JP4328351B2 - Electronic imaging device - Google Patents

Description

  The present invention relates to an electronic image pickup apparatus having an image pickup element, and more particularly to an electronic image pickup apparatus with a dustproof function capable of removing dust attached to components such as a camera system.

Conventionally, as an example of a technique related to a dustproof function of an optical device, a technique has been proposed in which a protective glass (dustproof glass) that protects an image sensor is vibrated to remove dust attached to the glass. Specifically, for example, there is one taught in Patent Document 1, in which a piezoelectric element is used as means for vibrating a glass plate. This piezoelectric element expands and contracts in response to an applied voltage, and vibrates the attached glass plate at a predetermined cycle.
JP 2002-204379 A

Various accessory device are provided, the user is available by mounting the camera a desired accessory device. When the attachment and detachment of the accessory device to the camera to internally circulate external air camera enters the dust in air, is often the dust adheres to the surface of such an optical element and an imaging device of the camera . However, the above Patent Document 1 does not disclose the point of removing dust attached to the glass plate when the accessory device is attached or detached.

SUMMARY OF THE INVENTION An object of the present invention is to provide an electronic imaging device with a dustproof function that reliably removes dust adhering to components when an accessory device is attached or detached.

In order to solve the above problems and achieve the object, the present invention takes the following measures. That is, according to the first aspect, an electronic imaging device in which an accessory device can be attached and detached, an imaging element that converts an optical image of a subject into an electrical signal, and an optical element that is disposed on the imaging surface side of the imaging element When mounting of the piezoelectric element of the optical element to vibrate, a drive circuit for outputting the optical element at least two drive signals Ru is vibrated at the resonance frequency to the piezoelectric element, the accessory device to the electronic imaging device Accordingly , an electronic imaging apparatus is proposed that includes a control circuit that performs output control of a drive signal to the piezoelectric element by the drive circuit .

  Thus, according to the present invention, it is possible to provide an electronic imaging device with a dustproof function that can reliably remove dust adhering to the constituent members when the accessory device is attached or detached.

  Hereinafter, a camera system having an image pickup device and various accessories will be described as an example of an electronic image pickup device with a dustproof function according to the present invention, and will be described in detail based on embodiments. FIG. 1 is a block diagram showing the configuration of a camera system according to an embodiment of the present invention. This camera system includes a body unit 100 as a camera body, a lens unit 10 as an interchangeable lens as an accessory device (hereinafter abbreviated as “accessory”), a recording medium 27 for recording captured image data, The system is mainly composed of an external power supply 70 and an external strobe unit 80.

  The lens unit 10 desired by the user is detachably set via a lens mount (not shown) provided on the front surface of the body unit 100. The recording medium 27 is an external recording medium such as various memory cards or an external HDD, and is attached to the camera body via the communication connector 35 so as to be communicable and exchangeable. The above external power supply 70 has a built-in AC / DC converter function, and the necessary power can be obtained by inserting the plug 72 from, for example, a household power outlet to the jack 37 on the camera body via the attached connector 71 and plug 72. Supply is possible.

  The strobe unit 80 includes a flash bulb 81, a DC / DC converter 82, a strobe control microcomputer 83, and a battery 84, and can be attached to the camera body via a strobe communication connector 85.

  The lens unit 10 is controlled by a lens control microcomputer (hereinafter referred to as “Lucom”) 5. The body unit 100 is controlled by a body control microcomputer (hereinafter referred to as “Bucom”) 50. The Lucom 5 and Bucom 50 are electrically connected to each other via the communication connector 6 when they are combined. As a camera system, the Lucom 5 operates in cooperation with the Bucom 50 in a dependent manner.

  In the lens unit 10, a photographing lens 1 and a diaphragm 3 are provided. The taking lens 1 is driven by a DC motor (not shown) in the lens driving mechanism 2. The diaphragm 3 is driven by a stepping motor (not shown) in the diaphragm drive mechanism 4. Lucom 5 controls each of these motors in accordance with a command from Bucom 50.

  The following structural members are arranged in the body unit 100 as shown in the figure. For example, a single-lens reflex component member (quick return mirror 11, pentaprism 12, eyepiece lens 13, submirror 14) as an optical system, a focal plane shutter 15 on the optical axis, and a reflected light beam from the submirror 14 In response, an AF sensor unit 16 for automatic ranging is provided. Also, an AF sensor driving circuit 17 for driving and controlling the AF sensor unit 16, a mirror driving mechanism 18 for driving and controlling the quick return mirror 11, and a shutter for charging a spring for driving the front curtain and the rear curtain of the shutter 15. A charging mechanism 19, a shutter control circuit 20 that controls the movement of the front and rear curtains, and a photometric circuit 21 that performs photometric processing based on the light flux from the pentaprism 12 are provided.

  On the optical axis, a CCD unit 22 for photoelectrically converting the subject image that has passed through the optical system is provided as a photoelectric conversion element. Further, as an optical element disposed between the CCD unit 22 and the photographing lens 1. It is protected by the dustproof glass 30. For example, a piezoelectric element 31 is attached to the periphery of the dust-proof glass 30 as a part of the vibration means that vibrates the dust-proof glass 30 at a predetermined frequency.

