Methods and systems for variable geometry turbocharger control

FIELD OF THE INVENTION

0001The present invention relates generally to the field of variable geometry turbocharger design and, more particularly, to method and system for controlling the position of a variable geometry member disposed within a variable geometry turbocharger.

BACKGROUND

0002Turbochargers are devices that are frequently used to increase the output of an internal combustion engine. A typical turbocharger comprises a turbine wheel coupled to a compressor impeller by a common shaft. Exhaust gas from the engine is diverted into a turbine housing of the turbocharger and through an inlet nozzle. The exhaust gas is directed onto the turbine wheel, causing it to spin, which in turn spins the common shaft and the compressor impeller.

0003The compressor impeller is disposed within a compressor housing having an air inlet and a pressurized or boosted air outlet. The spinning compressor impeller operates to pressurize air entering the compressor housing and generate a pressurized or boosted air stream that is directed into an inlet system of the internal combustion engine. This boosted air is mixed with fuel to provide a combustible mixture within the combustion chambers of an engine. In this manner, the turbocharger operates to provide a larger air mass and fuel mixture, than otherwise provided via an ambient pressure air intake stream, that results in a greater engine output during combustion.

0004The gain in engine output that can be achieved is directly proportional to the increase in intake air flow pressure generated by the turbocharger. However, allowing the boost pressure to reach too high a level can result in severe damage to both the turbocharger and the engine, particularly when the engine has to operate beyond its intended performance range.

0005Thus, an objective of turbocharger design is to regulate or control the boost pressure provided by the turbocharger in a manner that optimizes engine power output at different engine operating conditions without causing engine damage. A known technique for regulating boost pressure is by using a turbocharger having a variable geometry member that functions to control the amount of exhaust gas directed to the turbine wheel. Turbochargers comprising such variable geometry members are referred to as variable geometry turbochargers (VGTs).

0006One type of VGT includes a variable geometry member in the form of multiple adjustable-position vanes that are positioned within the turbine housing, and that are movable within in inlet nozzle of the turbine housing to regulate the amount of exhaust gas that is passed to the turbine wheel. The vanes in this type of VGT can be opened to permit greater gas flow across the turbine wheel, causing the turbine wheel to spin at a higher speed and raise the boost pressure, or closed to restrict exhaust gas flow to the turbine, thereby reducing the boost pressure. Thus, the amount of boost pressure generated by this type of VGT can be regulated by varying the vane position so as to optimize engine output while avoiding engine damage.

0007However, it is important for purposes of obtaining the desired result from the VGT and the desired output from the engine that the variable geometry member, in this or any type of VGT, be operated in a manner that will produce the desired change. Since this operation is taking place in a dynamic system of changing VGT and engine operating parameters, it is desired that a control system be used to for the purpose of taking these dynamic operating conditions into account for the purpose of provide the desired result. Other examples of prior art devices can be found in <patcit id="pcit0001" dnum="WO0155575A"><text>WO0155575A</text></patcit> and <patcit id="pcit0002" dnum="WO0159275A"><text>WO0159275A</text></patcit>.

0008It is, therefore, desired that a control system be devised that is capable of being used with a VGT to effect a desired change in the variable geometry member disposed therein for the purpose of achieving a desired VGT and engine output.

0009The present invention discloses a method for positioning a variable geometry member in a variable geometry turbocharger coupled to an internal combustible engine, the method comprises the steps of: <ul id="ul0001" list-style="none" compact="compact"><li>determining a boost pressure target for said turbocharger;</li><li>calculating an error value, err_boost, between said boost pressure target and a measured actual boost pressure;</li><li>determining a first new variable geometry member position for said turbocharger based on said err_boost;</li><li>determining a second new variable geometry member position for said turbocharger based on a measured speed of the engine; and</li><li>positioning the variable geometry member according to the first new variable geometry member position when the engine is in a power mode, or to the second new variable geometry position when the engine is in a braking mode.</li></ul>

0010The step of determining said first new variable geometry member position may comprise the steps of: <ul id="ul0002" list-style="none" compact="compact"><li>determining a change in variable geometry member position, Δ^θ,wherein said Δ^θ is substantially equal to k_p (err_boost) + k_d (err_boost)/dt; and</li><li>summing said Δ^θ with a preceding variable geometry member position.</li></ul>

0011Prior to the step of calculating said err_boost, the method may further comprise the step of limiting said boost pressure target based on an ambient pressure to prevent over speeding the turbocharger.

