Exhaust gas turbine type supercharger

Claim 2

An exhaust gas turbine type supercharger for an engine, the supercharger having a turbine and a compressor, a casing means for receiving said turbine, partition wall means for dividing the casing means into two scroll chambers, and means for supplying an exhaust gas to said two scroll chambers to rotate said turbine and to feed the engine with supercharged air through said compressor, said supercharger comprising a bypass passage means for connecting one of said scroll chambers to a portion downstream of said turbine, a first flow rate control valve means for controlling a flow rate of the exhaust gas passing through said bypass passage means, and a second flow rate control valve means for controlling a flow rate of the exhaust gas being fed to the other of said scroll chambers, and means for controlling said first and second flow rate control valve means in accordance with an electric signal representing an engine RPM corresponding to a supercharged pressure.

Claim 3

An exhaust gas turbine type supercharger as claimed in claim 1, wherein said first flow rate control valve means decreases the flow rate of the exhaust gas passing through said bypass passage means when said second flow rate control valve means is opened.

Claim 4

An exhaust gas turbine type supercharger for feeding an exhaust gas from cylinders of an engine to a turbine, thereby drivingly rotating the turbine to drive a compressor mounted on the same shaft as the turbine so that the compressor compresses air to be fed to the cylinders of the engine, comprising: a partition wall means for dividing a casing of said turbine into two scroll chambers; an exhaust gas flow rate control means for introducing the exhaust gas mainly into only one of said scroll chambers in a low speed/low load operation of the engine in which the supercharged pressure is lower than a first predetermined level and for introducing the exhaust gas of the engine into said two scroll chambers in a high speed/high load operation of the engine in which the supercharged pressure is higher than said first predetermined level, including an opening/closing valve interposed at an inlet of the other of said scroll chambers and a diaphragm type activator for controlling an opening degree of said opening/closing valve in response to a magnitude of said supercharged pressure; an exhaust gas bypass means for discharging to a portion downstream of said turbine a part of the exhaust gas fed to said turbine through one of said scroll chambers when the supercharged pressure is higher than a second predetermined level, including a port formed in a wall between said one of said scroll members and a downstream exhaust gas passage of said turbine, an opening/closing valve for opening and closing said port and a diaphragm type actuator for controlling an opening degree of said last mentioned opening/closing valve in response to a magnitude of said supercharged pressure; and means for controlling the exhaust gas flow rate means in response to an engine RPM signal corresponding to the supercharged pressure, wherein each of said diaphragm type actuators comprises an ON/OFF valve whose opening/closing duty is controlled in accordance with an electrical signal representing an engine RPM.

Claim 5

An exhaust gas turbine type supercharger for feeding an exhaust gas from cylinders of an engine to a turbine, thereby drivingly rotating the turbine to drive a compressor mounted on the same shaft as the turbine so that the compressor compresses air to be fed to the cylinders of the engine, comprising: a partition wall means for dividing a casing of said turbine into two scroll chambers; an exhaust gas flow rate control means for introducing the exhaust gas mainly into only one of said scroll chambers in a low speed/low load operation of the engine in which the supercharged pressure is lower than a first predetermined level and for introducing the exhaust gas of the engine into said two scroll chambers in a high speed/high load operation of the engine in which the supercharged pressure is higher than said first predetermined level, including an opening/closing valve interposed at an inlet of the other of said scroll chambers and a diaphragm type activator for controlling an opening degree of said opening/closing valve in response to a magnitude of said supercharged pressure; an exhaust gas bypass means for discharging to a portion downstream of said turbine a part of the exhaust gas fed to said turbine through one of said scroll chambers when the supercharged pressure is higher than a second predetermined level, including a port formed in a wall between said one of said scroll members and a downstream exhaust gas passage of said turbine, an opening/closing valve for opening and closing said port and a diaphragm type actuator for controlling an opening degree of said last mentioned opening/closing valve in response to a magnitude of said supercharged pressure; and means for controlling the exhaust gas flow rate means in response to an engine RPM signal corresponding to the supercharged pressure, wherein each of said diaphragm type actuators comprises an ON/OFF valve whose opening/closing duty is controlled in accordance with an electrical signal representing an engine RPM.