Supersonic flaw detecting system

• US 4,768,155 A
• Filed: 01/21/1986
• Issued: 08/30/1988
• Est. Priority Date: 01/19/1985
• Status: Expired due to Term

• Current Assignee: Hitachi Construction Machinery Company Limited (Hitachi, Ltd.)
• Original Assignee: Hitachi Construction Machinery Company Limited (Hitachi, Ltd.)
• Inventors: Takishita, Yoshihiko, Hayakawa, Yasuo, Nonaka, Toshio
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): MELNICK, STEVEN A
• Application Number:
  US06/820,607
• Time in Patent Office: 952 Days
• Field of Search: 364/507, 364/508, 364/506, 364/552, 364/490, 364/525, 364/414, 73/620, 73/632, 73/633, 73/634, 73/607, 73/618, 73/621, 340/731, 128/660, 358/112
• US Class Current: 702/39
• CPC Class Codes: B82Y 15/00 Nanotechnology for interacting, sensing or actuating, e.g. quantum dots as markers in protein assays or molecular motors
• CPC Class Codes: G01N 2291/02854 Length, thickness
• CPC Class Codes: G01N 29/0609 Display arrangements, e.g. colour displays indicating or recording in connection with measuring in general G01D
• CPC Class Codes: G01N 29/0627 Cathode-ray tube displays in general G01R13/20
• CPC Class Codes: G01N 29/0645 Display representation or displayed parameters, e.g. A-, B- or C-Scan
• CPC Class Codes: G01N 29/22 Details , e.g. general constructional or apparatus details

Abstract

A supersonic flaw detecting system has a probe adapted to emit a supersonic wave towards an object to be inspected, a scanning device for causing a relative movement between the probe and the object in two orthogonal directions, a pulser-receiver adapted to supply pulses to the probe and receive the supersonic wave from the object and produce an electric signal indicative thereof, a signal processing device for converting the electric signal from the pulser-receiver into an image data signal for a C-scope display, an oscilloscope for conducting an A-scope display of the electric signal from the pulser-receiver, and a monitor T.V. having a screen for conducting the C-scope display of the image data signal from the signal processing device. A control unit when the probe and object are relatively moved by the scanning device, the image data carried by the image data signal from the signal processing device at a corresponding address in the image memory at each pitch which has been determined such that the number of data pickups during the relative movement between the probe and the object coincides with the number of the corresponding addresses in the image memory to thereby cause C-scope display of the image data to be effected on the screen. The is operative to compute, when the cursor is displayed on the screen by the operation device, the amount of operation of the scanning device necessary for locating the probe relative to the object at a position corresponding to the cursor on the screen and operate the scanning device by the thus computed amount to locate the probe at the corresponding position, thereby permitting A-scope display to be effected at such a position on the oscilloscope.

Claims

1. A supersonic flaw detecting system having a probe that emits a supersonic wave towards an object to be inspected, scanning means for causing a relative movement between said probe and said object in two orthogonal directions, a pulser-receiver that supplys pulses to said probe and receive the supersonic wave from said object and produce an electric signal indicative thereof, signal processing means for converting said electric signal from said pulser-receiver into an image data signal for a C-scope display, oscilloscope means for conducting an A-scope display of said electric signal from said pulser-receiver, and a monitor T.V. having a screen for displaying the C-scope display of said image data signal from said signal processing means, said supersonic flaw detector further comprising:

image memory means connected to said monitor T.V. and having addresses corresponding to the coordinate values of a coordinate system assumed on the screen of said monitor T.V.;

operation means for being operated by an operator and including position indicating means for allowing the operator to designate a desired position on the screen of said monitor T.V.; and

control means connected to said scanning means, said signal processing means, said image memory means and said operation means, and including;

first means for writing, when said probe and object are relatively moved by said scanning means, the image data carried by said image data signal from said signal processing means in the image memory means at a corresponding address thereof at each pitch determined such that the number of data pickups during the relative movement between said probe and object coincides with the number of the corresponding addresses in said image memory means, to thereby provide data for C-scope display of the image data to be produced on the screen of said monitor T.V.;

