JP4299164B2 - Control device for variable valve timing mechanism - Google Patents

Description

  The present invention relates to a control device for a variable valve timing mechanism that changes a valve timing (opening / closing timing) of an intake valve or an exhaust valve of an engine by changing a rotational phase of a camshaft with respect to a crankshaft of an internal combustion engine.

As a control device for a variable valve timing mechanism that changes the valve timing of an intake valve or an exhaust valve by changing the rotational phase of a camshaft with respect to a crankshaft of an internal combustion engine, there is one disclosed in Patent Document 1. .
This includes a crank angle sensor that outputs a crank angle signal at the reference rotational position of the crankshaft, and a cam sensor that outputs a cam signal at the reference rotational position of the camshaft. The rotational phase of the camshaft relative to the shaft is detected, and the variable valve timing mechanism is feedback controlled so that this rotational phase becomes a target.
JP 2000-297686 A

  By the way, in the above-described conventional configuration, the rotation phase is detected at every constant crank angle (camshaft rotation cycle). However, feedback control of the variable valve timing mechanism is usually executed every minute unit time. Therefore, at the time of low rotation such as when the engine is started, the rotation phase detection cycle is longer than the feedback control execution cycle, and the rotation phase cannot be detected with sufficient frequency for control.

  Therefore, for example, even if an attempt is made to control the valve timing to a state suitable for engine start (starting timing) during cranking, the feedback manipulated variable is calculated until the rotation phase is detected even after engine start is started. In addition, after the rotational phase is detected, the feedback manipulated variable is calculated based on the deviation from the actual rotational phase until the rotational phase is updated. There is a risk of reducing the performance.

  The present invention has been made paying attention to such a problem, and an object of the present invention is to quickly converge the rotational phase to a target even at a low rotation speed, and to improve the startability particularly during cold operation.

For this reason, the invention according to claim 1 is a rotation speed detection means for detecting the engine rotation speed;
Rotational phase detection means is provided that can detect an actual value of the rotational phase of the camshaft relative to the crankshaft at a cycle shorter than the rotational cycle of the camshaft, and the rotational phase of the camshaft relative to the crankshaft is set according to the engine operating state. When the engine rotational speed is equal to or lower than a predetermined rotational speed and the deviation between the actual value of the rotational phase detected by the rotational speed detecting means and the target rotational phase is equal to or greater than a predetermined value, While feed-forward control is performed, feedback control is performed when the engine rotational speed exceeds the predetermined rotational speed or when the deviation is less than the predetermined value .
In this way, the actual rotation phase (valve timing) can be quickly controlled to the target rotation phase (target valve timing) even in the low rotation region where the rotation phase detection cycle becomes long. Thereby, the controllability at the time of starting the engine is improved, and in particular, the startability at the time of cold engine can be improved.

According to a second aspect of the invention, when the amount of change per predetermined time in the engine speed exceeds a predetermined amount, it performs the feedback control prohibit the feedforward control.
According to a third aspect of the present invention, the rotational phase detecting means outputs a signal different depending on a rotational position of the camshaft and a first sensor that outputs a signal for each reference rotational position and unit crank angle of the crankshaft. A second sensor for outputting, and detecting an actual value of the rotational phase based on output signals of the first sensor and the second sensor .

In this way, if the change amount of the engine rotation speed exceeds a predetermined value even in the low rotation region, it is determined that the explosion has been completed (cranking has been completed), and the feedforward control is shifted to the feedback control. . As a result, the valve timing can be controlled with good response to the start timing by feedforward control when the engine is started, and can be accurately controlled to the optimal valve timing by feedback control after the complete explosion.
Further, the actual value of the rotational phase can be detected at an arbitrary timing based on the output signals of the first sensor and the second sensor.

  Hereinafter, embodiments of the present invention will be described with reference to the drawings. FIG. 1 is a configuration diagram of an internal combustion engine for a vehicle in the embodiment. In FIG. 1, an electronic control throttle 104 that opens and closes a throttle valve 103 b by a throttle motor 103 a is interposed in an intake pipe 102 of the internal combustion engine 101, and the combustion chamber is connected via the electronic control throttle 104 and the intake valve 105. Air is inhaled into 106.

