Abstract:
A camera includes a shutter unit for limiting the exposure time to a record medium, a shutter time setting unit for setting the shutter time of the shutter unit, a shutter drive and control unit for driving and controlling the shutter unit, a shutter condition detecting unit for detecting the condition of the shutter unit, a manifesting unit for manifesting the result detected by the shutter condition detecting unit, a manifestation control unit for driving and controlling the manifesting unit and a memory unit for previously storing inherent data to detect with the shutter condition detecting unit whereby a photographer is informed of the fact that the detection accuracy of the detecting element is insufficient for a shutter time, thus dealing with the situation. The manifestation control unit drives the shutter condition detecting unit, based on a shutter time set by the shutter time setting unit and inherent data stored in the memory unit, thus notifying the shutter condition detecting unit of the result.

Description:
This application is a continuation of application Ser. No. 08/350,053, filed Nov. 29, 1994, now abandoned. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention relates to a camera that includes a shutter running condition detecting means. 
     2. Related Background Art 
     Conventionally, in operation of cameras, the lens diaphragm limits the light flux from a photographing subject and the mechanical shutter limits the exposure time for a photographing film. The shutter used for the single-lens reflex camera is basically formed of two sheets of curtain including the leading curtain and the trailing curtain and the so-called leading curtain covers the picture surface of the film before the exposure operation. 
     First, when the shutter button is depressed, the leading curtain is withdrawn from the picture surface to start exposing the surface of the film to light. After a predetermined period of time, the trailing curtain covers the surface of the film. The run of each of the curtains is done by means of a spring force biased mechanically. The start of the run is made by releasing each curtain latched. In prior art, these operations have been totally done under mechanical control, but now are done under electrical control in most cases. Like the prior art, the spring force is utilized to run the leading and trailing curtains, but the start of the run is controlled by activating the electromagnet that latches the curtains. 
     On the other hand, increasing the shutter speed to, for example, {fraction (1/8000)} sec. has been one of the important specifications. Moreover, recent frequent uses of a stroboscopic photography have been required the stroboscopic synchronization at high speed by which can perform imaging under a bright environment. 
     In order to achieve the purposes, the running speed (the curtain speed) of each of the curtains must be sharply increased by strengthening the spring force and controlled so as to narrow the width of the slit formed by the leading and trailing curtains. Even if the activating timing of the electromagnet is controlled accurately, the releasing speed of the latching mechanism to the electromagnet as well as the variation in the mechanical running system including a spring may prevent the shutter from operating at a desired shutter time, and more particularly at a high speed over {fraction (1/8000)} sec. This phenomenon can be first found after developing the film. Hence, a shutter which includes means for detecting its operational condition during or immediately after a photographing operation has been proposed. 
     However, there has been a problem in that a small detecting element mounted within a camera body cannot detect a high speed over {fraction (1/8000)} sec. with a good accuracy. A detecting element with a detection accuracy of 10 μs, for example, can detect {fraction (1/8000)} sec., or about 122 μs, but shows an inferior detection accuracy to high shutter speeds faster than {fraction (1/8000)} sec. Moreover, where the detection accuracy of the detection element depends on variations in temperatures, the above-mentioned problem arises. Furthermore, it has been required to consider a display mode in the case of an insufficient detection accuracy. 
     SUMMARY OF THE INVENTION 
     In order to overcome the foregoing problems, an object of the present invention is to provide an improved camera that can inform a photographer of the fact that the detection accuracy of the detecting element is insufficient with respect to the inspection shutter speed, thus dealing with the situation. 
     In order to achieve the objects described above, the camera according to the present invention is characterized by a shutter to limit the exposure time for a record medium; a shutter speed setting unit, hereinafter referred to as setting means, to set, the shutter speed of the shutter a shutter driver and controller, herein referred to as driving and controlling means, for driving and controlling the shutter; a shutter condition detector, hereinafter references as detecting means, to detect the operational condition of the shutter; a manifesting unit to manifest the result detected by the detector; and a memory to store previously inherent data to detect with the shutter condition detecting means. Thee manifesting unit is driven by the shutter condition detecting means, based on the shutter speed set by the shutter speed setting means and inherent data stored in the memory means, and then notifies of the result detected by the shutter condition detecting means. 
     Moreover, according to the present invention, the camera is characterized by a shutter to limit the exposure time for a record medium; a shutter speed setting means for setting the shutter speed of the shutter a shutter driving and controlling means for driving and controlling the shutter; a shutter operation condition detecting means for detecting the operational condition of the shutter condition detecting means; and a display means for displaying the operational time detected by the shutter condition detecting means. 
