains operative so that the oil film damper retains its operability.

Abstract: A sealing device has two circumferentially fixed sealing rings which, together with a common ring groove in a turbo-machine shaft for both sealing rings, result in a labyrinth seal between the sealing gas space and the lubricating-oil relief space and between the sealing gas space and the rotor disk space. In the event of a disturbance of the sealing gas supply, both sealing rings are supported at a gradation of a shaft lead-through bore which prevents a total wearing-out of the sealing rings.

Abstract: During idling or partial load of the reciprocating piston-internal combustion engine, the exhaust gas turbocharger (18) is shut-down and the fuel supply is interrupted with some cylinders (12). An optimum charging air supply matched to the operating condition of the reciprocating piston-internal combustion engine results by a controllable shifting device (32) in the charging air line section (14) of the shut-down cylinders (12). The passage from the charging air line (19) to the charging air line section (14) is closed by the shifting device (32) during operating periods with interruption of the fuel supply to the cylinders (12). At the same time, a passage opens from a suction opening (33) to the charging air line section (14), through which the air requirement of the disabled cylinders (12) is covered. The interconnected exhaust gas turbocharger (17) thereby operates in a favorable operating range.

Abstract: A sealing arrangement between a shaft and a housing of a fluid flow engine consists of a blocking gas space acted upon with blocking gas, which is delimited by two sealing rings guided in annular grooves of the shaft and radially sealingly abutting at the shaft through-bore. In order to avoid operation-endangering wear of the sealing rings in case of failure of the blocking gas supply, the shaft through-bore is constructed with three diameter regions mutually offset by right angle steps. The steps form each an axial support for the coordinated sealing ring which comes into action when a permissive initial wear has occurred at the sealing ring.

Abstract: A bearing support of the rotor of an exhaust gas turbocharger with two inwardly disposed roller bearings in which, to assure a long length of life of the bearing, the roller members of the bearings are pressed constantly against their races so that they roll off along the same in a defined manner and no wear occurs as a result of sliding or load changes. The abutment forces which act at the bearings are produced by one or several pneumatic cylinders whose pressure spaces are preferably in connection with a gas space of the compressor. As the magnitude of the charging pressure of the compressor is dependent on the rotational speed, the abutment forces are also variable with the rotational speed. The piston surfaces of the pressure cylinders are so matched that at low rotational speeds as low as possible a bearing friction loss results whereas the abutment forces are still sufficiently high to assure a damage-free bearing operation.

Abstract: A piston internal combustion engine with two-stage supercharging in which two exhaust gas turbocharger groups consisting each of a high pressure and low pressure exhaust gas turbocharger, supply the piston internal combustion engine with charging air. One exhaust gas turbocharger group is constructed to be connected and disconnected, whereby a closure device is arranged in the exhaust gas line of the high pressure exhaust gas turbocharger and a check valve is arranged in the suction line of the low pressure exhaust gas turbocharger. For connecting and disconnecting the exhaust gas turbocharger group at partial load, the cross section of the closure devices is controlled. In order to avoid nonpermissive excess rotational speeds in the rotating parts of the high pressure exhaust gas turbocharger during a connecting operation, charging air is conducted back from the pressure side to the suction side by way of a controllable bypass line between the suction and pressure line of the high pressure compressor.