0012Prior to said step of determining said second new variable geometry member position, the method may comprise a step of modifying the first new variable geometry member position with a feed forward value, wherein said feed forward valve is substantially equal to (|dTP/dt|Y*) K_a.

0013The present invention further provides a system for positioning a variable geometry member in a turbocharger that is coupled to an internal combustible engine, said system comprises: <ul id="ul0003" list-style="none" compact="compact"><li>a boost target map for determining a boost pressure target for said turbocharger;</li><li>an engine control unit configured to calculate an error value, err_boost, between the boost pressure target and an actual measured boost pressure, the engine control unit including a proportional integral differential module configured to determine a first new variable geometry member position for said turbocharger based on said err_boost;</li><li>an open loop control module to determine a second new variable geometry member position for the turbocharger based on a measured speed of the engine; and</li><li>an actuator configured to position said variable geometry member according to said first new variable geometry member position when the engine is in a power mode, or according to the second new variable geometry member position when the engine is in a braking mode.</li></ul>

0014The proportional integral differential module may generate the first new variable geometry member position by determining a change in the variable geometry member position, Δ^θ, wherein said Δ^θ is substantially equal to k_p(err_boost) + kd(err_boost)/dt, and summing said Δ^θ with a preceding variable geometry member position.

0015The boost pressure target may be limited based on an ambient pressure to prevent over speeding the turbocharger.

0016The system may further comprise a feed forward module configured to generate a feed forward value, FF, wherein said FF is substantially equal to (|dTP/dt|Y)* K_a, and wherein said FF is used to modify said first new variable geometry member position.

BRIEF DESCRIPTION OF THE DRAWINGS

0017<ul id="ul0004" list-style="none" compact="compact"><li><figref idref="f0001">FIG. 1</figref> illustrates a block diagram of a control system embodiment according to principles of this invention for use with a variable geometry turbocharger;</li><li><figref idref="f0002">FIG. 2</figref> is a flowchart of a control system method according to principles of this invention for use with a variable geometry turbocharger;</li><li><figref idref="f0003">FIG. 3</figref> illustrates a block diagram of a control system embodiment according to principles of this invention for use with a variable geometry turbocharger;</li><li><figref idref="f0004">FIG. 4</figref> illustrates a block diagram of a control system embodiment according to principles of this invention for use with a variable geometry turbocharger; and</li><li><figref idref="f0005">FIG. 5</figref> illustrates a block diagram of a control system embodiment according to principles of this invention for use with a variable geometry turbocharger.</li></ul>

DETAILED DESCRIPTION OF THE INVENTION

0018Control systems, constructed according to principles of this invention, for variable geometry turbochargers (VGTs) are specifically designed to govern the flow of exhaust gas to a turbine wheel in the turbocharger, thereby controlling pressurized air output by the turbochargers.

0019<figref idref="f0001">FIG. 1</figref> illustrates a turbocharged internal combustion engine system 100 comprising a control system according to one embodiment of this invention The engine system comprises an internal combustion engine 102, and engine control unit (ECU) 104, and actuator 106, and a VGT 108 in air and exhaust flow communication with the engine. The VGT includes one or more variable geometry members that are movably disposed therein, and that are coupled to the actuator for movement/position control.

0020The ECU 104 can include a boost target map 110, a boost target correcting module 112, a proportional/integral/differential (PID) module 11A, an open loop map 116, a fault detection module 118, a feed forward module 120, and a digital/analog (D/A) converter 122. The VGT 108 can include a variable geometry member in the form of a number of aerodynamic vanes that are movably attached to an inlet nozzle of the VGT turbine, and that are positioned upstream from a turbine wheel disposed within the housing. An example VGT of this type is disclosed in <patcit id="pcit0003" dnum="US6269642B"><text>U.S. Patent No. 6,269, 642</text></patcit>. The position of the vanes in the VGT 108 is controlled by the actuator 106, which can be configured to pivot the vanes in unison incrementally to control the throat area of the inlet nozzle, and thereby, control the amount of exhaust gas that flows into the VGT 108.

0021The actuator 106 can be one of suitable design known in the art, for example, a position-dependent actuator design. A suitable actuator design is disclosed in <patcit id="pcit0004" dnum="US6269642B"><text>U.S. Patent Number No. 6,269,642</text></patcit>. Alternatively, the actuator 106 can be an electrical actuator with position feedback configured to communicate with the ECU 104 as part of a controller area network (CAN), which is a communication standard frequently used for in-vehicle control.