     According to the present invention, the shutter detection estimation level can be varied in accordance with a set shutter time so that the optimum estimation can be performed corresponding to the detection accuracy of the shutter detection means. Varying the display mode in accordance with the detection accuracy enables a most suitable display even if the detection accuracy is insufficient. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a perspective view showing the camera according to an embodiment of the present invention; 
     FIG. 2 is a block connection diagram showing the camera according to an embodiment of the present invention; 
     FIG. 3 is a perspective view showing a shutter unit used for the camera according to an embodiment of the present invention; 
     FIG. 4 is a cross-sectional view, taken along the line IV—IV, showing the shutter unit according to an embodiment of the present invention; 
     FIG. 5 shows a timing chart for the shutter unit of the camera according to an embodiment of the present invention; 
     FIG. 6 is a flowchart showing a control CPU processing program used for the camera according to an embodiment of the present invention; 
     FIG. 7 is a flowchart showing a control CPU processing program used for the camera according to an embodiment of the present invention; 
     FIG. 8 is a flowchart showing a control CPU processing program used for the camera according to an embodiment of the present invention; 
     FIG. 9 is a flowchart showing a control CPU processing program used for the camera according to an embodiment of the present invention; 
     FIG. 10 shows a timing chart of the shutter used for the camera according to an embodiment of the present invention; 
     FIG. 11 shows a timing chart of the shutter used for the camera according to an embodiment of the present invention; 
     FIG. 12 shows a timing chart of the shutter used for the camera according to an embodiment of the present invention; 
     FIG. 13 is a front view showing an LCD (liquid crystal display) used for the camera according to an embodiment of the present invention, the LCD showing a display example; 
     FIG. 14 is a front view showing an LCD (liquid crystal display) used for the camera according to an embodiment of the present invention, the LCD showing a display example; 
     FIG. 15 is a front view showing an LCD (liquid crystal display) used for the camera according to an embodiment of the present invention, the LCD showing a display example; 
     FIG. 16 is a front view showing an LCD (liquid crystal display) used for the camera according to an embodiment of the present invention, the LCD showing a display example; 
     FIG. 17 is a front view showing an LCD (liquid crystal display) used for the camera according to an embodiment of the present invention, the LCD showing a display example; 
     FIG. 18 is a front view showing an LCD (liquid crystal display) used for the camera according to an embodiment of the present invention, the LCD showing a display example; and 
     FIG. 19 shows a control CPU processing program used for the camera according to an embodiment of the present invention. 
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     An embodiment of the present invention will be explained below with reference to the attached drawings. 
     FIG. 1 is a perspective view showing the camera according to an embodiment of the present invention. 
     FIG. 1 shows the back cover  4  opened. The film cartridge (not shown) is loaded around the cartridge room  5 . The film taken out of the cartridge is wound over the spool  7  across the front surface of the aperture  6 . The pressure plate  9  mounted on the inner side of the back cover  4  presses a film (not shown) against the aperture  6  to keep the flatness thereof. The shutter  8  mounted inside the aperture  6  covers the wider area (shown in broken lines) slightly larger than the aperture  6  and illuminates rays from a subject through the lens  2  onto the film surface for a predetermined period of time. 
     A photographer recognizes visually the condition of a subject passing through the lens  2  through the view finder  3  and depresses the release button  10  to command to start an exposure operation. The exposure mode and various conditions can be ascertained by the display unit  12 . The display unit  12  includes an LCD (liquid crystal diplay)  34  (to be described later). Two set buttons  11  are operational buttons each of which sets arbitrarily the operational mode and various conditions of the camera  1  and is operated over ascertaining characters on the display unit  12 . 
     FIG. 2 is a block connection diagram showing the camera according to an embodiment of the present invention. 
     The present circuit includes a battery  25  acting as a power source. The CPU  32  executes the central control. The CPU  32  receives input signals as follows: 
     The photometric meter unit  26  is a sensor unit that determines the brightness of each portion of a subject by plurally dividing the subject. The plural photometric values are input to the CPU  32 . The film sensitivity detecting unit  27  reads the code signal attached on the side surface of the film cartridge loaded. The information on the film sensitivity is input to the CPU  32 . The switch detecting unit  28  includes the release button  10 , a manually-operating switch including a switch cooperated with the set button  11 , and a timing switch to detect the sequence condition of a camera. The information regarding the condition of a camera is input to the CPU  32 . The temperature sensor  42  detects the temperature of the camera  1  and then input. the temperature information to the CPU  32 . 
     The CPU  32  executes the following drive control through the drive unit  33 . 
     The LCD  34  is driven to display information regarding exposure and an operational mode setting as well as warning information. The shutter  8  (in detail, the operational interval between the leading curtain magnet and the trailing curtain magnet) is controlled to adjust the exposure time. The diaphragm  35  in the lens  2  is driven to control amount of the passing rays. The motor  36  is driven to execute the biasing operation of the shutter drive spring, film winding, film rewinding feeding, charging the mirror and the diaphragm, and the like. Moreover, the CPU  32  controls the shutter-curtain run detecting unit  37 . The LED (light emitting diode)  38  emits light and then the CPU  32  receives the signal from the PTR (photo-transistor)  39 . These will be described later in detail. 