Each combustion chamber of the engine is provided with a spark plug 133, which ignites sparks to ignite and burn the air-fuel mixture. The combustion exhaust is discharged from the combustion chamber 106 through the exhaust valve 107, purified by the front catalyst 108 and the rear catalyst 109, and then released into the atmosphere.
The intake valve 105 and the exhaust valve 107 are driven to open and close by cams provided on the intake side camshaft 134 and the exhaust side camshaft 110, respectively. The intake side camshaft 134 includes a variable valve timing mechanism (VTC) 113. Is provided.

The VTC 113 is a mechanism that changes the opening / closing timing of the intake valve 105 by changing the rotational phase of the intake camshaft 134 with respect to the crankshaft 120, and details thereof will be described later.
In the present embodiment, the VTC 113 is provided only on the intake valve 105 side, but the VTC 113 may be provided on the exhaust valve 107 side instead of the intake valve 105 side or together with the intake valve 105 side.

In addition, an electromagnetic fuel injection valve 131 is provided in the intake port 130 of each cylinder. When the fuel injection valve 131 is driven to open by an injection pulse signal from an engine control unit (ECU) 114, a predetermined value is set. The fuel adjusted to the pressure is injected toward the intake valve 105.
The ECU 114 incorporating the microcomputer receives output signals from various sensors, and controls the electronic control throttle 104, the VTC 113, and the fuel injection valve 131 by arithmetic processing based on the signals.

  Examples of the various sensors include an accelerator opening sensor APS116 for detecting the accelerator opening, an air flow meter 115 for detecting the intake air amount Qa of the engine 101, and a reference crank angle signal at a reference rotational position at every crank angle of 180 ° from the crankshaft 120. A crank angle sensor 117 for taking out the REF and taking out a unit angle signal POS for each unit crank angle, a throttle sensor 118 for detecting the opening TVO of the throttle valve 103b, a water temperature sensor 119 for detecting the cooling water temperature Tw of the engine 101, the intake side A cam sensor 132 that extracts a cam signal CAM at a reference rotational position for each cam angle 90 ° (crank angle 180 °) from the cam shaft 134, a pressure sensor 135 that detects the combustion pressure in the combustion chamber 106, and a voltage sensor that detects the battery voltage Vb 136 etc. are provided . The engine speed Ne is calculated based on the cycle of the reference crank angle signal REF or the number of unit angle signals POS generated per unit time. Although not shown, the ECU 114 also receives operation signals such as an idle switch and a start switch.

  Next, the configuration of the VTC 113 will be described with reference to FIGS. As shown in FIG. 2, the VTC 113 according to the present embodiment is assembled to the intake side camshaft (hereinafter simply referred to as a camshaft) 134 and a front end portion of the camshaft 134 so as to be relatively rotatable as necessary. And a drive ring 303 (drive rotator) having a timing sprocket 302 linked to the crankshaft 120 via a chain (not shown) on the outer periphery, and a front side of the drive ring 303 and the camshaft 134 (in FIG. 2) An assembly angle operation mechanism 304 for operating an assembly angle between the camshaft 134 and the drive ring 303 and a further front side of the assembly angle operation mechanism 304. The operating force applying means 305 for driving, and the cylinder head and the head cover (not shown) of the internal combustion engine are attached to the front face of the head cover and assembled. And VTC cover outside view covering the front and periphery region of the operating mechanism 304 and the operation force imparting unit 305, and a. 3 (and FIG. 5) corresponds to the AA sectional view of FIG. 2, and FIG. 4 corresponds to the BB sectional view of FIG.

  The drive ring 303 is formed in a short shaft cylindrical shape having a step-like insertion hole 306, and the insertion hole 306 portion rotates to a driven shaft member 307 (driven rotating body) coupled to the front end portion of the camshaft 134. It is assembled as possible. As shown in FIG. 3, three radial grooves 308 (radial guides) having parallel side walls facing each other are provided on the front surface of the drive ring 303 (the surface opposite to the camshaft 134). It is formed so as to be along the substantially radial direction.

  In addition, as shown in FIG. 2, the driven shaft member 307 has an enlarged diameter portion formed on the outer periphery of the base that is abutted against the front end portion of the camshaft 134, and an outer peripheral surface on the front side of the enlarged diameter portion. The three levers 309 projecting radially are integrally formed, and are coupled to the camshaft 134 by bolts 310 penetrating the shaft core portion. The base end of each link 311 is pivotally connected to each lever 309 by a pin 312, and a columnar protrusion 313 slidably engaged with each radial groove 308 is integrally formed at the tip of each link 311. Is formed.