second means for allowing access to one of the addresses in said image memory means corresponding to said desired position on the screen designated by operation of said position indicating means, and

third means for computing, when said one of the addresses in said image memory means is accessed by the operation of said position indicating means, the amount of drive of said scanning means necessary for moving said probe relative to said object to a position corresponding to the designated position on the screen of the monitor T.V. from data on said pitch and said accessed address in said image memory means and driving said scanning means until said computed amount of drive is reached whereby said probe is automatically moved to and located at said position corresponding to the designated position on the screen of said monitor T.V. for allowing A-scope display at such a position to be successively followed.

2. A supersonic flaw detecting system according to claim 1, wherein said control means further provides the function of allowing the scanning range of said probe relative to said to be set by an operation of said operation means and stores beforehand a number of data pickups which coincides with the number of the corresponding addresses in said image memory means for computing said pitch from said number of data pickups and said scanning range as set.

3. A supersonic flaw detecting system according to claim 2, wherein said control means further function to compute, when the relative movement between said probe and said object caused by said scanning means is completed, the amount of drive of said scanning means necessary for returning said probe to an initial position for the probe, from said pitch and the address in said image memory means in which the last image data has been written, and driving said scanning means until the thus computed amount of drive is reached whereby said probe is automatically returned to said initial position.

4. A supersonic flaw detecting system according to any one of claims 1, 2 and 3, further comprising data pickup timing means connected to said scanning means, control means and said signal processing means for instructing said signal processing means to output said image data signal at the timing of each said pitch.

5. A supersonic flaw detecting system according to claim 4, wherein said scanning means includes a first motor and a second motor for effecting the relative movement in one and the other of two orthogonal directions, respectively, and a first encoder and a second encoder connected to said first motor and said second motor, respectively, for producing pulse signals of the same pulse width in proportion in number to the amounts of rotation of the respective motors;

said data pickup timing means includes a frequency divider connected between said first encoder and said signal processing means for demultiplying said pulse signals from said first encoder and delivering trigger signals to said signal processing means at timings obtained as a result of the demultiplication; and

said control means further functions to divide said pitch by the pulse width of said pulse signal from first encoder to compute a number of demultiplication, and instructs said frequency divider to effect the demultiplication by the thus computed number.

6. A supersonic flaw detecting system according to claim 5, wherein said control means further functions to divide X direction distance of the set scanning range by the pulse width of said encoder pulse signal to compute a number of pulses of said first encoder necessary for effecting the relative movement by said set distance in X direction and driving said first motor until said pulse number is counted;

for dividing Y direction distance of the set scanning range by said pitch to compute a data sample number necessary for covering the Y direction distance of said set scanning range and driving said first motor such that the relative movements in the X direction and in the -X direction are alternatingly repeated until said data sample number is counted; and

for driving, each time the relative movement in the X or the -X direction is completed, said second motor to effect the relative movement in the Y direction until the number of the encoder pulses coinciding with the number of demultiplication are counted, and thereafter initiating the next movement in the -X or the X direction.

7. A supersonic flaw detecting system according to claim 5, wherein said third means in said control means is programmed to multiply the X coordinate value and the Y coordinate value of the address in said image memory means set by said position indicating means with said number of demultiplication to compute numbers of pulses to be provided to said first and second encoders necessary for locating said probe at the position corresponding to the position of said position indicating means on the T.V. screen to thereby determine the amount of drive of said scanning means necessary for automatically locating said probe at said last-mentioned position for said A-scope display.

8. A supersonic flaw detecting system according to claim 5, wherein said control means multiplies the X coordinate value and the Y coordinate value of said address in said image memory means in which the last image data is written with said number of demultiplication to compute the numbers of pulses of said first and second encoders necessary for returning said probe to said initial position to thereby determine the amount of drive of said scanning means necessary for automatically returning said probe to said initial position.