1. An electronic control device, comprising:
a first switching element for driving a load, connected in series with the load between a power source and ground;
a second switching element for taking ONOFF control of the first switching element, connected to the control terminal of the first switching element;
a pulse generator for controlling the second switching element; and
a control circuit including a trigger circuit having a capacitor connected between the pulse generator and the second switching element, and a latch circuit connected via a diode, between a fist junction that is a connecting point of the load with the first switching element and the control terminal of the second switching element; wherein
when the pulse generator outputs a drive signal, the control circuit turns on through the trigger circuit the second switching element for a predetermined time, thereby also turning on the first switching element so as to drive the load, and in addition, holds the second switching element in an ON state through the latch circuit by a voltage generated at the fist junction, whereas when the pulse generator stops outputting the drive signal, the control circuit turns off both of the first switching element and the second switching element; meanwhile if the load is short-circuited, the control circuit turns off the second switching element through the latch circuit by the voltage generated at the fist junction even when the pulse generator is outputting the drive signal, thereby also turning off the first switching element.
2. An electronic control device according to claim 1, wherein the load is connected to the power supply side and the first switching element is connected downstream of the load.
3. An electronic control device according to claim 1, wherein the load is connected to the ground side and the first switching element is connected upstream of the load.
4. An electronic control device according to claim 2, wherein the second switching element is turned on for a predetermined time by making use of an integrating function of the capacitor used in the trigger circuit, and the first switching element is thereby also turned on so as to drive the load.
5. An electronic control device according to claim 3, wherein the second switching element is turned on for a predetermined time by making use of a differential function of the capacitor used in the trigger circuit, and the first switching element is thereby also turned on so as to drive the load.
6. An electronic control device according to claim 2, wherein the cathode of the diode included in the latch circuit is connected to the first junction between the load and the first switching element, and the capacitor included in the trigger circuit is thereby charged up without being affected by the power supply connected to the load, and in addition, a dark current is prevented from flowing into the control circuit when the electronic control device is not in operation.
7. An electronic control device according to claim 3, wherein the anode of the diode included in the latch circuit is connected to the first junction between the load and the first switching element, and the capacitor included in the trigger circuit is thereby charged up without being affected by the ground connected with the load.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. An exhaust gas turbocharger, comprising: a turbine wheel rotatably mounted about an axis of rotation, wherein the turbine wheel expands a combustion engine exhaust gas; and
a turbine housing, wherein the turbine housing includes a high-pressure region and a low-pressure region, the turbine wheel is arranged between the high-pressure region and the low-pressure region, and wherein the low-pressure region has an inner shell conducting the exhaust gas and an outer shell, which is arranged for forming an air gap insulation.
2. The exhaust gas turbocharger according to claim 1, wherein the turbine housing comprises an outlet flange for connecting the exhaust gas turbocharger to an exhaust system of the combustion engine, which with regard to the inner shell and the outer shell is a separate component, wherein the inner shell and the outer shell are connected to the outlet flange, and to each other on the outlet flange.
3. The exhaust gas turbocharger according to claim 1, wherein at least one of the inner shell and the outer shell are formed of at least one of sheet metal and a casting.
4. The exhaust gas turbocharger according to claim 1, wherein at least one guide vane is arranged in the high-pressure region between two walls located opposite each other and conducting the exhaust gas, and wherein the inner shell extends to the guide vanes and forms one of the walls conducting the exhaust gas.
5. The exhaust gas turbocharger according to claim 1, wherein the inner shell has a sliding seat, wherein on the onflow side an inner shell portion is fixedly connected to the outer shell upstream of the sliding seat, and wherein the sliding seat is adjustable relative to an inner shell portion on the outflow side and is fixedly connected to at least one of the outer shell and the outlet flange downstream of the sliding seat.
6. The exhaust gas turbocharger according to claim 1, wherein the inner shell comprises at least one bead which protrudes towards the outer shell so that the inner shell supports itself on the outer shell in the region of the bead, wherein the inner shell is connected to the outer shell in the region of the bead, and wherein the outer shell includes at least one additional bead, which protrudes towards the inner shell so that the bead of the inner shell supports itself on the additional bead of the outer shell.
7. The exhaust gas turbocharger according claim 1, wherein the turbine housing in the high-pressure region comprises a volute which with respect to the inner shell is a separate component, wherein the inner shell is connected to the volute and the outer shell is connected to at least one of the volute, the inner shell and the volute, and is integrally moulded out of the volute.
8. The exhaust gas turbocharger according to claim 1, wherein the inner shell extends to an inlet of the turbine wheel and defines a turbine wheel contour gap, which extends between the turbine wheel and the inner shell from the inlet of the turbine wheel to the outlet of the turbine wheel, and wherein the inner shell extends to an inlet of guide vanes arranged upstream of the turbine wheel and defines a guide vane contour gap, which extends between the guide vanes and the inner shell from the inlet of the guide vanes to the outlet of the guide vanes wherein at least one of the inner shell and the turbine wheel; and the inner shell, the turbine wheel and the guide vanes are produced of materials having at least one of similar and same heat expansion coefficients.