  The piezoelectric element 31 has two electrodes (details will be described later). The piezoelectric element 31 vibrates the dust-proof glass 30 by the dust-proof glass driving circuit 40 as a part of the vibration means, and adheres to the glass surface. It is configured so that the dust that has been removed can be removed. Therefore, this camera system is an electronic camera having a basic structure belonging to a so-called “camera with dustproof function”. In order to measure the temperature around the CCD unit 22, a temperature measurement circuit 33 is provided in the vicinity of the dust-proof glass 30.

  This camera system is also provided with a CCD interface circuit 23 connected to the CCD unit 22, a liquid crystal monitor 24, an SDRAM 25 provided as a storage area, a Flash ROM 26, a recording medium 27, and the like, and an image processing controller 28 for image processing. In addition, the electronic recording display function can be provided together with the electronic imaging function. As other storage areas, a nonvolatile memory 29 made of, for example, an EEPROM is provided as a nonvolatile storage means for storing predetermined control parameters necessary for camera control, and is accessible from the Bucom 50.

  The Bucom 50 is provided with an operation display LCD 51 and a camera operation SW 52 for notifying the user of the operation state of the camera by display output. The camera operation SW 52 is a group of switches including operation buttons necessary for operating the camera, such as a release SW, a mode change SW, and a power SW. Further, a battery 54 as a power source and a power circuit 53a that converts the voltage of the power source into a voltage required by each circuit unit constituting the camera system and supplies the same are provided. Thus, a voltage detection circuit 53b for detecting a voltage change when the current is supplied is also provided.

  In the camera system configured as described above, each unit operates as follows. The image processing controller 28 takes in image data from the CCD unit 22 by controlling the CCD interface circuit 23 in accordance with an instruction from the Bucom 50. This image data is converted into a video signal by the image processing controller 28 and output and displayed on the liquid crystal monitor 24. The user can confirm the captured image from the display image on the liquid crystal monitor 24. The SDRAM 25 is a memory for temporarily storing image data, and is used as a work area when image data is converted. The image data is set to be stored in the recording medium 27 after being converted into JPEG data.

  The CCD unit 22 is protected by a transparent dustproof glass 30. A piezoelectric element 31 for oscillating the glass surface is disposed on the periphery of the dust-proof glass 30, and the piezoelectric element 31 serves as a driving means for this purpose as will be described in detail later. It is driven by the drive circuit 40. It is more preferable for dust prevention that the CCD unit 22 and the piezoelectric element 31 are housed integrally in a case having the dust-proof glass 30 as one surface and surrounded by a frame as indicated by a broken line.

  Normally, temperature affects the elastic modulus of glass materials and is one of the factors that change its natural frequency. Therefore, the temperature must be measured during operation to take into account the change in natural frequency. Don't be. It is better to predict the natural frequency at that time by measuring the temperature change of the dust-proof glass 30 provided to protect the front surface of the CCD unit 22 where the temperature rises rapidly during operation. Therefore, in this example, a sensor (not shown) connected to the temperature measurement circuit 33 is provided to measure the ambient temperature of the CCD unit 22. The temperature measurement point of the sensor is preferably set in the vicinity of the vibration surface of the dustproof glass 30.

  The mirror driving mechanism 18 is a mechanism for driving the quick return mirror 11 to the UP position and the DOWN position. When the quick return mirror 11 is at the DOWN position, the light flux from the photographing lens 1 is on the AF sensor unit 16 side. The light is divided and guided to the pentaprism 12 side. The output from the AF sensor in the AF sensor unit 16 is transmitted to the Bucom 50 via the AF sensor driving circuit 17 and a known distance measurement process is performed.

  The eyepiece 13 adjacent to the pentaprism 12 allows the user to see the subject, while part of the light beam that has passed through the pentaprism 12 is guided to a photosensor (not shown) in the photometry circuit 21 where it is detected. A well-known photometric process is performed based on the light quantity.

  Next, based on the circuit diagram of the dust-proof glass drive circuit 40 shown in FIG. 2 and the time chart of FIG. 3, the drive of the dust-proof glass 30 of the camera with a dust-proof function in this embodiment, its operation | movement, and control are demonstrated. The dust-proof glass driving circuit 40 exemplified here has a circuit configuration as shown in FIG. 2, and waveform signals (Sig 1 to Sig 6) shown in the time chart of FIG. 3 are generated in each part, and based on those signals. Is controlled as follows. That is, as shown in FIG. 2, the dust-proof glass driving circuit 40 includes an N-ary counter 41, a 1/2 frequency divider circuit 42, an inverter 43, a plurality of MOS transistors (Q00, Q01, Q02) 44a, 44b, 44c, and a transformer 45. , Resistor (R00) 46, A / D converter 60, first electrode A of piezoelectric element 31 and second electrode B61 aligned therewith, diode (D00) 62, resistors (R01, R02) 63, 64, and capacitor (C00) 65.

  The ON / OFF switching operation of the transistor (Q01) 44b and the transistor (Q02) 44c connected to the primary side of the transformer 45 causes a signal (Sig4) having a predetermined cycle to be generated on the secondary side of the transformer 45. It is configured to search for an efficient resonance frequency and effectively resonate the dust-proof glass 30 while variously driving the piezoelectric element 31 having the two electrodes A and B based on the signal of this predetermined period. (Details will be described later).