0022According to the present embodiment, sensors can be used to measure the quantity of fuel flow to engine 102, as well as the engine speed of engine 102, in a manner known in the art. It is noted that fuel quantity and engine speed are also referred to as "engine parameters" in the present application. The fuel quantity and engine speed measured by the sensors are fed into the boost target map 110. The boost target map 110 can be a map stored in a memory component of the ECU 104, for example, containing desired boost pressure data for a given fuel quantity or engine speed. Based on the fuel quantity or engine speed, a boost target is determined from boost target map 110. In one embodiment, braking status of the vehicle can also be factored into the determination of the boost target.

0023The boost target is input into the boost target correcting module 112, which also receives input from sensors that measure the ambient pressure, P_o. One function of the boost target correcting module 112 is to prevent the VGT 108 from overspeeding in instances where the ambient pressure is relatively low, such that meeting the boost target would overspeed the turbocharger. For example, the boost target correcting module 112 can determine a maximum permissible boost as a function of the ambient pressure, the engine speed, and the turbocharger speed limit. If the boost target that is determined from the boost target map 110 exceeds the maximum permissible boost, then the boost target correcting module 112 can reduce the boost target to a permissible level. In this manner, the boost target correcting module 112 can be configured to adjust the boost target in instances where the boost target could result in overspeeding the turbocharger.

0024The corrected boost target generated by the boost target correcting module 112 is then compared to the actual boost at summing node 113 to determine the error between the boost target and the actual boost. The error value, which is also referred to as "err" in the present application, is fed into the PID module 114. The PID module 114 can be configured to determine a new variable geometry member, e.g., vane position, θ_new, to achieve the boost target utilizing a suitable PID filtering method known in the art.

0025In one embodiment, rather than determining θ_new directly, the PID module 114 can be configured to calculate the change in vane position, i.e., Δ^θ, needed in order to meet the boost target. For example, the PID module 114 can be configured to calculate Δ^θ according to Equation 1, below: <maths id="math0001" num="Equation 1:"><math display="block"><msup><mi mathvariant="normal">Δ</mi><mi mathvariant="normal">θ</mi></msup><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><mi>err</mi></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><mi>err</mi></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0001.tif" /></maths> wherein "err" is the error value defined as the difference between the actual boost and the boost target as determined at summing node 113, and wherein k_p is the proportional gain value and k_d is the differential gain value determined in a manner known in the art. A new vane position, i.e. θ_new, is then determined by summing Δ^θ and θ_old at the summing node 115. Once θ_new has been determined, other corrective/diagnostic mechanisms can be utilized to enhance the level of control. In one embodiment, an open loop diagnostic mechanism can be implemented wherein a target vane position, θ_target, is determined from open an loop map 116.

0026The open loop map 116 can be, for example, a map stored in a memory component in the ECU 104 that, based only on fuel quantity and engine speed, plots a desired vane position for different fuel quantities and engine speeds. θ_new and θ_target can then be inputted into a fault detection module 118, which can be configured to determine the difference in value between θ_new and θ_target to generate θ_diff. The Fault detection module 118 can be further configured to compare θ_diff against a threshold fault value. If the fault detection module 118 determines that θ_diff is equal to, or exceeds, the threshold fault value, for example, then the fault detection module 118 can send an error message to a control module (not shown) in the ECU 104 signaling the ECU 104 to enter a fault mode.

0027In one embodiment, a feed forward mechanism can also be implemented subsequent to the determination of θ_new. The feed forward module 120, which receives data on throttle position and/or fuel rate from engine 102, can be configured to determine the feed-forward value ("FF") as a function of the absolute value of the change in throttle position ("TP"), a threshold value ("Y") and a constant value ("K_a") according to Equation 2, below: <maths id="math0002" num="Equation 2:"><math display="block"><mi>FF</mi><mo mathvariant="normal">=</mo><mfenced><mfenced open="|" close="|"><mi>dTP</mi><mo mathvariant="normal">/</mo><mi>dt</mi></mfenced><mo mathvariant="normal">-</mo><mi mathvariant="normal">Y</mi></mfenced><mo mathvariant="normal">*</mo><msub><mi mathvariant="normal">K</mi><mi mathvariant="normal">a</mi></msub></math><img file="EP1529159B1_D0002.tif" /></maths>

0028Alternatively, the feed forward value can be determined from the absolute value of the change in fuel rate, rather than throttle position. The feed forward value generated by the feed forward module 120 may then be summed with θ_new to modify θ_new. In this manner, i.e., by taking into account throttle position and/or fuel rate to complement the error-based determination of θ_new by the PID module 114, the feed forward module 120 operates to provide numerous advantages, including a reduction in turbo lag.