  Since each link 311 is connected to the driven shaft member 307 via the pin 312 in a state where the protruding portion 313 is engaged with the corresponding radial groove 308, the distal end side of the link 311 receives an external force and receives the radial groove. When displaced along 308, the drive ring 303 and the driven shaft member 307 are relatively rotated by a direction and an angle corresponding to the displacement of the protruding portion 313 by the action of the link 311.

  In addition, a housing hole 314 that opens to the front side in the axial direction is formed at the tip of each link 311, and the housing hole 314 has a spherical protrusion 316 a that engages with a spiral groove 315 (spiral guide) described later. An engagement pin 316 (rolling member) and a coil spring 317 that biases the engagement pin 316 forward (spiral groove 315 side) are accommodated. In this embodiment, a movable guide portion that is displaceable in the radial direction is configured by the protruding portion 313 at the tip of the link 311, the engagement pin 316, the coil spring 317, and the like.

  On the other hand, an intermediate rotating body 318 having a disk-like flange wall 318 a is rotatably supported via a bearing 331 in front of the protruding position of the lever 309 of the driven shaft member 307. The aforementioned spiral groove 315 having a semicircular cross section is formed on the rear surface side of the flange wall 318a of the intermediate rotating body 318, and the engagement pin 316 at the tip of each link 311 can freely roll in the spiral groove 315. Is engaged with the guide. The spiral of the spiral groove 315 is formed so as to gradually reduce the diameter along the rotation direction of the drive ring 303. Accordingly, in the state where the engagement pin 316 at the tip of each link 311 is engaged with the spiral groove 315, when the intermediate rotating body 318 rotates relative to the drive ring 303 in the delay direction, the tip of the link 311 becomes the radial groove 308. When the intermediate rotating body 318 is relatively displaced in the advancing direction, it is guided radially by the spiral shape of the spiral groove 315 and conversely moves in the radial direction.

  The assembly angle operation mechanism 304 of this embodiment is constituted by the radial groove 308, the link 311, the protrusion 313, the engagement pin 316, the lever 309, the intermediate rotating body 318, the spiral groove 315, etc. of the drive ring 303 described above. Has been. When the relative turning operation force with respect to the camshaft 134 is input from the operation force applying means 305 to the intermediate rotating body 318, the assembly angle operation mechanism 304 receives the operation force from the spiral groove 315 and the engagement pin 316. The distal end of the link 311 is displaced in the radial direction through the engaging portion, and at this time, relative rotational force is transmitted to the drive link 303 and the driven shaft member 307 by the action of the link 311 and the lever 309.

  On the other hand, the operating force applying means 305 includes a spring 319 that urges the intermediate rotator 318 in the rotation direction of the drive ring 303 and a braking mechanism that urges the intermediate rotator 318 in the direction opposite to the rotation direction of the drive ring 303. The intermediate rotating body 318 relative to the drive ring 303 by appropriately controlling the braking force of the hysteresis brake 320 according to the operating state of the internal combustion engine, or Is configured to maintain the rotational position of both.

The spring spring 319 has an outer peripheral end coupled to a cylindrical member 321 integrally attached to the drive ring 303, while an inner peripheral end is coupled to a cylindrical base of the intermediate rotating body 318, and the whole is intermediate. The rotating body 318 is disposed in the space on the front side of the flange wall 318a.
On the other hand, the hysteresis brake 320 is in a state in which the rotation is restricted by a bottomed cylindrical hysteresis ring 323 attached to the front end portion of the intermediate rotating body 318 via a retainer plate 322 and a VTC cover (not shown) which is a non-rotating member. And a coil yoke 325 which is a magnetic induction member for guiding the magnetism of the electromagnetic coil 324. The electromagnetic coil 324 is energized by the ECU 114 according to the operating state of the engine. To be controlled. Specifically, the ECU 114 controls the energization amount for the electromagnetic coil 324 based on a duty control signal on which a dither signal is superimposed.