  The Bucom 50 controls the dustproof glass driving circuit 40 through the two IO ports P_PwCont and IO port D_NCnt provided as control ports and the clock generator 55 existing inside the Bucom 50 as follows. The clock generator 55 outputs a pulse signal (basic clock signal) to the N-ary counter 41 at a frequency sufficiently faster than the signal frequency applied to the piezoelectric element 31. This output signal is a signal Sig1 having a waveform represented by the time chart in FIG. This basic clock signal is input to the N-ary counter 41.

  The N-ary counter 41 counts the pulse signal and outputs a count end pulse signal every time it reaches a predetermined value “N”. That is, the basic clock signal is divided by 1 / N. This output signal is a signal Sig2 having a waveform represented by the time chart in FIG. In this divided pulse signal, the duty ratio between High and Low is not 1: 1. Therefore, the duty ratio is converted to 1: 1 through the 1/2 frequency divider circuit.

  The converted pulse signal corresponds to the signal Sig3 having a waveform represented by the time chart in FIG. In the High state of the converted pulse signal, the MOS transistor (Q01) 44b to which this signal is input is turned on. On the other hand, this pulse signal is applied to the transistor (Q02) 44c via the inverter 43. Therefore, in the low state of the pulse signal, the transistor (Q02) 44c to which this signal is input is turned on. When the transistor (Q01) 44b and the transistor (Q02) 44c connected to the primary side of the transformer 45 are alternately turned on, a signal having a cycle such as the signal Sig4 in FIG. 3 is generated on the secondary side.

  The winding ratio of the transformer 45 is determined from the output voltage of the unit of the power supply circuit 53 and the voltage necessary for driving the piezoelectric element 31. The resistor (R00) 46 is provided to limit an excessive current flowing through the transformer 45. When driving the piezoelectric element 31, the transistor (Q00) 44a must be in an ON state, and a voltage must be applied from the power supply circuit 53 unit to the center tap of the transformer 45. In the figure, ON / OFF control of the transistor (Q00) 44a is performed via P_PwCont of the IO port. The set value “N” of the N-ary counter 41 can be set from the IO port D_NCnt. Therefore, the Bucom 50 can arbitrarily change the drive frequency of the piezoelectric element 31 by appropriately controlling the set value “N”.

  At this time, the frequency can be calculated by the following equation.

N: set value to counter, fpls: frequency of output pulse of clock generator, fdrv: frequency of signal applied to piezoelectric element, fdrv = fpls / 2N (1)
The calculation based on this equation is performed by the CPU (control means) of the Bucom 50.

  The electrode B61 is an electrode of a piezoelectric element for detecting the vibration state of the glass plate. An alternating voltage (monitor signal) corresponding to the vibration state of the glass plate is generated from the electrode B61. This is Sig5 on the time chart of FIG. A diode (D00) 62 connected to the electrode B61 is provided for half-wave rectification of the monitor signal. An envelope of the monitor signal is formed by the resistors (R01, R02) 63 and 64 and the capacitor (C00) 65 following the diode (D00) 62. The optimum value of the time constant determined by the detection circuit including the resistors (R01, R02) 63 and 64 and the capacitor (C00) 65 varies depending on the vibration frequency of the glass. The glass plate of this embodiment is driven in two resonance modes (first and second drive modes). When the drive frequencies in these two resonance modes are greatly different, it is necessary to adopt a circuit configuration so that the time constant can be changed. The monitor signal is reduced to a level that can be input to the A / D converter 60 by the resistors (R01, R02) 63, 64. This signal is Sig6 on the time chart of FIG.

  This signal is converted into digital data by the A / D converter 60 and read from the IO port D_DACin of the Bucom 50. The Bucom 50 may change the value set in the N-ary counter 41 so that the monitor signal becomes the maximum level. When the glass is driven with the value (resonance frequency) of the N-ary counter 41 indicating the maximum level, dust can be efficiently removed.

  The control performed by the camera body control microcomputer (Bucom) 50 will be described in detail based on the main routine of the control program shown in FIG. When the camera power SW (not shown) is turned on, the Bucom 50 starts operation. In # 000, first, processing for starting the camera system is executed. The power supply circuit 53 is controlled to supply power to each circuit unit constituting this camera system. Also, initial setting of each circuit unit is performed.

  In # 001, the subroutine “resonance point detection operation” is called and executed. In this subroutine, a driving frequency (resonance frequency) suitable for efficiently vibrating the dustproof glass 30 is detected (details will be described later). The frequency data for this purpose is stored in a memory area of a predetermined address of Bucom 50.

  Subsequently, in # 002, the subroutine “dust removal operation” is called and executed. During this subroutine, the dust-proof glass 30 is vibrated at the resonance frequency detected in # 001 and the dust adhering to the glass surface is shaken off. The attached dust can be removed.

  In processing steps # 003 to # 0105, which is one of the characteristic features of the present invention, whether or not various accessories are attached and their states are sequentially checked. First, # 003 is a step periodically executed, and is an operation step for detecting the state of the lens unit 10 by performing a communication operation with Lucom5. If it is detected in # 0041 that the lens unit 10 is attached to the body unit 100, the process proceeds to # 0044. On the other hand, when it is detected that the lens unit 10 is detached from the body unit 100, the process proceeds from # 0042 to # 0043, and the control flag F_Lens is reset. Then, the process proceeds to # 005. In # 0044, the control flag F_Lens is set. This control flag indicates “1” when the lens unit 10 is attached to the body unit 100 of the camera, and indicates “0” when the lens unit 10 is removed.