0029θ_new is fed into a D/A converter 122, which can be configured to convert θ_new into an analog signal. In one embodiment, the D/A converter 122 is a voltage driver configured to convert θ_new into a pulse code modulation ("PWM") signal. Alternatively, the D/A converter 122 can be a current driver configured to convert θ_new into a dithered current. The signal from the D/A converter 122 is then used to control the position of the actuator 106.

0030In response to the signal from the D/A converter 122, the actuator 106 adjusts the vane position of the VGT 108 to match θ_new. In this manner, the vane position of the VGT 108 can be controlled and adjusted, thereby regulating the flow of exhaust gas into the VGT 108, and thereby controlling the level of boost pressure generated by the VGT 108.

0031<figref idref="f0002">FIG. 2</figref> illustrates an exemplary VGT control system method 200 according to one embodiment of this invention, wherein the variable geometry member of the VGT is adjusted. It is noted that control method 200 can be implemented in an engine system such as the engine system 100 in <figref idref="f0001">FIG. 1</figref>.

0032The control method 200 begins at step 202 and proceeds to step 204, where the engine speed and/or fuel quantity are measured. The engine speed and fuel quantity can be measured using a suitable measurement means known in the art, for example, by way of a sensor. The measured engine speed and fuel quantity are input into an ECUt, which can use either the engine speed or fuel quantity to determine a desired vane position for a VGT coupled to the engine.

0033Next, at step 206 of the control method 200, the measured engine speed and/or fuel quantity are used to determine a boost target for the VGT. The boost target can be determined, for example, from a boost target map stored in a memory component in the ECU containing desired boost levels for different engine speeds and fuel quantities. Subsequently, the boost target can be corrected, if necessary, at step 208 if it is determined that realizing the boost target would result in overspeeding the turbocharger. In such instance, the boost target may be reduced to avoid overspeeding the turbocharger.

0034After the boost target has been corrected, if necessary, at step 208, the VGT control method 200 continues to step 210, where the error value, or "err," between the boost target and the actual boost is determined. The error value from step 210 is then used in step 212 to determine a new vane position, θ_new, for the VGT. The new vane position can be determined by using a suitable PID filter known in the art. Alternatively, θ_new can be determined by first calculating the change in vane position, i.e. Δ^θ, needed to realize the boost target. In one embodiment, Δ^θ is determined according to equation 1, below: <maths id="math0003" num="Equation 3:"><math display="block"><msup><mi mathvariant="normal">Δ</mi><mi mathvariant="normal">θ</mi></msup><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><mi>err</mi></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><mi>err</mi></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0003.tif" /></maths> wherein k_p is a proportional gain value and k_d is the differential gain value determined in a manner known in the art. Once Δ^θ has been calculated, θ_new can then be determined by summing Δ^θ with the old vane position.

0035Following the determination of θ_new at step 212, in one embodiment, the control method 200 includes step 214, where an open loop diagnostic mechanism is applied. At step 214, a target vane position, θ_target, can be determined from an open loop map stored in a memory component in the ECU. The map can plot desired vane positions based only on fuel quantity and engine speed. The difference between θ_new and θ_target is then compared against a threshold fault value. If the difference between θ_new and θ_target is equal to, or exceeds, the threshold fault value, then an error message can be generated, for example, and the system can be triggered to enter a fault mode.

0036In one embodiment, following the determination of θ_new at step 212, a feed-forward mechanism is applied at step 216. At step 216, a feed forward value, FF, can be calculated according to Equation 2, below: <maths id="math0004" num="Equation 2:"><math display="block"><mi>FF</mi><mo mathvariant="normal">=</mo><mfenced><mfenced open="|" close="|"><mi>dTP</mi><mo mathvariant="normal">/</mo><mi>dt</mi></mfenced><mo mathvariant="normal">-</mo><mi mathvariant="normal">Y</mi></mfenced><mo mathvariant="normal">*</mo><msub><mi mathvariant="normal">K</mi><mi mathvariant="normal">a</mi></msub></math><img file="EP1529159B1_D0004.tif" /></maths> wherein TP is the throttle position, Y is a threshold value and K_a is a constant. In one embodiment, a fuel quantity measurement can be used in place of throttle position in Equation 2 to calculate FF.

