Variable geometry turbine
US-2015361875-A1 · Dec 17, 2015 · US
US9353677B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9353677-B2 |
| Application number | US-201313973737-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 22, 2013 |
| Priority date | Aug 28, 2012 |
| Publication date | May 31, 2016 |
| Grant date | May 31, 2016 |
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A control apparatus calculates an upstream side pressure and temperature on an upstream side of a turbine impeller and a turbine flow rate, and calculates an upper limit threshold value of an opening degree level of a variable nozzle of a turbo supercharger such that a turbine pressure ratio is equal to or less than a predetermined ratio on a basis of the turbine flow rate and a pressure ratio•turbine flow rate characteristic. The pressure ratio•turbine flow rate characteristic is pre-stored information indicating a relationship between the turbine pressure ratio, the turbine flow rate, and the opening degree level of the variable nozzle. The control apparatus controls an opening degree of the variable nozzle so as to be an opening degree equal to or less than the upper limit threshold value.
Opening claim text (preview).
This invention claims: 1. A control method of an internal-combustion engine having a turbo supercharger with a variable nozzle capable of adjusting a flow velocity of gas exhausted to a turbine impeller, and an opening degree adjustment device configured to adjust an opening degree of the variable nozzle, the method executed by a control apparatus comprising the steps of: determining a fuel flow rate according to an injection command signal sent to an injector for injecting fuel in the internal-combustion engine and a number of revolutions of the internal-combustion engine according to a detection signal from an internal-combustion engine revolution number detection device; determining an upstream side pressure on an upstream side of the turbine impeller; determining an upstream side temperature on the upstream side of the turbine impeller; determining a turbine flow rate of gas flowing toward the turbine impeller; determining an upper limit threshold value of an opening degree level of the variable nozzle such that a turbine pressure ratio is equal to or less than a predetermined ratio according to the turbine flow rate and a pressure ratio•turbine flow rate characteristic, wherein the turbine pressure ratio is a ratio of the upstream side pressure to a downstream side pressure of the turbine impeller, wherein the pressure ratio•turbine flow rate characteristic is pre-stored information indicating a relationship between the turbine pressure ratio, the turbine flow rate, and the opening degree level of the variable nozzle; controlling an opening degree of the variable nozzle to be the opening degree level equal to or less than the upper limit threshold value, wherein the control apparatus determines the upstream side pressure according to an intake air flow rate received in the internal-combustion engine, the fuel flow rate, and an atmospheric pressure, wherein the control apparatus determines the upstream side temperature according to an injection quantity, the intake air flow rate, and the fuel flow rate and wherein the control apparatus determines the turbine flow rate according to the fuel flow rate, the intake air flow rate, the upstream side pressure, and the upstream side temperature. 2. A control apparatus of an internal-combustion engine comprising: a turbo supercharger having a variable nozzle capable of adjusting a flow velocity of gas exhausted to a turbine impeller; a controller configured to adjust an opening degree of the variable nozzle; a memory configured to store a pressure ratio•turbine flow rate characteristic indicating a relationship between a turbine pressure ratio, a turbine flow rate, and an opening degree level of the variable nozzle, wherein the turbine pressure ratio is a ratio of a pressure on an upstream side of the turbine impeller to a pressure on a downstream side of the turbine impeller; and the controller configured to detect an intake air flow rate received in the internal-combustion engine based on a detection signal from an air flow rate detecting sensor, the controller configured to detect an injection quantity of fuel into the internal-combustion engine according to an injection command signal sent to an injector for injecting the fuel into the internal-combustion engine, the controller configured to detect a number of revolutions of the internal-combustion engine according to a detection signal from an internal-combustion engine revolution number detection device, the controller configured to detect an atmospheric pressure based on a detection signal from an atmospheric pressure sensor, the controller configured to determine a fuel flow rate according to the injection quantity and the internal-combustion engine revolution number, the controller configured to determine an upstream side pressure on the upstream side of the turbine impeller, the controller configured to determine an upstream side temperature on the upstream side of the turbine impeller, the controller configured to determine the turbine flow rate, the controller configured to determine an upper limit threshold value of the opening degree level of the variable nozzle such that the turbine pressure ratio is equal to or less than a predetermined value according to the turbine flow rate and the pressure ratio•turbine flow rate characteristic, the controller configured to adjust the opening degree of the variable nozzle to be the opening degree level equal to or less than the upper limit threshold value by using the opening degree adjustment device wherein the controller is configured to determine the upstream side pressure according to the intake air flow rate, the fuel flow rate, and the atmospheric pressure, wherein the controller is configured to determine the upstream side temperature according to the injection quantity, the intake air flow rate, and the fuel flow rate, and wherein the controller is configured to determine the turbine flow rate according to the fuel flow rate, the intake air flow rate, the upstream side pressure, and the upstream side temperature.
the characteristics being exhaust temperatures · CPC title
by measuring intake air flow · CPC title
for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title
by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title
with determination means using an estimation · CPC title
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