  # 005 is a step periodically executed, and is a step in which the state of the communication connector 35 is determined to detect the state in which the recording medium 27 is mounted in the body unit 100. In # 0061, when it is detected that the recording medium 27 is mounted in the body unit 100, the process proceeds to # 0064. On the other hand, when it is detected that the recording medium 27 has been removed from the body unit 100, the process proceeds from # 0062 to # 0063, and the control flag F_Medium is reset. Then, the process proceeds to # 010. In # 0064, the control flag F_Medium is set. Then, the process proceeds to # 008. This control flag indicates “1” when the recording medium 27 is mounted in the body unit 100 of the camera, and indicates “0” during the removal period.

  Similarly, the strobe unit 80 as an accessory, the external power source 70, and the like can be determined by the following processing procedure. That is, # 010 is a step periodically executed, and it is determined whether or not the strobe unit 80 is attached to the body unit 100 by determining the state of the strobe communication connector 85. If it is detected at # 0100 that the strobe unit 80 is attached to the body unit 100, the process proceeds to # 0103, the control flag F_Strobe is set, and then the process proceeds to # 008. On the other hand, when it is detected that the strobe unit 80 is taken out from the body unit 100, the process proceeds from # 0101 to # 0102, the control flag F_Strobe is reset, and then the process proceeds to # 0104.

  This control flag also indicates “1” when the strobe unit 80 is attached and indicates “0” when it is removed.

  Next, # 0104 is also a step periodically executed, and it is determined whether or not the plug 72 is inserted into the jack 37 of the body unit 100 by determining the state of the jack 37. If the connection of the external power supply 70 can be detected as the plug 72 is inserted into the jack 37 at # 0105, the process proceeds to # 008. If the connection of the external power supply 70 is not detected, the process proceeds to # 014. Specifically, when a current is supplied to the power supply circuit 53a and the voltage detection circuit 53b via the external power supply 70, a change in voltage occurs, which can be detected. Therefore, the connection state can be known here without setting a dedicated control flag.

  When any of the above-mentioned accessories is mounted, the subroutine “resonance point detection operation” is called and executed in the same manner as described above in # 008, and in # 009 immediately thereafter, the dust-proof glass 30 is similarly installed. A subroutine “dust removal operation” for removing dust is called and executed.

  Usually, there is a high possibility that dust adheres to the lens, the dust-proof glass 30 and the like during a period when the lens unit 10 is not attached to the body unit 100 which is a camera body. Therefore, it is desirable to perform the dusting operation at the timing when the mounting of the lens unit 10 is detected. Further, when the lens is exchanged or an accessory is attached, external air may circulate inside the camera and the temperature inside the camera may change. Therefore, the resonance frequency of the glass also changes with this temperature change. Therefore, in # 008, the "resonance point detection operation" is executed to determine a new drive frequency (resonance frequency). Subsequently, in # 009 immediately thereafter, the "dust removal operation is performed at the determined frequency. "Is to be executed.

  In # 014, it is determined whether or not a first release SW (not shown), which is one of the camera operation SWs, has been operated. If the 1st release SW is ON, the process proceeds to # 015, and if it is OFF, the process proceeds to # 003 again.

  In # 015, the luminance information of the subject is obtained from the photometry circuit 21. From this information, the exposure time (Tv value) of the CCD unit 22 and the aperture setting value (Av value) of the photographing lens 1 are calculated. In # 016, the detection data of the AF sensor unit 16 is obtained via the AF sensor drive circuit 17. Based on this data, the amount of focus shift is calculated. Here, in # 017, the state of F_Lens is determined. If it is “0”, it means that the lens unit 10 does not exist, and therefore the next photographing operation after # 018 cannot be executed. Therefore, in this case, the process shifts to # 003 again.

  In # 018, the amount of focus shift is transmitted to Lucom 5, and the driving of the photographing lens 1 based on this amount of shift is commanded. In # 019, it is determined whether or not a 2nd. Release SW (not shown), which is one of the camera operation SWs 52, has been operated. When the 2nd. Release SW is ON, the process proceeds to # 0190, but when it is OFF, the process proceeds to # 003 again.

  In # 0190, the presence / absence of a recording medium is determined based on the value of the control flag F_Medium. If it is other than “1”, the process proceeds to # 003 again. On the other hand, if “1”, a “dust removal operation” routine is executed to remove dust prior to the photographing operation. However, in order to avoid the occurrence of a time lag due to this operation, the “resonance point detection operation” routine is not executed here.

  In order to reliably remove dust, it is desirable to perform the operations of these two routines together. However, if there is no possibility that the resonance frequency will change, the “resonance point detection operation” routine may be omitted. Note that the omission of execution of this routine is not limited to this, not only when the lens is replaced, but also when the camera system is powered on or when the sleep state is canceled. However, in the continuous shooting mode, the execution of this routine may be omitted after the second imaging operation.

  As an image pickup operation, first, an Av value is transmitted from # 020 to Lucom 5 to instruct to drive the diaphragm 3, and in # 021, the quick return mirror 11 is moved to the UP position. In step # 022, the shutter 15 starts to travel to the front curtain, and the shutter 15 is opened. In # 0220, if the control flag F_Strobe is set to “1”, the strobe is emitted in # 0230, otherwise the strobe is not emitted and the image processing controller 28 is imaged in # 023. Command execution of action.