As shown in FIG. 6, the hysteresis ring 323 is formed of a hysteresis material (semi-hard material) having a characteristic (magnetic hysteresis characteristic) in which the magnetic flux force changes with a phase lag with respect to a change in an external magnetic field, and the outer peripheral side. The cylindrical wall 323a is subjected to a braking action by the coil yoke 325.
The entire coil yoke 325 is formed in a substantially cylindrical shape so as to surround the electromagnetic coil 325, and the inner peripheral surface thereof is rotatably supported by the distal end portion of the driven shaft member 307 via the bearing 328. A pair of circumferential facing surfaces 326 and 327 are formed on the rear surface side (intermediate rotating body 318 side) of the coil yoke 315 so that the magnetic input / output portions face each other with a cylindrical gap.

In addition, as shown in FIG. 7, a plurality of concavities and convexities are continuously formed along the circumferential direction on both facing surfaces 326 and 327 of the coil yoke 325, and the convex portions 326 a and 327 a are magnetic poles among these concavities and convexities. (Magnetic field generator).
And the convex part 326a of one opposing surface 326 and the convex part 327a of the other opposing surface 327 are alternately arrange | positioned in the circumferential direction, and the convex parts 326a and 327a which the opposing surfaces 326 and 327 mutually adjoin are all the circumferential direction. It is shifted to. Therefore, a magnetic field having an inclination in the circumferential direction as shown in FIG. 7 is generated by the excitation of the electromagnetic coil 24 between the adjacent convex portions 326a and 327a of the opposing surfaces 326 and 327. A cylindrical wall 323a of the hysteresis ring 323 is interposed in a non-contact state in the gap between the opposing surfaces 326 and 327.

Here, the operating principle of the hysteresis brake 320 will be described with reference to FIG. 8A shows a state where a magnetic field is first applied to the hysteresis ring 323 (hysteresis material), and FIG. 8B shows a state where the hysteresis ring 323 is displaced (rotated) from the state of FIG. 8A. Indicates.
In the state of FIG. 8A, the direction of the magnetic field between the opposing surfaces 326 and 327 of the coil yoke 325 (the direction of the magnetic field from the convex portion 327a of the opposing surface 27 toward the convex portion 327a of the other opposing surface 326). A magnetic flux flows in the hysteresis ring 323 along the line.

  When the hysteresis ring 323 receives the external force F and moves to the state shown in FIG. 8B from this state, the hysteresis ring 323 is displaced in the external magnetic field. At this time, the magnetic flux inside the hysteresis ring 323 is The direction of the magnetic flux inside the hysteresis ring 323 has a phase delay, and the direction of the magnetic field between the opposing surfaces 326 and 327 is shifted (tilted). Accordingly, the flow of magnetic flux (magnetic lines) entering the hysteresis ring 323 from the convex portion 327a of the opposing surface 327 and the flow of magnetic flux (magnetic lines) from the hysteresis ring 323 toward the convex portion 326a of the other opposing surface 326 are distorted. An attractive force that corrects the distortion of the magnetic flux acts between the opposing surfaces 326 and 327 and the hysteresis ring 323, and the attractive force acts as a drag force F ′ that brakes the hysteresis ring 323.

  When the hysteresis ring 323 is displaced in the magnetic field between the opposing surfaces 326 and 327 as described above, the hysteresis brake 320 generates a braking force due to the deviation of the direction of the magnetic flux inside the hysteresis ring 323 and the direction of the magnetic field. However, the braking force depends on the strength of the magnetic field, that is, the magnitude of the excitation current of the electromagnetic coil 324, regardless of the rotational speed of the hysteresis ring 323 (relative speed between the opposed surfaces 326 and 327 and the hysteresis ring 323). It becomes a constant value approximately proportional to.

  FIG. 9 shows test results obtained by examining the relationship between the rotational speed and the braking torque in the hysteresis brake 320 by changing the excitation current to a to d (a <b <c <d). As is apparent from the test results, the hysteresis brake 320 is not affected by the rotational speed unlike a brake using an eddy current, for example, and can always obtain a braking force according to the excitation current value. .

  The VTC 113 according to the present embodiment is configured as described above. When the excitation of the electromagnetic coil 324 of the hysteresis brake 320 is turned off, the intermediate rotating body 318 is engineed against the drive ring 303 by the force of the mainspring spring 319. It is rotated to the maximum in the direction of rotation (see FIG. 3). Thereby, the rotational phase of the camshaft 134 with respect to the crankshaft 120 is maintained on the most retarded angle side where the valve timing is most delayed (the valve timing of the intake valve 105 is the most retarded timing).

