US3803474A - Detection of blemishes on surfaces - Google Patents

Detection of blemishes on surfaces Download PDF

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Publication number
US3803474A
US3803474A US00309719A US30971972A US3803474A US 3803474 A US3803474 A US 3803474A US 00309719 A US00309719 A US 00309719A US 30971972 A US30971972 A US 30971972A US 3803474 A US3803474 A US 3803474A
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pulse
signal
produce
fault
circuit arrangement
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G Clarke
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Ferranti International PLC
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Ferranti PLC
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Priority to US00309719A priority patent/US3803474A/en
Priority to DE2258158A priority patent/DE2258158C3/de
Priority to FR7242397A priority patent/FR2163148A5/fr
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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/84—Systems specially adapted for particular applications
    • G01N21/88—Investigating the presence of flaws or contamination
    • G01N21/89—Investigating the presence of flaws or contamination in moving material, e.g. running paper or textiles

Definitions

  • ABSTRACT A circuit arrangement for use with a detector of faults in a moving surface, the detector comprising a source of a beam of light caused to scan repetitively across the surface transversely to its direction of motion and detection means to collect light emanating from the surface to produce, in response to a change in the radiation collected, a fault signal.
  • the circuit arrangement comprises means for generating an edge slot" pulse which coincides with the engagement of the beam and the surface. The duration of the edge-slot pulse is chosen to ensure its existence at any engagement time allowing for unpredictable but limited movements of the edge of the surface.
  • Fault counting is delayed until the edge of the surface (characterised as the first fault detected) is engaged by the beam during the presence of the edge slot pulse. This ensures that any signal received prior to the edge slot does not begin fault counting.
  • the circuit may be modified to incorporate controls for the repositioning of the surface if it is engaged by the beam not during the presence of the edge slot pulse.
  • This invention relates to the detection of faults on surfaces and in particular to circuit arrangements associated with such detection.
  • Detectors of faults are widely used in relation to moving strip-like surfaces such as those of paper webs, plastics material and steel.
  • the particular type of detector with which this invention is concerned comprises a source of a beam of optical radiation, means to scan the beam repetitively across the surface transversely to the direction of motion of the surface and detection means to collect optical radiation emanating from the surface and to produce, in response to a change in the radiation collected, a fault signal.
  • a detector of faults will hereinafter be referred to as being of the type stated.
  • optical radiation and light are intended to include electromagnetic radiation of the visible, infra-red and ultra-violet parts of the spectrum.
  • This form of detector is adequate if the beam scans the surface exactly from edge to edge. However, it is unlikely that the surface will always be of sufficient width to completely fill the scan so that it is necessary to arrange means whereby any signals derived from reflections of the beam from the background and from the edge of the surface are not interpreted as faults.
  • a typical solution has been to position a photo-diode such that it is crossed by the beam just as the beam is about to engage the surface; the photo-diode is used in a gate circuit to activate a counter of faults detected in the detection means for a predetermined period, that is, for the time taken for the beam to scan over the surface, so that only faults on the surface are counted.
  • a circuit arrangement for use with a detector of the type stated includes sensing means'operable to detect the passage of the beam past a point to produce, in each scan, a timing reference signal, primary pulse means responsive to the timing reference signal to generate a primary pulse extending from some time before the beam engages a known discontinuity in the radiation absorbing properties of the surface until sometime after the engagement, timing means responsive to the occurrence of a fault signal greater than a predetermined threshold value during the presence of the primary pulse to produce a counter enabling signal, and acounter, enabled by the counter enabling signal, to count subsequent fault signals.