     FIG. 3 is a perspective view showing the shutter  8 . The substrate  13  and the cover plate  14  are arranged substantially in parallel so as to hold a spacing by a shaft member (not shown). A wing room  15  is formed in the spacing. The aperture  13   a  for exposure is formed in the substrate  13  and at the same position as that of the aperture  6  of the camera  1 . An aperture  14   a (not shown) is formed in the cover plate  14  and substantially at the same position as the aperture  6  and aperture  13   a . A shutter mechanism  16  is formed of a drive mechanism including shutter wing springs, a control mechanism with an electromagnet for performing the second control, a charging mechanism for charging the former mechanism, and others. The shutter-curtain run detecting unit  37  is mounted on the substrate  13  and on the opposite side from the shutter mechanism  16  via the aperture  13   a . Moreover, the temperature sensor  42  is mounted on the substrate  13 . 
     FIG. 4 is a cross sectional view of the shutter  8  taken along the line IV—IV shown in FIG.  3 . The front wing group  17  and the rear wing group  21  are arranged in the wing room  15  so as to travel between the position where the opening  13   a  is covered and the position where the opening  13   a  is opened. The LED  38  and the PTR  39  are arranged in the shutter-curtain run detecting units  37 . The front wing group  17  and the rear wing group  21  are detected through the detection opening  13 b opened in the substrate  13  in the front of the shutter-curtain run detecting unit  37 . That is, if the front wing group  17  and the rear wing group  21  exist in the light path, the rays from the LED  38  are reflected by the front wing group  17  and the rear wing group  21  and then enter the PTR  39 . If the front wing group  17  and the rear wing group  21  do not exist in the light path, the PTR  39  does not receive the reflected rays. According to the above-discriminating operation, the front wing group  17  and the rear wing group  21  can be detected. The PTR  39  outputs its signal at light receiving time but does not output it at no light receiving time. 
     In other words, in order to start an exposure, the front wing group  17  shown in FIG. 4, is driven from the position where the opening  13   a  is covered to the position where the opening  13   a  is opened. When the end of the slit forming wing  17   b  of the slit forming wing  17   a  comes to the position of the shutter-curtain run detecting units  37 , the output of the PTR  39  changes from a low level to a high level. In order to terminate the exposure, the rear wing group  21  is driven from the position where the opening  13   a  is opened to the position where the opening  13   a  is covered. Then, the end of the slit forming wing  21   b  of the slit forming wing  21   a  comes to the position of the shutter-curtain run detecting unit  37 , the PTR  39  changes its output from a high level to a low level. 
     FIG. 5 is a timing chart showing the operation of the shutter  8 . 
     FIG. 5 shows the running condition of each curtain that changes and a change in the detection signal from the PTR  39 , in accordance with the on/off operation of the leading curtain and trailing curtain control magnet (Mg). When the release button  10  is depressed, the leading curtain magnet and the trailing curtain magnet are energized on, thus starting the electrical latching of each curtain. In this step, the condition mechanically-latched before depressing the release button  10  is switched. 
     Thereafter, in normal photographing, the mechanism (not shown) controls the diaphragm of the lens  2  and elevates the reflecting mirror in the photographing optical path. Next when the leading curtain magnet is turned off, the slit forming wing  17   b  of the slit forming wing  17   a  in the front wing group  17  travels as shown with the running curve  40 . The range shown with F shows the vertical opening of the aperture  6 . After a lapse of time tf when the leading curtain magnet has been turned off, the slit forming wing  17   b  of the front wing group  17  passes by the front surface of the shutter-curtain run detecting unit  37  so that the output of the PTR  39  is inverted from a high level to a low level. 
     When the leading curtain magnet has been turned off, the trailing curtain magnet is turned off after a lapse of a predetermined time T, or of a predetermined exposure time. This process allows the slit forming wing  21   b  of the slit forming wing  21   a  of the trailing wing group  21  to cross the opening F as shown with the running curve  41 . At this time, when the trailing curtain magnet is turned off, the slit forming wing  21   b  of the rear wing group  21  passes by the front surface of the shutter-curtain run detecting unit  37  after a lapse of time tr so that the output of the PTR  39  is inverted from a high level to a low level. 
     As described above, an actual exposure time t can be recognized by measuring the period between the rise time to the falling time in the reversing time of the PTR  39 . 
     Even if the exposure control circuit, for example, measures correctly the exposure time T and drives the leading and trailing curtain magnets with the normal timing, when the control time t obtained via the PTR  39  is different with the exposure time T, it can be decided that an erroneous operation has occurred in the mechanical system. 
     Furthermore, the running time (curtain speed) of each curtain can be known by measuring the time tf and the time tr. When the shutter operates normally, the time tf and the time tr represents a standard value determined in design, respectively. When the time tf and the time tr are longer than the standard values, respectively, it is decided that the curtain speed is slow. When the time tf and the time tr are shorter than the standard values, respectively, it is decided that the curtain speed is fast. Hence it can be decided that there is an exposure unevenness. 