  When the ECU 114 issues a command to change the rotational phase to the most advanced angle side from this state, the excitation of the electromagnetic coil 324 of the hysteresis brake 320 is turned on, and the braking force that resists the force of the mainspring spring 319. Is applied to the intermediate rotating body 318. As a result, the intermediate rotating body 318 rotates and moves with respect to the drive ring 303, whereby the engaging pin 316 at the tip of the link 311 is guided to the spiral groove 315, and the tip of the link 311 moves along the radial groove 308. As shown in FIG. 5, the assembly angle of the drive ring 303 and the driven shaft member 307 is changed to the most advanced angle side by the action of the link 311. As a result, the rotational phase is changed to the most advanced angle side where the valve timing is most advanced (the valve timing of the intake valve 105 is the most advanced angle timing).

  On the other hand, when the ECU 114 emits the rotational phase from this state (the most advanced angle side) to the most retarded angle side, the excitation of the electromagnetic coil 324 of the hysteresis brake 320 is turned off, and the spring spring 319 is again activated. The intermediate rotating body 318 is rotationally moved in the returning direction by the force. Then, the link 311 swings in the direction opposite to the above by the guide of the engaging pin 316 by the spiral groove 315, and the assembly angle of the drive ring 303 and the driven shaft member 307 is caused by the action of the link 311 as shown in FIG. Is again changed to the most retarded angle side.

  Note that the rotational phase (of the camshaft 134 with respect to the crankshaft) changed by the VTC 113 is not limited to the two phases of the most retarded angle and the most advanced angle described above, but can be arbitrarily set by controlling the braking force of the hysteresis brake 320. The phase can also be maintained by the balance between the force of the mainspring spring 319 and the braking force of the hysteresis brake 320.

In the present embodiment, as shown in FIG. 10, a rotating body 401 that rotates together with the intake camshaft 134 and an electromagnetic gap sensor 402 that is disposed in the vicinity of the outer periphery of the rotating body 401 are provided.
The rotating body 401 is fixed to the intake camshaft 134 directly or indirectly through another member, and the outer periphery thereof has a circumferential distance from the center of the intake camshaft 134 as shown in FIG. It is formed to change gradually. The gap sensor 402 outputs to the ECU 114 a signal (voltage) corresponding to the gap Gp between the intake camshaft 134 and the outer periphery of the rotating body 401 that changes with rotation. In addition, as long as the rotating body 401 is provided so as to rotate together with the intake side camshaft 134, the fixing method and the fixing position are not limited, and the gap sensor 402 is configured to have a gap Gp with the outer periphery of the rotating body 401. Any system may be used as long as a signal corresponding to the signal can be output continuously.

  Here, as shown in FIG. 11, the output from the gap sensor 402 is in a substantially direct relationship with the gap with the outer periphery of the rotating body 401, and the rotation angle of the intake camshaft 134 is the gap. Since there is a one-to-one correspondence, the output of the gap sensor 402 and the rotation angle (cam angle) of the intake camshaft 134 are substantially directly proportional as shown in FIG. Therefore, the ECU 114 can instantaneously detect the rotation angle of the intake side camshaft 134 based on the output signal from the gap sensor 402.

  That is, in this embodiment, (1) based on the detection signals of the crank angle sensor 117 and the cam sensor 132, the rotational phase of the intake camshaft 134 relative to the crankshaft 120 (intake air) for each rotation cycle of the intake camshaft 134. (The valve timing of the valve 105) can be detected (hereinafter referred to as detection by the first rotational phase detection means), and (2) based on the detection signals of the crank angle sensor 117 and the gap sensor 402, continuously at an arbitrary timing. It is possible to detect the rotational phase (valve timing of the intake valve 105) (hereinafter referred to as detection by the second rotational phase detection means).

  Specifically, the first rotation phase detection means detects (calculates) the rotation phase by counting the unit angle signal POS from the generation of the reference crank angle signal REF to the generation of the cam signal CAM, and performs the second rotation. The phase detection means detects the rotation angle of the intake camshaft 134 detected based on the output signal of the gap sensor 402, and the unit angle signal POS from the generation of the reference crank angle signal REF to the detection of the rotation angle of the intake camshaft 134. The rotational phase is detected (calculated) from the rotational angle of the crankshaft 120 detected by counting.