9. The exhaust gas turbocharger according to claim 1, wherein the inner shell extends to at least one of an inlet of the turbine wheel and an inlet of guide vanes arranged upstream of the turbine wheel, and wherein the inner shell downstream of the turbine wheel has a smaller wall thickness than in at least one of the region of the turbine wheel, and the region of the turbine wheel and the guide vanes.
10. The exhaust gas turbocharger according to claim 1, wherein the inner shell extends to the inlet of guide vanes arranged upstream of the turbine wheel, wherein the inner shell in the region of the guide vanes comprises at least one bead which protrudes to at least one guide vane, wherein the respective bead supports itself on the respective at least one guide vane in a dot-shaped manner, wherein the guide vanes for a variable turbine geometry are each adjustable about a swivel axis, wherein the respective bead in the region of the swivel axis supports itself on the respective guide vane in a dot-shaped manner.
11. The exhaust gas turbocharger according to claim 1, wherein guide vanes are arranged upstream of the turbine wheel, wherein the inner shell extends to an inlet of the guide vanes, wherein the guide vanes are attached to a guide vane carrier having several spacer elements, on which the inner shell in the region of the guide vanes is supported and moveable relative to the spacer elements transversely to the support direction, wherein the guide vanes for a variable turbine geometry are each adjustably arranged about a swivel axis on the guide vane carrier, and wherein the respective spacer element parallel to the swivel axes is longer than the guide vanes.
12. The exhaust gas turbocharger according to claim 1, wherein guide vanes are arranged and attached to a guide vane carrier upstream of the turbine wheel, wherein the inner shell extends over and beyond the inlet of the guide vanes to the guide vane carrier and at the inlet of the guide vanes, the guide vane carrier includes inflow openings through which the exhaust gas reaches the guide vanes, and wherein the guide vane carrier is positioned radially through the inner shell with respect to the axis of rotation.
13. The exhaust gas turbocharger according to claim 1, wherein a guide vane carrier carries several guide vanes arranged upstream of the turbine wheel and with respect to the axis of rotation is arranged axially between the turbine wheel and a bearing housing in which a driveshaft comprising the turbine wheel is rotatably mounted about the axis of rotation, wherein at least one of the outer shell and a volute of the turbine housing is fastened to the bearing housing, wherein at least one of the outer shell and the volute encloses the guide vane carrier with respect to the axis of rotation, wherein at least one of the outer shell and the volute radially positions the guide vane carrier with respect to the axis of rotation, by at least one of at least one bead protruding to the guide vane carrier and in that the inner shell extends to the bearing housing where it is fastened to the bearing housing together with at least one of the outer shell and with the volute, encloses the guide vane carrier with respect to the axis of rotation and radially positions said guide vane carrier by at least one bead protruding to the guide vane carrier.
14. The exhaust gas turbocharger according to claim 2, wherein at least one of the inner shell and the outer shell are formed of at least one of sheet metal and casting.
15. The exhaust gas turbocharger according to claim 2, wherein at least one guide vane is arranged in the high-pressure region between two walls located opposite each other and conducting the exhaust gas, and wherein the inner shell extends to the guide vanes and forms one of the walls conducting the exhaust gas.
16. The exhaust gas turbocharger according to claim 2, wherein the inner shell has a sliding seat, wherein on the onflow side an inner shell portion is fixedly connected to the outer shell upstream of the sliding seat, and wherein the sliding seat is adjustable relative to an inner shell portion on the outflow side and is fixedly connected to at least one of the outer shell and the outlet flange downstream of the sliding seat.
17. The exhaust gas turbocharger according to claim 2, wherein the inner shell comprises at least one bead which protrudes towards the outer shell so that the inner shell supports itself on the outer shell in the region of the bead, wherein the inner shell is materially connected to the outer shell in the region of the bead, and wherein the outer shell includes at least one additional bead, which protrudes towards the inner shell so that the bead of the inner shell supports itself on the additional bead of the outer shell.
18. The exhaust gas turbocharger according claim 2, wherein the turbine housing in the high-pressure region comprises a volute which with respect to the inner shell is a separate component, wherein the inner shell is materially connected to the volute and the outer shell is likewise materially connected to at least one of the volute, the inner shell and the volute, and is integrally moulded out of the volute.
19. The exhaust gas turbocharger according to claim 2, wherein the inner shell extends to an inlet of the turbine wheel and defines a turbine wheel contour gap which extends between the turbine wheel and the inner shell from the inlet of the turbine wheel to the outlet of the turbine wheel, and wherein the inner shell extends to an inlet of guide vanes arranged upstream of the turbine wheel and defines a guide vane contour gap which extends between the guide vanes and the inner shell from the inlet of the guide vanes to the outlet of the guide vanes wherein at least one of the inner shell and the turbine wheel; and the inner shell, the turbine wheel and the guide vanes are produced of materials having at least one of similar and same heat expansion coefficients.
20. The exhaust gas turbocharger according to claim 2, wherein the inner shell extends to at least one of an inlet of the turbine wheel and an inlet of guide vanes arranged upstream of the turbine wheel, and wherein the inner shell downstream of the turbine wheel has a smaller wall thickness than in at least one of the region of the turbine wheel, the region of the turbine wheel and the guide vanes.