0037Next, at step 218, the signal representing the new vane position is converted to an analog signal. The signal can be converted, for example, by either a voltage driver or a current driver. The converted signal is then used at step 220 to set the actuator position, which in turn sets the vane position of the VGT at step 222. The vane position is set so as to achieve the boost target determined in earlier steps. The control method 200 then returns to step 204 where the engine speed and fuel quantity are again measured, and the control loop can be repeated. In this manner, the geometry of the VGT, and more particularly the vane position of the VGT, can be controlled.

0038In certain embodiments, additional control mechanisms can be implemented that take into consideration other factors, such as vehicle braking, in determining a new vane position for the turbocharger. Reference is now made to <figref idref="f0003">FIG. 3</figref> illustrating exemplary engine system 300 according to one embodiment of the invention, in which embodiment an open loop engine braking control mechanism is implemented to enhance vane position control. It is noted that the engine 302, VGT 308, actuator 306, and D/A converter 322 of the engine system 300 are respectively equivalent to the engine 102, VGT 108, actuator 106, and D/A converter 122 of the engine system 100 illustrated in <figref idref="f0001">FIG. 1</figref>. As shown, the engine system 300 further includes an ECU 304.

0039According to the present embodiment, sensors can be used to measure the quantity of fuel flow to the engine 302, as well as the engine speed of the engine 302. The fuel rate and/or engine speed measured by the sensors are fed into the boost target map 310. The boost target map 310 can be a file stored in a memory component of the ECU 304, for example, mapping desired boost pressure for a given fuel rate or engine speed. Based on the fuel rate or engine speed, a boost target is determined from the boost target map 310.

0040The boost target is input into a boost target correcting module 312, which also receives input from sensors on the engine 302 measuring the ambient pressure, P_o. One function of the boost target correcting module 312 is to prevent the VGT 308 from overspeeding in instances where the ambient pressure is relatively low, such that meeting the boost target would overspeed the turbocharger. For example, a maximum permissible boost can be defined as a function of the ambient pressure, the engine speed, and the VGT turbine speed limit. If the boost target determined from the boost target map 310 exceeds the maximum permissible boost, then the boost target correcting module 312 can operate to reduce the boost target to a permissible level. In this manner, the boost target correcting module 312 adjusts the boost target in instances where the boost target derived from the boost target map 310 would result in overspeeding the VGT.

0041The corrected boost target generated by the boost target correcting module 312 is then compared to the actual boost at a summing node 313 to determine the error between the boost target and the actual boost. The error value, which is also referred to as "err" in the present application, is fed into a PID module 314. The PID module 314 can be configured to determine a new vane position, θ_new, for the VGT 308 needed to achieve the boost target utilizing a suitable proportional gain, integral gain, and differential gain filtering technique ("PID technique"). In one embodiment, rather than determining θ_new directly by means of a conventional PID technique, the PID module 314 can be configured to calculate the change in vane position, i.e., Δ^θ, needed in order to meet the boost target. For example, the PID module 314 can be configured to calculate Δ^θ according to Equation 3, below: <maths id="math0005" num="Equation 3:"><math display="block"><msup><mi mathvariant="normal">Δ</mi><mi mathvariant="normal">θ</mi></msup><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><msub><mi>err</mi><mi>boost</mi></msub></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><msub><mi>err</mi><mi>boost</mi></msub></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0005.tif" /></maths> wherein "err_boost" is the error value defined as the difference between the actual boost and the boost target as determined at summing node 313, and wherein k_p is the proportional gain value and k_d is the differential gain value. A new vane position, i.e. θ_new, may then be determined by summing Δ^θ with the vane position from the preceding iteration at summing node 315.

0042In one embodiment; a feed forward mechanism can also be implemented subsequent to the determination of θ_new. A feed forward module 320, which receives data on throttle position and/or fuel rate from engine 302, can be configured to determine a feed forward value ("FF") as a function of the absolute value of the change in throttle position ("TP"), a threshold value ("Y") and a constant value ("K_a") according to Equation 2, discussed above, and shown below: <maths id="math0006" num="Equation 2:"><math display="block"><mi>FF</mi><mo mathvariant="normal">=</mo><mfenced><mfenced open="|" close="|"><mi>dTP</mi><mo mathvariant="normal">/</mo><mi>dt</mi></mfenced><mo mathvariant="normal">-</mo><mi mathvariant="normal">Y</mi></mfenced><mo mathvariant="normal">*</mo><msub><mi mathvariant="normal">K</mi><mi mathvariant="normal">a</mi></msub></math><img file="EP1529159B1_D0006.tif" /></maths>

0043Alternatively, the feed forward value can be determined from the absolute value of the change in fuel rate, rather than throttle position. The feed forward value generated by the feed forward module 320 may then be summed with θ_new at summing node 315 to modify θ_new. In this manner, i.e., by taking into account throttle position and/or fuel rate to complement the error-based determination of θ_new by PID module 314, the feed forward module 320 provides numerous advantages, including a reduction in turbo lag.