  When imaging by the CCD unit 22 is completed for the time indicated by the Tv value, the rear curtain travel of the shutter 15 is started in # 024, and the quick return mirror 11 is driven to the Down position in # 025. In parallel with this, the shutter 15 is charged. In # 026, Lucom 5 is instructed to return the diaphragm 3 to the open position, and in # 027, the image processing controller 28 is instructed to record the captured image data on the recording medium 27. When the recording of the image data ends, the process proceeds to # 003 again, and a series of similar processing steps are repeated.

  Hereinafter, the sub-routine “resonance point detection operation” will be described in detail based on the flowchart illustrated in FIG. 5 and FIGS. 7A to 11B. Before that, the support structure and vibration mode of the dust-proof glass 30 to be resonated will be outlined with reference to FIGS. 7 (a) to 8 (b). In the electronic imaging device according to the present invention, the dust-proof glass 30 is assumed to be a disk. When the piezoelectric element 31 for vibration is arranged along the circumference of the glass plate of the dustproof glass 30, the glass plate is supported on the circumference. At this time, the glass plate vibrates in a plurality of vibration modes (vibration modes). In the present invention, two modes are selected from these vibration modes and used separately. FIGS. 7A and 7B and FIGS. 8A and 8B show the vibration state of the glass plate in the selected vibration mode.

  The dust-proof glass 30 according to this embodiment exhibits a vibration mode as illustrated in FIGS. 7A and 7B. That is, when vibration is applied by the piezoelectric element 31 acting as a vibration means, “nodes” that do not vibrate are generated around the glass plate, but the entire surface of the glass is generally in the same phase as shown by the thick arrows. 7 (a) and FIG. 7 (b) are alternately repeated to vibrate. Such a vibration mode is hereinafter referred to as “vibration mode 1”.

  Similarly, the dust-proof glass 30 of this embodiment can vibrate in the form shown in FIGS. 8A and 8B, depending on the frequency of vibration applied. That is, the vibration mode of the dust-proof glass 30 illustrated in FIGS. 8A and 8B is that the glass plate vibrates with a phase shifted by 180 degrees. Specifically, in the illustrated vibration mode, nodes are generated around and inside the glass plate. As shown in the figure, the vibration in the region surrounded by the inner node and the outer region of the inner node (the donut-shaped region) ) Is 180 degrees out of phase. Hereinafter, this is referred to as “vibration mode 2”.

  Therefore, in the subroutine “resonance point detection operation” shown in FIG. 5, the resonance frequency detection operation in the two vibration modes of vibration mode 1 and vibration mode 2 described above is performed first. Since a range where the resonance frequency exists can be predicted depending on the characteristics of glass (for example, shape, composition, support method, etc.), the resonance point should be detected by applying vibration to the glass plate within this range. Otherwise, the detection operation takes longer than necessary. If the detection range is not assumed, there is a risk of detecting the resonance frequency in a higher-order resonance mode other than the intended vibration mode.

  Therefore, in the present embodiment, parameters necessary for the detection operation of the resonance frequency are stored in advance in the EEPROM 29 having a plurality of areas shown by the memory map in FIG. It has as. The details of the control parameter values corresponding to the vibration mode 1 are stored as the values illustrated in FIG. For example, StartOffset indicates the reading start position of this table.

  Similarly, the details of the control parameter values corresponding to the vibration mode 1 are stored as values illustrated in FIG. 11A as the “vibration mode 1 frequency correction table”. Such a data table shows values set in the N-ary counter 41 when the glass is driven in the vibration mode 1. This table is calculated on the assumption that the clock generator 55 outputs a pulse signal having a frequency of 40 (MHz). The driving frequency can be calculated by using (Expression 1) already described.

  StopOffset indicates the read end position of the vibration mode 1 compatible frequency correction table. When the drive frequency is changed in the range from StartOffset to StopOffset, the glass plate vibrates in the vibration mode 1 with any table value.

  StepTime indicates the time to drive at one frequency when the drive frequency is changed. This is determined in consideration of the stabilization time of the dustproof glass driving circuit 40. Even when the drive frequency is changed, the vibration of the glass plate does not immediately follow. If it does not follow, the monitor signal output cannot be relied upon.

  ADwait is a parameter that determines the frequency at which the monitor signal is A / D converted, and is determined to an appropriate value according to the resonance frequency of the glass. M1OscTime indicates the time for which the dustproof glass 30 is vibrated at the detected frequency. This is necessary in the subroutine “dust removal operation”. The above are the control parameters in the vibration mode 1. Details of the control parameters corresponding to the vibration mode 2 are shown in FIG. Details of the frequency correction table corresponding to the vibration mode 2 are shown in FIG. 11B and are parameters having the same configuration as that of the vibration mode 1 and are basically the same as those in FIG.

  Further, the procedure of “resonance point detection operation” will be described based on the flowchart of FIG. 5 and FIGS. 9 to 12. In # 100, four control parameters (StartOffset, StopOffset, StepTime, ADwait) are read from the EEPROM 29. In # 101, Address M1 + StartOffset is set as the read start address of the EEPROM 29, and Address M1 + StopOffset is set as the read end address. Address M1 indicates the head address of the vibration mode 1 frequency correction table.