     FIG. 6 is a flow chart showing the process routine of the CPU  32  shown in FIG.  2 . This routine is repeated during feeding electric energy. Now, for explanation, it is assumed that the camera according to the present invention has the maximum shutter speed of {fraction (1/8000)} sec. (=122 μs), and time tf is a standard time (design value) of 3.0 μs, and time tr is a standard time (design time) of 3.0 μs. However, it is apparent that other design values can be adopted. 
     In the step S 1 , the photometric meter unit  26  inputs a photometric signal and the sensitivity detecting unit  27  inputs a sensitivity signal. In the step S 2 , the two signals are subjected to an arithmetic operation and then the shutter time in seconds and the diaphragm stop are calculated. In the step S 3 , the above-exposure conditions are dislayed on the LCD  34 . 
     In the step S 4 , it is decided whether the release button  10  has been depressed through the switch detecting unit  28 . When the release button  10  is not depressed, the flow returns to the step S 1  to repeat the above procedure. In the step S 4 , when the release button has been depressed, the leading and trailing curtain magnets, as described with respect to FIG. 5, are first turned on (step S 5 ). In the step S 6 , the reflecting mirror (not shown) is flipped up to be withdrawn from the optical path. In the step S 7 , the diaphragm  35  is controlled to be opened to a predetermined opening size. In the step S 8 , the shutter routine in which the exposure of the film is controlled by opening and closing the shutter  8 , and the routine in which the shutter-curtain run detecting unit  37  detects the condition of the shutter-curtain run are executed. The shutter-curtain run detecting routine will be explained in detail with reference to FIGS. 7 and 8. 
     In the step S 9 , the second data detected by the shutter-curtain run detecting unit  37  is evaluated. The second data estimating routine is explained in detail with reference to FIG.  9 . In the step  10 , after a completion of the exposure operation, the motor  36  is rotated positively to charge the mechanism and to take up the spool of film. Then the flow goes back to the step S 1 . 
     FIGS. 7 and 8 are a flow chart showing in detail the shutter-curtain run condition detecting routine (step S 8 ), respectively. 
     In the step S 11 , the shutter speed T in seconds set in the step S 2  is read out. In the step S 12 , feeding electric energy to the leading curtain magnet is terminated and then the front wing group  17  starts running. Thereafter, steps following the steps  13  and  17  are performed simultaneously. For easy explanation, the shutter speed T in seconds sufficiently longer than the running time of each wing group has been shown in the present embodiment. However, it can be considered in accordance with the present flow chart that the shutter speed T in seconds is shorter than the running time of each wing group. 
     In the step S 13 , measuring the shutter speed T in seconds starts. A completion of the measurement of the shutter speed T in second is awaited in the step S 14 . In the step S 15 , activating the trailing curtain magnet is completed after a lapse of the shutter time T in seconds, and then the run of the rear wing group  21  is started. In the step S 16 , measuring the count time tr is started while the tr timer is operated. In the step S 17 , as in the step  13 , measuring the count time tf is started while the tf timer is operated. In the step S 18 , the LED  38  emits light. In the step S 19 , if the passage of the slit forming wing  17   a  of the front wing group  17  causes an inverted signal output from the PTR  39 , the flow goes to the step S 20 . If the output is not inverted, the flow goes to the step S 26 . In the step S 20 , it is completed to measure the count time tf. In the step S 21 , it is started to measure the count time t. 
     In the step S 22  (FIG.  8 ), if the output of the PTR  39  is inverted because of the passage of the slit forming wing  21   a  of the rear wing group  21 , the flow goes to the step S 23 . If not inverted, the flow goes to the step S 28 . In the step S 24 , measuring the count time tr has been completed. In the step S 25 , the LED  38  is turned off after the completion of the measurement and then the flow goes back to the step S 9  in FIG.  6 . In the step S 26  (FIG.  7 ), it is decided whether the tf timer has counted a count time exceeding a predetermined period of time (preferably, a time suitably longer than the time tf of the standard value 3 ms, for example, 10 ms). If the count time does not exceed the predetermined value, the flow goes back to the step S 19 . If the time exceeds the predetermined value, the flow goes to the step S 27  in FIG.  8 . In the step S 27 , it is decided that an abnormal condition has occurred because the tr timer has counted a count time over a predetermined value (10 ms) (abnormal condition  1 ). At this time, the processes following the step S 16  advancing simultaneously from the step S 13  are interrupted. Then the flow goes to the step S 25 . 
     In the step S 28 , it is decided whether the tr timer has counted a count time exceeding a predetermined value (preferably, a time tr suitably longer than the standard value 3 ms, for example, 10 ms). If the count time does not exceed the predetermined value, the flow goes to the step S 22 . If the count time exceeds the predetermined value, the flow goes to the step S 29 . Now, in the step S 29 , it is decided that an abnormal condition has occurred because the tr timer has counted a count time over a predetermined value (10 ms) (abnormal condition  2 ). Then the flow goes to the step S 25 . 