0044In certain embodiments, a decision block, such as a limiting block 319, may be implemented to ensure that θ_new is within a desired or acceptable range. At limiting block 319, θ_new can be compared to a maximum and a minimum vane position. If θ_new exceeds either threshold position, then θ_new can be altered at limiting block 319 to bring θ_new within the maximum and minimum vane position settings. For example, if θ_new exceeds the maximum vane position, then θ_new would be reset to the maximum vane position threshold. Following, θ_new is fed into the decision block 321.

0045Continuing with <figref idref="f0003">FIG. 3</figref>, the ECU 304 further comprises an open-loop control module 316, which receives input from sensors measuring the engine 302 speed. The open-loop control module 316 can be configured to generate an open-loop vane position target as a function of the engine speed. A suitable map stored in a memory component and mapping vane position as a function of the engine speed may be used to derive the vane position target. The open-loop vane position target generated by open loop control module 316 is then fed into decision block 321.

0046At decision block 321, the ECU 304 determines whether engine 302 is in braking or non-braking, i.e., "power", mode. If the engine 302 is in power mode, then θ_new is the preferred vane position target for the current iteration and is not altered. However, in instances where engine 302 is in braking mode, the open-loop vane position target generated by open loop control module 316 is preferred. In such case, θ_new would assume the open loop vane position target generated by the open loop control module 316.

0047Following, θ_new is fed into a D/A converter 322, which can be configured to convert θ_new into an analog signal. In one embodiment, the D/A converter 322 is a voltage driver configured to convert θ_new into a pulse code modulation ("PWM") signal. Alternatively, the D/A converter 322 can be a current driver configured to convert θ_new into a dithered current. The signal from the D/A converter 322 is then used to control the position of the actuator 306. In response to the signal from the D/A converter 322, the actuator 306 adjusts the vane position of the VGT 308 to match θ_new.

0048Reference is now made to <figref idref="f0004">FIG. 4</figref>, which illustrates an exemplary engine system 400 according to one embodiment of the invention, according to which a cascaded PID technique is implemented to control the speed of the turbocharger as a means for managing vane position. It is noted that the engine 402, VGT 408, actuator 406, and D/A converter 422 of engine system 400 are respectively equivalent to the engine 102, VGT 108, actuator 106, and D/A converter 122 illustrated in <figref idref="f0001">FIG. 1</figref>.

0049As shown, the engine system 400 also comprises a ECU 404. A boost target map 410 of the ECU 404 receives input from the engine 402 indicating the engine speed and/or fuel rate of the engine 402. Based on the fuel rate or engine speed of the engine 402, a boost target is derived from the boost target map 410. The boost target is then compared to the actual boost of the VGT 408 at summing node 411 in order to determine a boost error.

0050The boost error is then input into a PID 412, which may utilize any suitable PID technique known in the art to determine a turbo speed target. In certain embodiments, the PID 412 may be configured to produce the turbo speed target using a modified PID approach. According to the modified PID approach, a change in the speed of the turbo, i.e., Δ_speed, needed to achieve the boost target is first calculated and then summed with the actual turbo speed in order to arrive at a turbo speed target. In such embodiments, delta turbo speed may be calculated according to Equation 4, as follows: <maths id="math0007" num="Equation 4:"><math display="block"><msub><mi mathvariant="normal">Δ</mi><mi>speed</mi></msub><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><msub><mi>err</mi><mi>boost</mi></msub></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><msub><mi>err</mi><mi>boost</mi></msub></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0007.tif" /></maths> wherein "err_boost" is an error value defined as the difference between the actual boost and the boost target as determined at the summing node 411, and wherein k_p is the proportional gain value and k_d is the differential gain value. Once Δ_speed has been determined, then the turbo speed limit may be calculated by summing Δ_speed with the actual turbo speed.