  If the read start position (StartOffset) is set to “3” and the read end position (StopOffset) is set to “9”, the preset value “N” in the area indicated by * 1 to * 2 in FIG. Is set in the N-ary counter 41. That is, the frequency at which the output of the monitor signal is maximum is detected from the frequencies f1, f2, f3,..., F7.

  In # 102, # 0, which is the minimum value of the monitor signal, is set for convenience in the memory D_ADMAX reserved for temporarily storing the maximum value of the monitor signal. In # 103, a preparatory operation for driving the piezoelectric element 31 is performed. The transistor Q00 is turned on by controlling the P_PwCont of the IO port. Further, output of a pulse signal from the clock generator 55 is started. If the data extracted from the table is set in the N-ary counter 41 in this state, the piezoelectric element 31 can be driven at a desired frequency.

  In step # 104, the preset value (N) is read from the set address of the EEPROM 29. Then, the preset value read from the D_NCnt of the IO port to the N-ary counter 41 is set. In step # 105, the system waits for a predetermined time until the frequency driving circuit is stabilized.

  In # 106, Steptime is set in the timer counter 1, and the timer counting operation is started. For example, as shown in FIG. 10A, if Steptime is stored, 2 (msec) is set in the timer counter 1. In # 107, # 0 is set in the memory area D_ADSUM reserved for temporarily storing the addition data of the A / D converter 60. Further, # 0 is set in the memory D_ADcount reserved for counting the number of operations of the A / D converter 60.

  In # 108, ADwait is set in the timer counter 2 and the count operation is started. For example, when ADwait is stored as shown in FIG. 10A, 80 (μsec) is set in the timer counter 2. In step # 109, the A / D conversion value of the monitor signal is acquired using the A / D converter 60.

  In # 110, the A / D conversion value of the monitor signal is added to the memory area D_ADSUM. Further, the memory area D_ADcount is incremented (1 is added). In # 111, it waits until the count operation of the timer counter 2 is completed. In step # 112, it is determined whether or not the count operation of the timer counter 1 has been completed. If it has not been completed yet, the process proceeds to # 108 to measure the monitor signal again. If completed, the process proceeds to # 113.

  In step # 113, an average value of AD conversion values is obtained from the memory areas D_ADSUM and D_ADcount. The average value is stored in the memory area D_ADAVE reserved for recording the average value. D_ADAVE indicates the level of the monitor signal at the current drive frequency. In # 114, the contents of D_ADAVE and D_ADMAX are compared. If the contents of D_ADAVE is larger than the contents of D_ADMAX, the process proceeds to # 115, and if smaller, the process proceeds to # 119.

  In step # 115, the contents of D_ADAVE are moved into D_ADMAX. The old maximum value is discarded, and the value measured this time is stored as the maximum value of the monitor signal. If the monitor signal is currently being measured in the vibration mode 1, the process proceeds from # 116 to # 117. If the monitor signal is currently being measured in the vibration mode 2, the process proceeds from # 116 to # 118.

  In # 117, the address of the current EEPROM 29 is stored in D_M1resonant. D_M1resonant is an area secured on the memory to store the address for vibration mode 1. In # 118, the current EEPROM address is stored in D_M2resonant. D_M2resonant is an area secured on the memory to store the address for vibration mode 2. These values of D_M1resonant and D_M2resonant are used in a subroutine “dust removal operation” described later.

  In step # 119, it is determined whether or not the measurement of the monitor signal is completed up to the drive frequency indicated by the EEPROM read end address. If not completed yet, the process proceeds to # 121, and if completed, the process proceeds to the next # 120. In # 120, a process for stopping the driving operation is performed. The transistor Q00 is turned off to stop the operation of the clock generator. In # 121, the read address of the EEPROM 29 is incremented, and the process proceeds to # 104.

  In # 122, it is determined whether or not the resonance point detection operation in the vibration mode 1 and the vibration mode 2 is completed. If both detection operations are completed, the process returns to the main routine. When only the vibration mode 1 is completed, the process proceeds to # 130 in order to detect the resonance frequency in the vibration mode 2. Since the operations of # 130 and # 131 are basically the same as those of # 100 and # 101 already described, description thereof will be omitted. Then, the process shifts again to # 102 to detect the resonance frequency.

  In this subroutine, preset values are read from the frequency correction table within a range defined by two parameters (StartOffset, StopOffset). The glass plate is driven using all the preset values to measure the level of the monitor signal.

  FIG. 12 shows the relationship between the frequency and the amplitude of the glass plate. It is assumed that * 3 indicates the resonance mode 1 characteristic. In this routine, the monitor signal level is measured at the frequencies (preset values) f1, f2, f3,..., F7 illustrated in FIG. The resonance frequency in the characteristic of * 3 is fc. fc corresponds to f4. In this routine, the monitor signal is measured while changing the drive frequency in order of f1, f2, f3, and f4. Even after the resonance frequency fc is passed, the driving is continued in order of f5, f6, and f7.

  In f1 to f4, the monitor signal is in an increasing direction. Then, the monitor signal changes in a decreasing direction from f5. Therefore, if the change of the monitor signal from the increasing direction to the decreasing direction is detected, there is no need to drive with the frequencies of f6 and f7. If the frequency change range is wide, it is desirable to create a control program as illustrated here in order to shorten the detection time of the resonance frequency.