     FIG. 9 is a flow chart showing in detail the routine evaluating data regarding the second data estimating routine as shown in FIG. 6 (step S 9 ). 
     In the step S 30 , it is decided whether the step S 27  in FIG. 8 was in the abnormal condition  1 . If in the abnormal condition  1 , the flow goes to the step S 33  and if not in the abnormal condition  1 , the flow goes to the step S 31 . In the step S 31 , it is decided whether the step S 29  in FIG. 8 was in the abnormal condition  2 . If in the abnormal condition  2 , the flow goes to the step S 34  and if not in the abnormal condition  2 , the flow goes to the step S 32 . In the step S 32 , it is decided whether the shutter speed T in seconds set in the step S 2  (FIG. 6) is {fraction (1/8000)} sec. (the maximum shutter speed). If {fraction (1/8000)} sec., the flow goes to the step S 35  and if not, the flow goes to the step S 36 . 
     In the step S 33 , because the step S 30  decided to be the abnormal condition  1 , the LCD  34  displays the corresponding indication (warning display). In the step S 34 , because the step S 31  decided to be the abnormal condition  2 , the LCD  34  displays the corresponding indication (warning display). In the step S 35 , since the situation is not the abnormal condition  1  or  2  but the shutter speed is set to {fraction (1/8000)} sec., the LCD display unit  34  displays the time t, time tf and time tr. In the step S 36 , since the situation is not the abnormal condition  1  or  2  and the shutter speed is not set to {fraction (1/8000)} sec., the LCD  34  displays the time t, time tf and time tr. 
     The time chart for a normally-operating shutter is shown in FIG.  5 . Here because the shutter is malfunctioning, the-main aspects will be explained in detail using the time chart. 
     (1) Malfunction of the Leading Curtain (Refer to the Time Chart in FIG.  10 ): 
     In this abnormal condition, the leading-curtain magnet remains on state because of its operational failure (as shown in FIG.  10 ). In this case, since the front wing group  17  does not run, the exposure operation is not performed. Since the shutter-curtain run detecting unit  37  is kept to be covered by the front wing group  17 , the output of the PTR  39  is in a low level. Referring to FIG. 10, both the trailing-curtain magnet and the rear wing group  21  operate normally. However, even if these elements are in an abnormal condition, the PTR  39  produces no output. Hence the time t, time tf, and time tr cannot be detected, as shown in FIG.  10 . 
     The abnormal condition includes, for example, the case where an electrical failure does not release the electrical attraction of the leading-curtain magnet and keeps the leading-curtain magnet in operational failure, thus paralyzing the run of the front wing group  17 ; the case where a mechanical failure stops an operation of the leading-curtain magnet, thus paralyzing the run of the front wing group  17 ; and the case where the failure of the front wing group  17  alone paralyzes its running. With the shutter speed in seconds for example set near to the maximum high speed in second, even if the leading and trailing curtain magnets and the front and rear wing groups  17  and  21  operate normally, the slight shift between the operational timings may cause the operational timings of the front wing group  17  and the rear wing group  21  to be inverted. The reason is that the time difference each between the operational timing of the leading-curtain magnet and the operational timing of the trailing-curtain magnet and between the running timing of the front wing group  17  and the running timing of the rear wing group  21  is very small. In this case, since either the front wing group  17  or the rear wing group  21  covers always the opening F and the shutter-curtain run detecting unit  37 , the exposure operation is not performed while the PTR  39  does not produce its output. 
     (2) Malfunction of the Trailing Curtain (Refer to the Time Chart in FIG.  11 ): 
     In this abnormal condition, for example, the trailing-curtain magnet remains in the on state because of its operational failure, as shown in FIG.  11 . In this case, since the rear wing group  21  does not run, the opening F is kept open. Moreover, since the rear wing group  21  does not cover the shutter-curtain run detecting unit  37 , the output of the PTR  39  is in a high level. 
     Therefore the time tf can be detected but the time t and time tr cannot be detected. This abnormal condition includes the case where since the electrical attraction of the trailing-curtain magnet is not released due to an electrical failure (or the trailing-curtain magnet does not operate), the rear wing group  21  does not run; the case where a mechanical failure causes a malfunction of the trailing-curtain magnet so that the rear wing group does not run; and the case where the rear wing group  21  alone does not run due to its operational failure. 