0051A limiting block 413 may next be implemented to limit the turbo speed target to within a desired range. Lower and upper turbo speed limits may be set for the system in order to enhance performance while minimizing stress to the system. Thus, if the turbo speed target determined by the PID 412 falls outside the desired range, the turbo speed target can be reset to with the desired range at the limiting block 413.

0052After the turbo speed target has been determined, it is compared to the actual turbo speed at the summing node 415. The difference between the turbo speed target and the actual turbo speed, which is defined as the turbo speed error, or "err_speed," is then fed into a PID 414. The PID 414 may be configured to determine a new vane position (i.e., θ_new) based on err_speed and a known PID technique. Alternatively, the PID 414 may determine θ_new by first utilizing a modified PID to calculate a desired change in vane position, i.e. Δ^θ, according to Equation 5, below: <maths id="math0008" num="Equation 5:"><math display="block"><msup><mi mathvariant="normal">Δ</mi><mi mathvariant="normal">θ</mi></msup><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><msub><mi>err</mi><mi>speed</mi></msub></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><msub><mi>err</mi><mi>speed</mi></msub></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0008.tif" /></maths> wherein "err_speed" is the difference between the actual turbo speed and the turbo speed target as determined at a summing node 415, and wherein k_p is the proportional gain value and k_d is the differential gain value. Following, Δ^θ is summed with the vane position from the preceding iteration to arrive at θ_new, which is then inputted into summing node 417..

0053As shown in <figref idref="f0004">FIG. 4</figref>, certain embodiments of the engine system 400 may also include a feed forward module 420, which is equivalent to the feed forward module 120 of engine system 100 in <figref idref="f0001">FIG. 1</figref>. Accordingly, the feed forward module 420 receives input from sensors on the engine 402 indicating the throttle position and/or fuel rate of the engine 402. Based on the input throttle position or fuel rate, a threshold value ("Y") and a constant value ("K_a"), the feed forward module 420 generates a feed forward value that is fed into the summing node 417 in order to modify θ_new as needed. The feed forward value can be calculated according to Equation 2, described above.

0054Next, a limiting block 419 maybe implemented as a safeguard to keep θ_new within a desired range. An upper and lower vane position can be defmed, and in instances where θ_new is outside these parameters, then θ_new can be reset to be within the upper and lower thresholds. Following, θ_new is fed into a D/A converter 422, which converts θ_new into an analog signal for the controlling actuator 406. In response to the signal from the D/A converter 422, the actuator 406 adjusts the vane position of the VGT 408 to match θ_new. In this manner, the vane position of the VGT 408 can be controlled and adjusted.

0055Reference is now made to <figref idref="f0005">FIG. 5</figref>, which illustrates an engine system 500 in accordance with one embodiment, according to which a closed loop engine braking control based on turbine pressure, combined with a cascaded PID technique, is utilized to manage vane position. It is noted that the engine 502, VGT 508, actuator 506, and D/A converter 522 of the engine system 500 are respectively equivalent to the engine 102, VGT 108, actuator 106, and D/A converter 122 of the system 100 illustrated in <figref idref="f0001">FIG. 1</figref>.

0056In the present embodiment, an ECU 504 first determines a turbo speed target for the VGT 508 according to two methods. According to the first method, a boost target map 510 determines a boost target based on the engine speed and fuel rate of the engine 502. The boost target is then compared to the actual boost of the VGT 508 at a summing node 511 to derive the boost error. Next, the boost error is input into a PID 512, which can utilize a conventional PID technique to generate a turbo speed target based on the boost error. Alternatively, the PID 512 may be configured to generate the turbo speed target using a modified PID technique, whereby a desired change in turbo speed, i.e., Δ_speed, is calculated and summed with the actual turbo speed to produce the turbo speed target. Equation 4, which is described above, may be used to calculate Δ_speed, as shown below: <maths id="math0009" num="Equation 4:"><math display="block"><msub><mi mathvariant="normal">Δ</mi><mi>speed</mi></msub><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><msub><mi>err</mi><mi>boost</mi></msub></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><msub><mi>err</mi><mi>boost</mi></msub></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0009.tif" /></maths> wherein "err_boost" is the error value defined as the difference between the actual boost and the boost target, and wherein k_p is the proportional gain value and k_d is the differential gain value. Once Δ_speed has been determined, the turbo speed target may be calculated by summing Δ_speed with the actual turbo speed.