  Thus, by providing the two rotational phase detecting means, for example, the rotational phase of the intake camshaft 134 with respect to the crankshaft 120 is detected stably and accurately by the first rotational phase detecting means at the time of high rotation, while the valve At the time of low rotation in which the rotation phase detection period by the first rotation phase detection means is longer than the execution period of timing control or the like, the rotation phase is detected by the second rotation phase detection means. The rotational phase can be detected by appropriately selecting the second rotational phase detection means.

  By the way, in the VTC 113 according to the present embodiment, as will be described later, when the engine is started, the valve timing of the intake valve 105 (starting timing) that is optimal for starting is set to an advance side with respect to the most retarded timing. (See FIG. 14). This is because the valve timing is set so as not to impair the startability when the engine is started, and the output can be improved by retarding the valve timing when the engine speed is high. In this embodiment, when the engine is stopped, the valve timing of the intake valve 105 is the most retarded timing. Therefore, when the engine is started, it is necessary to advance the valve timing from the most retarded timing to the starting timing. .

Therefore, the ECU 114 switches the valve timing control between when the engine is started (during cranking) and during normal operation. Hereinafter, the valve timing control in the present embodiment will be described based on the flowcharts shown in FIGS. 13 and 14.
FIG. 13 is a flowchart showing a main routine of valve timing control. This flow is started when the key switch is turned on, and is executed every predetermined time (for example, 10 ms).

In S11, the target valve timing (target rotation phase) θtg (deg) of the intake valve 105 is set. In the present embodiment, such setting is performed based on the engine rotational speed Ne, the engine load, the engine temperature, and the like, details of which will be described later (see FIG. 14).
In S12, the actual valve timing (actual rotation phase) θdet (deg) of the intake valve 105 is detected. Such detection is performed based on detection signals of the crank angle sensor 117 and the gap sensor 402, that is, by the second rotational phase detection means.

In S13, a deviation Er (θtg−θdet) between the target rotation phase θtg and the actual rotation phase θdet is calculated.
In S14, it is determined whether or not the start switch is ON. If the start switch is ON, the process proceeds to S15, and if it is OFF, the process proceeds to S21. Instead of the start switch ON / OFF determination, the start motor ON / OFF determination may be used.

In S15, it is determined whether or not the engine rotational speed Ne is equal to or lower than a predetermined rotational speed Ns1 (for example, 300 rpm). If Ne ≦ Ns1, the process proceeds to S16, and if Ne> Ns1, the process proceeds to S21.
In S16, it is determined whether or not the change amount ΔNe of the engine rotation speed Ne from the previous value Nez is equal to or less than a predetermined value Ns2 (for example, 100 rpm). If ΔNe ≦ Ns2, the process proceeds to S17, and if ΔNe> Ns2, the process proceeds to S21.

  It is determined whether or not cranking is in progress (whether complete explosion has occurred) through the above S14 to S16, and if all are YES, it is determined that cranking is in progress and the process proceeds to S17. On the other hand, if any of them is NO, it is determined that cranking has been completed (complete explosion), and the process proceeds to S21, and normal valve timing control is performed. In this embodiment, it is determined whether or not cranking is being performed by determining all of S14 to S16. For example, it is determined whether or not the engine is in the low rotation range only by S15. It may be. Here, the normal valve timing control in the present embodiment refers to feedback control based on the deviation Er calculated in S13. Specifically, the feedback operation amount U is calculated by PID control or the like. The duty control signal corresponding to the feedback operation amount U is output to the VTC 113 (the electromagnetic coil 324 thereof).

  In S17, it is determined whether or not the battery voltage Vb is equal to or higher than a predetermined voltage Vs (eg, 8V). This condition is determined because if the battery voltage Vb is low, the VTC 113 cannot actually be driven even if a drive signal (duty control signal to the electromagnetic coil 324) is output to the VTC 113. Therefore, if Vb ≧ Vs, the process proceeds to S18, but if Vb <Vs, the process proceeds to S21 to perform normal valve timing control.