     (3) Erroneous Timing in Exposure Operation (Refer to the Time Chart in FIG.  12 ): 
     FIG. 12 shows the example where the operational timing of the trailing-curtain magnet is delayed by ΔT, or the running curve  41  of the trailing curtain is shifted behind by ΔT. In this case, since the exposure operation has been performed, the PTR  39  produces its output so that the time t, time tf and time tr can be detected. FIG. 12 shows the case where the timing is delayed on the running curve of the trailing curtain. Such a shift in timing is caused due to the case where the timing of the running curve  41  of the trailing curtain advances more, the case where the timing of the running curve  40  of the leading curtain becomes slower or faster; or the case where the timings of the leading curtain and the trailing curtain are shifted to each other. 
     With the slow timing of running curve  40  of the leading curtain or/and the fast timing of the running curve  41  of the trailing curtain, and the shift in timing larger than the shutter time T in seconds even if the shutter is operated as the operational failure of the leading curtain described in the item (1), the operational timings of the front wing group  17  and the rear wing group  21  are inverted so that the PTR  39  does not produce its output because no exposure operation has occurred. Hence in consideration of the output of the PTR  39 , the above-described operation is similar to that according to the time chart shown in FIG.  10 . 
     FIGS. 13 to  17  show the contents displayed on the LCD  34  regarding part of the shutter information. The LCD  34  displays four kinds of information: t he display  34  of set time in seconds, the display  34   b  of count time t and the display  34   c  of time tf, and the display  34   d  of time tr. 
     Explanation will be made next as for the case where the front wing group  17  and the rear wing group  21  operate according to the timing charts shown in FIG.  5  and FIGS. 10 and 12, as well as the case where the shutter operates according to the timing charts shown in FIGS. 7 and 8. The evaluative operation also will be explained corresponding to the flow chart shown in FIG.  9 . First, the case where the shutter speed T is set to a value in seconds (e.g. {fraction (1/1000)} sec.) except the maximum speed in second. will be explained. Next the case where the shutter speed T is set to the maximum speed in seconds (e.g. {fraction (1/8000)} sec.) will be explained. 
     1. Shutter Speed Set to {fraction (1/1000)} Sec.: 
     (1) Normal Operation (Refer to the Time Chart in FIG.  5 ): 
     In the step S 11 , the shutter speed T in second at {fraction (1/1000)} sec. is read out. In the step S 12 , the leading curtain magnet is turned off and then the front wing group  17  starts its running. In the step S 13 , the measurement of the shutter time T in second is started. After a lapse of T={fraction (1/1000)} sec. in the step S 14 , the flow goes to the step S 15 . Then the trailing curtain magnet is turned off and the rear wing  21  starts its running. In the step S 12 , measuring the time tr is stated. 
     On the other hand, immediately after the leading-curtain magnet is turned off in the step S 12 , the measurement of the time tf is started in the step S 17 . The LED  38  of the shutter-curtain run detecting means  37  emits light in the step S 18 . In the step S 19 , the flow waits for the inversion (rise-up) of the output of the PTR  39 . A rise-up is obtained because of the normal operation of the shutter. The flow goes to the step S 20  and then the time tf is completely measured. Hence data on the time tf (in this normal case, 3 ms) can be obtained. 
     Next, measuring the time t is started in the step S 21 . The inversion (falling) of the output from the PTR  39  is waited for in the step S 22 . Since the shutter is in a normal operation, the output rises up. Hence measuring the time t is completed in the step S 23  and measuring the time tr is completed in the step S 24 . Hence data regarding the time t ({fraction (1/1000)} sec.) as well as data regarding the time tr (3 ms) can be obtained. Thereafter, the LED  38  is turned off in the step S 25 . 
     In succession, the evaluative operation will be explained below with reference to the flow chart shown in FIG.  9 . 
     Because of the normal operation, through the steps S 30  and S 31 , the set time T in seconds is decided in the step S 32 . Since the shutter speed is now set to {fraction (1/1000)} sec., the flow goes to the step S 36  and then the resultant data is displayed on the LCD  34 . FIG. 13 shows the display example. The set second display  34   a  displays the set time of {fraction (1/1000)} sec., the count time display  34   b  displays {fraction (1/1000)} sec., the tf display  34   c  displays 3.0 ms, and the tr display  34   d  displays 3.0 ms. 
     (2) Malfunction of the Leading Curtain (Refer to the Time Chart in FIG.  10 ): 
     The steps S 11  to S 18  are similar to the steps in the normal operation. However, in the step S 19 , as shown with the time chart in FIG. 10, since the PTR  39  does not produce its inverted (rise-up) output due to the front wing group  17 , the flow does not go to the step S 20 . After a lapse of the set time (10 ms) set by the tf timer in the step S 26 , the flow goes to the step S 27 . Immediately after it is decided that the system is in the abnormal condition  1 , the steps following the step S 16  and advancing at the same time from the step S 13  are interrupted. Hence data regarding the time t, tf, and tr cannot be obtained. Thereafter, the LED  38  is turned off in the step S 25 . 
     Next, an evaluative operation will be explained with the flow chart shown in FIG.  9 . 