  Here, the subroutine “dust removal operation” shown in FIG. 6 will be described. In this subroutine, the piezoelectric element 31 is set to be driven so that the dust-proof glass 30 is resonated in the two modes of vibration mode 1 and vibration mode 2 described above. Generally, the frequency and amplitude at which dust is easily removed vary depending on the characteristics of the dust (for example, weight, shape, material, etc.). Therefore, in order to remove dust reliably, the glass plate should be resonated in these two vibration modes. Of course, you may resonate in more than one vibration mode. However, since the time required for the removal operation may also be increased by that amount, an appropriate number should be set in consideration of the degree of the removal effect and the required time.

  Therefore, first, in # 200, M1OSCtime is read from the vibration mode 1 compatible control parameter of the EEPROM 29, and M2OSCtime is read from the vibration mode 2 compatible control parameter. In # 201, a preparatory operation for driving the piezoelectric element 31 is performed. The P_PwCont of the IO port is controlled to turn on the transistor Q00. Further, output of a pulse signal from the clock generator 55 is started. If the data extracted from the table of the EEPROM 29 is set in the N-ary counter 41 in this state, the piezoelectric element 31 can be driven at a desired frequency.

  In # 202, the preset value (N) is read from the address of the EEPROM 29 indicated by D_M1resonant. This value is set in the N-ary counter 41. Thereby, the dustproof glass driving circuit 40 drives the glass plate at the resonance frequency of the vibration mode 1. In # 203, M1OscTime is set in the timer counter 1, and the count operation is started. For example, if M1OscTime is stored as shown in FIG. 10A, 200 (msec) is set to the timer counter 1. In step # 204, the process waits until the count operation of the timer counter 1 is completed. Thus, the dust removal operation in the vibration mode 1 is completed. Further, the glass plate is vibrated in the vibration mode 2 in order to surely perform dust removal.

  In # 205, the preset value (N) is read from the address of the EEPROM 29 indicated by D_M2resonant. This value is set in the N-ary counter 41. Thereby, the dustproof glass driving circuit 40 drives the glass plate at the resonance frequency of the vibration mode 2. In # 206, M2OscTime is set in the timer counter 2, and the count operation is started. For example, if M2OscTime is stored as shown in FIG. 10B, 100 (msec) is set in the timer counter 2.

  In # 207, the process waits until the count operation of the timer counter 2 is completed. In # 208, a process for stopping the driving operation is performed. The transistor Q00 is turned off and the operation of the clock generator 55 is stopped. Thereafter, the process returns to the main routine.

  It should be noted that it is very difficult to predict variations in the resonance frequency of the glass plate at the design stage of the camera system. Therefore, it should be possible to set a control parameter for determining the drive frequency of the piezoelectric element 31 after the camera system is completed. Therefore, all necessary parameters are stored in the EEPROM 29 so as to be selectable in the present invention as described above. Further, in this subroutine “dust removal operation”, the glass plate is driven only at the resonance frequency detected in the subroutine “resonance point detection operation” described above.

  FIG. 12 shows the relationship between the frequency and the amplitude of the glass plate. The characteristic when executing the subroutine “resonance point detection operation” is * 3. The resonance frequency fc is assumed to correspond to f4 in FIG. However, there is a possibility that the characteristic fluctuates as * 4 and * 5 due to an unexpected factor of the resonance frequency. In order to be able to cope with such fluctuations, the subroutine may be executed by reading the data of f3 and f5 other than f4 from the table of the EEPROM 29.

  In addition, since the resonance frequency fluctuates within a certain range depending on the temperature, the temperature correction table created by a predetermined experiment is appropriately set and retained so that it can be referred to. The glass plate may be driven. For this purpose, temperature information (t) is read by a temperature sensor (not shown) of the temperature measurement circuit 33 before executing this subroutine in order to read out the parameter corresponding to the temperature at that time from the temperature correction table corresponding to the vibration mode. It only has to be detected.

  As described above, according to the electronic image pickup apparatus (for example, a camera) with a dustproof function of the embodiment, accessories such as the recording medium 27, the external power supply 70, or the strobe unit 80 can be attached and detached in addition to the lens unit 10. And a dust removing means (piezoelectric element 31 and dust-proof glass driving circuit 40) for removing dust adhering by vibrating the glass at a plurality of types of frequencies. Therefore, the dust removal operation can be performed by the resonance operation of the piezoelectric element 31 at an effective timing according to the attachment of any of the above accessories.

  In particular, in the dustproof function here, a resonance frequency detection mode for driving the vibration means (piezoelectric element 31) to detect the resonance frequency of the optical element (dustproof glass 30) and the dust adhering to the optical element are removed. In order to do this, it has a dust removal mode for driving the piezoelectric element 31, and basically executes the resonance frequency detection mode and the dust removal mode continuously at the timing when the accessory device is mounted. Yes. Also, the resonance frequency detection operation is omitted immediately before shooting so as not to give a time lag due to the time required for resonance frequency detection during shooting. Therefore, dust can be removed efficiently and reliably without adversely affecting the shooting timing.

  (Modification) As described above, the embodiment of the protective glass (dust-proof glass) has been described by taking the camera system as an example of the electronic imaging device. However, in other electronic imaging devices that dislike dust and dust, the configuration other than the dust-proof glass If the present invention is similarly applied to members and other parts, the same effects as those of the above-described embodiment can be obtained. In addition, an optical element member other than glass whose resonance frequency cannot be specified can also be applied. In this case, adjustment to the natural resonance frequency due to variations in individual products is unnecessary, and the same effect as described above can be expected. In addition, various modifications can be made without departing from the scope of the present invention.