  In S18, it is determined whether or not the coolant temperature (engine temperature) Tw is equal to or lower than a predetermined temperature Ts (for example, 100 ° C.). The reason for determining such a condition is that if the amount of current supplied to the electromagnetic coil 324 is increased at a high temperature, the coil temperature may increase excessively. Therefore, if Tw ≦ Ts, the process proceeds to S19, but if Tw> Ts, the process proceeds to S21 and normal valve timing control is performed.

  In S19, it is determined whether or not the deviation Er calculated in S13 is equal to or greater than a predetermined value θs (for example, 10 deg). This condition is determined because overshoot may occur when the VTC 113 is driven at a high speed by increasing the energization amount of the electromagnetic coil 324 even though the deviation Er is small. Therefore, if Er ≧ θs, the process proceeds to S20, but if Er <θs, the process proceeds to S21 and normal valve timing control is performed.

Although it is desirable to determine all of the conditions of S17 to S19, it may be configured to determine any of them, and further conditions may be added.
In S20, cranking is in progress and there is no problem even if the energization amount to the electromagnetic coil 324 is increased. Therefore, the valve timing of the intake valve 105 is quickly changed from the most retarded timing to the start timing. A control signal EVTCDYT having a predetermined duty value (Duty = n%) is output to the VTC 113 (the electromagnetic coil 324) so as to control. Here, the duty value to be output may be a fixed value (for example, n = 100%). However, a duty value to be output is determined in advance according to the deviation Er, and a table or the like is created in advance. It is desirable to variably set. This is because the timing is accurately controlled at the time of starting. In this case, the duty value may be further corrected according to the coolant temperature Tw.

FIG. 14 is a flowchart for setting the target rotation phase θtg, and is executed in S11 of FIG.
In S101, it is determined whether or not the engine is rotating (whether rotation has started). If the engine is rotating, the process proceeds to S102. If the engine is not rotating, the VTC 113 does not operate. Therefore, the process proceeds to S105 and the target rotation phase θtg is set to 0 (deg).

In S102, it is determined whether or not the start switch (or starter motor) is ON as in S14 of FIG. If the start switch (starting motor) is ON, the process proceeds to S103, and if it is OFF, the process proceeds to S104.
In S103, assuming that the engine is starting (during cranking), a target rotation phase (starting timing) θtg for starting is set. Specifically, this setting is performed by searching a table as shown in the figure based on the coolant temperature (engine temperature) Tw. Here, the target rotation phase θtg for starting is set to be larger as the coolant temperature Tw is lower (set to the advance side). This is because at the time of cold start, the closing timing IVC of the intake valve 105 is brought close to the intake bottom dead center (BDC) to increase the effective compression ratio and improve the startability. The vibration is reduced by moving away from it.

  In S104, the normal rotation target rotation phase (normal timing) θtg is set on the assumption that the normal operation is being performed. Specifically, as shown in the figure, the target rotational phase θtg is set with reference to a map based on the engine rotational speed Ne and the engine load (target volume efficiency ηV). Considering that the required valve timing changes in accordance with the temperature (engine temperature) Tw, the map to be referred to is switched according to the coolant temperature Tw.

  As described above, in the present embodiment, when the engine is started, the target rotational phase θtg that is a valve timing suitable for starting the engine is set, and as a general rule, the actual rotational phase θdet is set to be the target rotational phase θtg (to be close). Forward control is performed. As a result, when the engine is started, the valve timing can be controlled with good response from the state where the engine is stopped to the valve timing at the start, and fuel is injected and ignited before the start timing is reached. (Explosion) can be avoided, and mission deterioration and combustion instability can be prevented. On the other hand, when it is determined that it is not appropriate to perform feedforward control even when the engine is started, or when the engine is in normal operation, the actual rotational phase θdet is set to the target rotational phase θtg as in the conventional case. Feedback control is performed so as to match.

In the embodiment described above, the intake valve 105 provided with the VTC 113 has been described. However, the same applies to the case where the exhaust valve 107 is provided with the VTC 113.
Further, if the rotational phase of the intake camshaft 134 relative to the crankshaft 120 can be detected at an arbitrary timing, the second rotational phase detector is not limited to the above, and the cycle is shorter than the rotational cycle of the intake camshaft 134. A device that detects the rotational phase may be substituted.