     Because of the abnormal condition  1 , the flow goes from the step S 30  to the step S 31 . The LCD  34  displays the abnormal condition  1 . FIG. 14 shows the display example. The set time in second display  34   a  displays a set second (e.g. {fraction (1/1000)} sec.). The time t, tf and tr cannot be detected and displayed. However, in order to display the abnormal condition  1 , the count time display  34   b  displays, for example, “shutter closed” as shown in FIG.  14 . 
     (3) Malfunction of the Trailing Curtain: 
     The step S 11  to S 21  are similar to the steps in the normal operation. As shown with the time chart in the step S 22  shown in FIG. 11, the rear wing group  21  does not allow the output of the PTR  39  to be inverted (risen up), the flow does not go to the step S 23 . After the tr timer operates for a set time (10 ms) in the step S 28 , the flow goes to the step S 29 , so that it is decided that the system is in the abnormal condition  2 . Thereafter, the flow goes to the step S 25  and then the LED  38  is turned off. Hence data on the time tf can be obtained but data on the time t and tr cannot be obtained. 
     Next, explanation will be made as for the evaluative operation in accordance with the flow chart shown in FIG.  9 . 
     Because of the abnormal condition  2 , the flow goes from the step S 30  to the step S 31  and then the LCD  34  displays the abnormal condition  2  in the step S 34 . FIG. 15 shows the display example. The second display  34   a  displays a set seconds ({fraction (1/1000)} sec.) and the time tf display  34   c  displays a detected time (3 ms). Since the time t and tr cannot be detected, they are not being displayed. The count time display  34   b  displays, for example, “shutter closed”. 
     (4) Erroneous Timing in Exposure Operation (Refer to the Time Chart in FIG.  12 ): 
     Since the exposure operation is performed, the operations in accordance with the flow charts shown in FIGS. 7 and 8 are similar to the item (1) normal operation, but data on a different time can be obtained. According to the present embodiment, it is assumed that the operational timing of the rear wing group  21  is delayed by ΔT (=0.1 ms). Hence the resultant time data includes t={fraction (1/928)}, tf=3 ms and tr=3.1 ms. The evaluative operation in accordance with the flow chart shown in FIG. 9 is similar to that in the normal operation. However, the resultant time data, as described above, is displayed on the LCD  34 , as shown in FIG.  16 . 
     2. Maximum Shutter Speed Set to {fraction (1/8000)} sec.: 
     (1) Normal Operation: Time Chart in FIG.  5 : 
     The shutter operation in accordance with the flow chart shown in FIGS. 7 and 8 is similar to the normal operation in which the set time is {fraction (1/1000)} sec. In the evaluative operation of the flow chart shown in FIG. 9, since T={fraction (1/8000)} sec. in the step S 32 , the flow goes to the step S 35 . Similarly, the LCD  34  displays the corresponding data. However, since the detection accuracy of the shutter-curtain run detecting unit  37  is insufficient to the maximum speed of {fraction (1/8000)} sec, it is meaningless to display the data t regarding the detected second without any change. For that reason, when the shutter speed is set to the maximum speed in seconds, the levels of the detection and the decision are lowered to a small value to decide whether the shutter has been opened (or an exposure operation has been performed), and then the resultant data is displayed. When the shutter in open (exposure operation completed) is detected, the count time display  34   b , as shown in FIG. 17, displays “shutter opened” as second data “t”. When the shutter is not opened, the situation is treated as the abnormal condition  1  to be described below. 
     (2) Malfunction of the Trailing Curtain (Refer to the Time Chart in FIG.  10 ): 
     This situation resembles the case where the leading curtain has been failed in the operation at the set time of {fraction (1/1000)} sec. and is decided as the abnormal condition  1 . The LCD  34  displays as the case shown in FIG. 14, (but the set second display  34   a  displays {fraction (1/8000)} sec.). 
     (3) Malfunction of the Trailing Curtain: 
     This case corresponds to the operational failure of the trailing curtain set to a shutter time of {fraction (1/1000 )}sec. and is decided as the abnormal condition  2 . The LCD  34  displays data as shown in FIG. 15 (in this case, the set shutter speed display  34   a  displays {fraction (1/8000)} sec. and the tf display  34   c  displays data regarding tf). 
     (4) Erroneous Timing in Exposure Operation (Refer to the Time Chart in FIG.  12 ): 
     This case corresponds to the normal operation at the set shutter speed of {fraction (1/8000)} sec. The LCD  34  displays data as shown in FIG.  17 . 
     As described above, the shutter speed is varied from the maximum value to other values in accordance with the shutter speed detection level and the decision level. Where the shutter-curtain run detecting means  37  has a worse detection accuracy, the levels of the shutter speed detection and the decision can be lowered in accordance with the detection accuracy to set them to an arbitrary value. That is, the levels of the shutter speed detection and the decision can be varied in the lower shutter speed range (e.g. {fraction (1/4000)} sec.). In this case, it is decided whether T≦{fraction (1/4000)} sec. in the step S 32  shown in FIG.  9 . If so, the flow goes to the step S 35 . If not so, the flow goes to the step S 36 . When a sufficient accuracy is obtained over all shutter speed ranges, it is possible to remove the steps S 32  and S 35 . 