The block block diagram which shows the structure of the camera of embodiment concerning this invention. The circuit diagram which shows the circuit structure of the vibration means (dust-proof glass drive circuit) as embodiment of this invention. FIG. 3 is a time chart showing signal waveforms at various parts in FIG. 2 in order to explain the operation of the dustproof glass driving circuit. The flowchart showing the procedure of the camera sequence of the microcomputer for camera body control. 5 is a flowchart showing a detailed procedure of a routine “resonance point detection operation” in the flowchart of FIG. 4. 5 is a flowchart showing a detailed procedure of a routine “dust removal operation” in the flowchart of FIG. 4. FIGS. 7A and 7B show vibration modes of the dust-proof glass according to the present invention, and are explanatory diagrams of a mode in which nodes are generated around the glass plate and the entire surface vibrates in the same phase (vibration mode 1). FIGS. 8A and 8B show vibration modes of the dust-proof glass according to the present invention, and are explanatory diagrams of a mode (vibration mode 2) in which the inside and outside of the glass plate vibrate with a phase different by 180 °. The memory map which shows the table area | region regarding the frequency correction which occupies for EEPROM. 10A and 10B show control parameters related to frequency correction in the vibration mode, FIG. 10A is a list showing details of the control parameter table corresponding to vibration mode 1, and FIG. 10B corresponds to vibration mode 2. A list showing details of the control parameter table. 11A and 11B show correction values corresponding to the vibration mode, FIG. 11A is a detailed table of the frequency correction table corresponding to vibration mode 1, and FIG. 11B is a detail of the frequency correction table corresponding to vibration mode 2. table. The characteristic graph showing the relationship between a drive frequency and the amplitude of the vibration of a glass plate.

Explanation of symbols

    DESCRIPTION OF SYMBOLS 1 ... Shooting lens, 2 ... Lens drive mechanism, 3 ... Diaphragm, 4 ... Diaphragm drive mechanism, 5 ... Microcomputer for lens control, 6 ... Communication connector, 10 ... Lens unit (exchangeable lens), 11 ... Quick return mirror, 12 DESCRIPTION OF SYMBOLS ... Pentate prism, 13 ... Eyepiece, 14 ... Sub mirror, 15 ... Shutter (front curtain, rear curtain), 16 ... AF sensor, 17 ... AF sensor drive circuit, 18 ... Mirror drive mechanism, 19 ... Shutter charge mechanism, 20 ... Shutter control circuit, 21 ... photometry circuit, 22 ... CCD unit (photoelectric conversion element), 23 ... CCD interface circuit, 24 ... LCD monitor, 25 ... SDRAM, 26 ... Flash ROM, 27 ... Recording medium (accessory), 28 ... Image processing Controller 29 ... Nonvolatile memory (EEPROM) 30 ... Dust-proof glass (light Scientific element), 31 ... piezoelectric element (vibration means, dust removal means), 33 ... temperature measurement circuit, 35 ... communication connector, 37 ... jack, 40 ... dustproof glass drive circuit (vibration, drive means), 41 ... N 42 ... 1/2 frequency divider, 43 ... inverter, 44 ... transistor, 44a, 44b, 44c ... MOS transistor, 45 ... transformer, 46 ... resistor, 47 ... D / A converter, 48 ... VCO (voltage control) (Oscillator), 49 ... amplifier, 50 ... microcomputer for body control, 51 ... LCD for operation display, 52 ... camera operation SW, 53a ... power supply circuit, 53b ... voltage detection circuit, 54 ... battery, 55 ... clock generator, 60 ... A / D converter, 61... Electrode B (monitoring piezoelectric element electrode), 62... Diode (detection circuit element), 63 and 64. 5 ... Condenser (:), 70 ... External power supply (accessory), 71 ... Connector (plug for outlet), 72 ... Plug (pin jack), 80 ... Strobe unit (accessory), 81 ... Flash light bulb, 82 ... DC / DC Converter, 83 ... strobe control microcomputer, 84 ... battery (battery for strobe), 85 ... strobe communication connector.

Claims (4)

An electronic imaging device to which an accessory device can be attached and detached,
An image sensor that converts an optical image of a subject into an electrical signal;
An optical element disposed on the imaging surface side of the imaging element;
A piezoelectric element that vibrates the optical element;
A drive signal to the optical element Ru is vibrated in at least two resonant frequencies and driving circuit for outputting to said piezoelectric element,
A control circuit that performs output control of a drive signal to the piezoelectric element by the drive circuit according to the attachment of the accessory device to the electronic imaging device;
An electronic imaging device comprising: The drive signal output from the drive circuit includes at least a drive signal that vibrates the piezoelectric element with a resonance frequency that generates one node in the optical element, and a resonance signal that generates two nodes in the optical element. The electronic imaging apparatus according to claim 1, wherein the electronic imaging apparatus is a drive signal that vibrates . The electronic imaging apparatus according to claim 1, wherein the drive circuit generates the drive signal by dividing a basic clock . The accessory device is
4. The interchangeable photographing lens, at least one of an image recording medium for recording an electronic image picked up by the image pickup device, a strobe device, and an external power source. The electronic imaging device as described in any one of them.

Images