Furthermore, although the electromagnetic VTC has been described above, the present invention may be applied to a hydraulic VTC (for example, one having a means for increasing the hydraulic pressure when the engine is started).
Here, the technical idea other than the claims that can be grasped from the above-described embodiment will be described together with the effects thereof (a) In the control device for the variable valve timing mechanism according to any one of claims 1 to 3,
Temperature detecting means for detecting the engine temperature,
When the engine temperature detected by the temperature detecting means exceeds a predetermined temperature, the feedforward control is prohibited. When the temperature of the electromagnetic coil (actuator) of the variable valve timing mechanism is high, Thus, it is possible to avoid a situation where the energization amount to the electromagnetic coil is increased and the coil temperature is excessively increased.
(B) In the control apparatus for a variable valve timing mechanism according to any one of claims 1 to 3 and (a) above,
Voltage detecting means for detecting the battery voltage;
When the battery voltage detected by the voltage detection means falls below a predetermined value, the fee forward control is prohibited.

In this way, when the variable valve timing mechanism does not operate even when the drive signal is output, it is possible to avoid a situation in which the battery voltage is further lowered by performing the feedforward control.
(C) In the control device for the variable valve timing mechanism according to claim 2 or 3,
The target rotational phase is set according to the engine temperature,
A feedforward operation amount output to the variable valve timing mechanism is set according to a deviation between the actual rotational phase and the set target rotational phase.

  This makes it possible to perform highly responsive and highly accurate valve timing control even when starting the engine while setting a target rotational phase (valve timing) suitable for starting the engine from both aspects of improving startability and reducing vibration. be able to.

1 is a system configuration diagram of an internal combustion engine according to an embodiment. It is sectional drawing which shows the variable valve timing mechanism (VTC) which concerns on embodiment. It is AA sectional drawing of FIG. It is BB sectional drawing of FIG. Sectional drawing which shows the operating state of the said VTC (equivalent to AA sectional drawing). It is a graph which shows the magnetic flux density-magnetic field characteristic of a hysteresis material. It is a partial expanded sectional view of FIG. FIG. 8 is a schematic diagram in which the component of FIG. 7 is developed linearly, and shows the flow of magnetic flux in the initial state (a) and when the hysteresis ring rotates (b). It is a graph which shows the brake torque-rotation speed characteristic of the said VTC. It is a figure explaining the rotary body 401 and the gap sensor 402 which comprise a 2nd rotation position detection means. It is a graph which shows the gap-output characteristic of a gap sensor. It is a graph which shows the output-cam angle (rotation position) characteristic of a gap sensor. It is a flowchart of valve timing control concerning this embodiment. It is a flowchart which sets a target rotation phase.

Explanation of symbols

      DESCRIPTION OF SYMBOLS 101 ... Internal combustion engine, 105 ... Intake valve, 113 ... VTC (variable valve timing mechanism), 114 ... ECU (engine control unit), Crank angle sensor ... 117, 120 ... Crankshaft, 132 ... Cam sensor, 134 ... Intake side camshaft 401 ... Rotating body 402 ... Gap sensor

Claims (3)

In a control device for a variable valve timing mechanism that changes the opening / closing timing of an intake valve or an exhaust valve of an engine by changing a rotational phase of a camshaft with respect to a crankshaft of an internal combustion engine.
A rotational speed detecting means for detecting the engine rotational speed;
A rotation phase detecting means capable of detecting an actual value of the rotation phase at a cycle shorter than a rotation cycle of the camshaft;
The control of the direction in which the rotational phase coincides with the target rotational phase set according to the engine operating state, the engine rotational speed is equal to or lower than a predetermined rotational speed and the actual value of the rotational phase detected by the rotational speed detecting means and the target While the feed-forward control is performed when the deviation from the rotational phase is a predetermined value or more ,
A variable valve timing control device, wherein feedback control is performed when an engine rotational speed exceeds the predetermined rotational speed or when the deviation falls below the predetermined value . 2. The variable valve according to claim 1 , wherein when the amount of change of the engine rotation speed per predetermined time exceeds a predetermined value, the feedforward control is prohibited and the feedback control is performed. Control device for timing mechanism. The rotational phase detecting means is
A first sensor that outputs a signal for each reference rotational position and unit crank angle of the crankshaft;
A second sensor that outputs a different signal according to the rotational position of the camshaft,
3. The variable valve timing control device according to claim 1, wherein an actual value of the rotation phase is detected based on output signals of the first sensor and the second sensor . 4.

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