     FIG. 18 shows the example that the LCD  34  displays another information. The second error display  34   c  is used instead of the count time display  34   b . The tf error display  34   f  is used instead of the tf display  34   c . The tr error display  34   g  is used instead of the tr display  34   d . Each display shows an error shifted from the standard value. The values calculated according to the following formulas are displayed: 
     
       
         Error in seconds=log 2  (t/T) 
       
     
     
       
         tf error=tf (count value)−tf(standard value) 
       
     
     
       
         tr error=tr (count value)−tr (standard value) 
       
     
     FIG. 18 shows data obtained converting data displayed as shown in FIG. 16 using the above formulas. The error in second-may be displayed as (t−T) without displaying logarithmically. As described above, various displaying modes can be selected. 
     FIG. 19 shows another example of the evaluative routine. In the evaluative routine, the detection level at a high shutter speed is varied as the detection accuracy of the shutter-curtain run detecting unit  37  varies with temperature. For example, the evaluative routine is showed to the example where the detection accuracy of the shutter-curtain run detecting unit  37  becomes worse as the temperature drops. The temperature sensor  42  can detect the temperature. In concrete, FIG. 19 shows the case where the detection accuracy of {fraction (1/8000)} sec. is insufficient over temperatures of more than zero ° C. and more; the case where the detection accuracy at a high shutter speed of {fraction (1/4000)} sec. is insufficient over temperatures ranging less than 0° C. to more than −10° C.; and the case where the detection accuracy at a high shutter speed of less than {fraction (1/2000)} sec. is insufficient over temperatures of less than −10° C. In FIG. 19, the steps S 37  and S 38  for detecting temperatures as well as the steps S 39  and S 40  for deciding a set shutter speed T are added to the routine shown in FIG.  9 . Other steps corresponds to the remaining steps shown in FIG.  9 . Hence, the abnormal conditions  1  and  2  are dealt within the same process as that shown in FIG.  9 . When the system is not in the abnormal conditions  1  and  2 , the temperature decision is done in the step S 37 . The flow goes to the step S 32  at 0° C. and more. The flow goes to the step S 38  at less than 0° C. The temperature decision is repeated again in the step S 38 . Then the flow goes to the step S 39  at −10° C. or more. If the temperature is less than −10° C., the flow goes to the step S 40 . Hence, when the temperature is more than 0° C., the flow goes to the step S 32 . When the temperature is less than 0° C. or more than 10° C., the flow goes to the step S 39 . When the temperature is less than −10° C., the flow goes to the step S 40 . The set shutter speed T is decided in each of the steps S 32 , S 39  and S 40 . If the set shutter speed T is set to {fraction (1/8000)} sec. in the step S 32 , the set shutter speed T is set to a high speed of less than {fraction (1/4000)} sec. in the step S 39 , or the set shutter speed T is set to a high speed of less than {fraction (1/2000)} sec. in the step S 40 , the flow goes to the step S 35 . Thus data is displayed on the display unit  34  as shown in FIG.  17 . If the above conditions are not set, the flow goes to the step S 36 . Then data are displayed on the display unit  34  in accordance with the set time or the detection result, as shown any one of FIGS. 13,  16  and  18 . The detection level can be varied in accordance with the shutter speed. For example, T={fraction (1/8000)} sec. when the temperature is more than 0° C., T={fraction (1/4000)} sec. when the temperature ranges from less than 0° C. to more than −10° C., and T={fraction (1/2000)} sec. when the temperature is less than −10° C. 
     The above-mentioned configuration can vary the accuracy level for shutter time detection in accordance with temperature. The combination of temperature and detected time in second is an example. The accuracy level can be arbitrarily set in accordance with the detection accuracy with respect to the temperature of the shutter-curtain run detecting units  37 . 
     As described above, according to the present embodiment, the camera with the shutter speed detecting means can evaluate the operation of the shutter and also can display the resultant data. The camera also can detect various abnormal conditions and also can display the resultant data. Furthermore, since the decision level of the shutter speed for inspection can be set to a desired value, an optimum inspection can be performed in accordance with the detection accuracy of the shutter-curtain run detecting means. Furthermore it is possible to consider a change in temperature of the detection accuracy of the shutter-curtain run detecting means. Since various display modes can be set, an optimum display mode can be select to meet the use purpose of a camera. 
     As described above, according to the present invention, the notification control means drives the shutter condition detecting means, based on both the shutter speed set by means of the shutter speed setting means and inherent data stored in memory means to inform a photographer of the result detected by the shutter condition detecting means. Hence even if the detection accuracy of the detecting element is insufficient for the inspection shutter speed in seconds, a precise display can be provided to the photographer.