0057In the second method for determining a turbo speed target, the engine speed of the engine 502 is fed into a turbine pressure map 514. The turbine pressure map 514 can be a file stored in a memory component of the ECU 504, for example, mapping desired turbine pressures for a given engine speeds. Based on the input engine speed, a turbine pressure target is determined from the turbine pressure map 514. The turbine pressure target is then compared to the actual turbine pressure, as measured by sensors on the engine 502. The turbine pressure error, which is referred to as the difference between the turbine pressure target and the actual turbine pressure, is determined by comparing the turbine pressure target and the actual turbine pressure at summing node 515. The turbine pressure error is then input into a PID 516, which can generate a turbo speed target utilizing a conventional PID technique. Alternatively, a modified PID technique may instead be used to arrive at the turbo speed target by first determining a desired change in turbo speed, or Δ_speed, and then adding the Δ_speed to the actual turbo speed. Δ_speed may be calculated according to Equation 6, below: <maths id="math0010" num="Equation 6:"><math display="block"><msub><mi mathvariant="normal">Δ</mi><mi>turbine</mi></msub><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><msub><mi>err</mi><mi>turbine</mi></msub></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><msub><mi>err</mi><mi>turbine</mi></msub></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0010.tif" /></maths> wherein "err_turbine" is the error value defined as the difference between the actual turbine pressure and the turbine pressure target, and wherein k_p is the proportional gain value and k_d is the differential gain value. Summing Δ_speed with the actual turbo speed produces the turbo target speed according to the second method.

0058Continuing with <figref idref="f0005">FIG. 5</figref>, at decision block 517, the ECU 504 determines whether the engine 502 is in power or braking mode. If the engine 502 is in a power mode, then the turbo speed target generated by the first method (i.e., by PID 512) is selected to establish new vane position for the current iteration. On the other had, if the engine 502 is in braking mode, then the turbo speed target generated according to the second method (i.e., by PID 516) is selected. It is noted that the turbo speed target selected at decision block 517 is also referred to as a "selected turbo speed target," in the present application.

0059Next, the turbo speed target selected at the decision block 517 may be limited to within a desired range of turbo speeds at a limiting block 519, where, if the turbo speed target falls outside the desired range, the turbo speed target can be reset to be within the desired range. The turbo speed target is then compared to the actual turbo speed at a summing node 521 to determine a turbo speed error, or "err_speed" which is fed into a PID 518. The PID 518 may be configured to determine a new vane position (i.e., θ_new) based on err_speed and a known PID technique. Alternatively, the PID 518 may determine θ_new by first utilizing a modified PID to calculate a desired change in vane position, i.e. Δ^θ, according to Equation 5, discussed above and shown below: <maths id="math0011" num="Equation 5:"><math display="block"><msup><mi mathvariant="normal">Δ</mi><mi mathvariant="normal">θ</mi></msup><mo mathvariant="normal">=</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">p</mi></msub><mfenced><msub><mi>err</mi><mi>speed</mi></msub></mfenced><mo mathvariant="normal">+</mo><msub><mi mathvariant="normal">k</mi><mi mathvariant="normal">d</mi></msub><mfenced><msub><mi>err</mi><mi>speed</mi></msub></mfenced><mo mathvariant="normal">/</mo><mi>dt</mi></math><img file="EP1529159B1_D0011.tif" /></maths> wherein "err_speed" is the error value defined as the difference between the actual turbo speed and the turbo speed target as determined at the summing node 521, and wherein k_p is the proportional gain value and k_d is the differential gain value. Following, Δ^θ is summed with the vane position from the preceding iteration to arrive at θ_new, which is then inputted into a summing node 523.

0060In certain aspects of the present embodiment, a feed forward module 520 may be implemented to improve control of the vane position. The feed forward module 520 receives input from sensors on the engine 502 indicating the throttle position and/or fuel rate of the engine 502. The forward module 520 can be configured to generate a feed forward value based on the inputted throttle position or fuel rate, a threshold value ("Y") and a constant value ("K_a"). The feed forward value may then be input into the summing node 523 in order to modify θ_new as may be needed. The feed forward value can be calculated according to Equation 2, described above.

0061Following, a limiting block 525 may be included in the ECU 504 to ensure that θ_new is within a desired range of vane positions. If θ_new does not fall within the desired range, then θ_new may be reset at the limiting block 525 so as to be within the desired range. θ_new is then fed into a D/A converter 522, which converts θ_new into an analog signal for controlling the actuator 506. Based on the signal received from the D/A converter 522, the actuator 506 adjusts the vane position of the VGT 508 to match θ_new. In this manner, the vane position of the VGT 508 can be controlled and adjusted.