  • the circuit arrangement may also include secondary pulse means responsive to the timing reference signal for providing a plurality of secondary pulses, at least one immediately preceding and at least one immediately succeeding the primary pulse, switching'means responsive to a fault signal greater than said predetermined threshold value'during the presence of a secondary pulse to produce a servo error signal, and servo control means responsive to said servo error signal to cause the surface to be moved substantially parallel to the line of scan of the beam until said fault signal is detected during the presence of the primary pulse.
  • a detector of the type stated includes a circuit arrangement as defined in one or both of the two preceding paragraphs.
  • FIG. 2(a) illustrates the angular position of the scanning beam at various times into the scan
  • FIG. 2(b) shows waveforms of signals at various points in the circuit of FIG. 1 in relation to the time scale of FIG. 2(a),
  • FIG. 3 is a modified form of the edge detection circuitry of FIG. 1,
  • FIGS. 4(a) and 4(b) correspond the FIGS. 2(a) and (b) but relate to FIG. 3,
  • FIG. 5 shows a modified form of scanning arrangement
  • FIG. 6 shows an alternative form of part of the circuit arrangement of FIG. 3.
  • the part 10 of the Figure shows a section of a continuous web 11 of paper or other material which is caused to move continuously over a roller 12 in a direction perpendicular to the plane of the drawing.
  • a detector of faults includes a scanning station 13, mounted over the web as it crosses the roller 12, and containing a source of a beam of optical radiation 14, a multi-faceted mirror 15 and a photomultiplier detection means 16.
  • Optical radiation, or light, from the source 14- is emitted in a beam such that after reflection at a facet of the mirror, the beam converges to illuminate a small area on the roller 12 or on the surface of the web 11.
  • the mirror 15 is rotatable about its axis so that the light beam is caused to scan along the axis of the roller 12, and transversely across the moving web 11, as each facet of the mirror rotates relative to the incident beam.
  • the beam moves between limits shown by the broken lines 17 and 18.
  • the surface of the roller 12 is treated to make it generally non-reflecting of the light. For a use in which the web is generally non-reflecting, then the roller is made reflecting so that similar signals, but of opposite polarity, are detected.
  • Sensing means in the form of a photo-diode 19 is placed in the path of the beam at some convenient point near the start of the scan to produce a timing reference signal for subsequent circuit functions.
  • Light that is reflected from the roller and light reflected from the web is collected in the photomultiplier detection means 16 and any fault signal obtained therefrom is passed to the remainder of the circuit arrangement indicated at 20.
  • the output of the photo-diode 19 is fed to primary pulse means.
  • This includes an amplifier 21 and a squaring amplifier 22, whereby a rectangular pulse is produced near the beginning of each scan.
  • the squaring amplifier conveniently produces a pulse of known amplitude.
  • the falling edge of the pulse triggers an adjustable delay unit 23.
  • the unit may take any convenient form but is shown as a pulse generator.
  • the duration of the generated pulse is adjusted in accordance with the approximate width of the web so that it ends at a time just prior to that at which the beam is expected to engage the edge of the web.
  • the falling edge of the delay pulse triggers an edge slot pulse generator 24.
  • the edge slot generator produces a primary pulse of predetermined duration which extends until a time at which the beam must have engaged the web, for any likely position of the edge.
  • the edge slot, (primary), pulse is thus generated in response to the timing reference signal, the adjustable delay unit 23 varying the position of the edge slot pulse into the scan in order to accommodate different web widths.
  • Fault counting is begun when the edge of the web is detected within the edge slot, that is, during the presence of the edge slot pulse, so that faults are counted after the edge is detected and not after an arbitrary period as in previous arrangements.
  • the output of the photomultiplier detection means 16 is passed through a high-pass filter 25 to remove any do. component of the signal and then to a comparator 26.
  • the sudden change in the amount of light reflected as the beam engages the web creates a large input signal, and the comparator'output is dependent on the input signal being above the threshold value chosen to exclude pulses other than the large edge pulse.
  • the output of the comparator 26 is fed to a tail-biter circuit 27.
  • the tail-biter circuit 27 includes a bistable circuit 27' which gives a normally positive output that is reduced to zero or a negative value when a positive input signal is applied; the change in output is delayed for a very small period of time, say, 20 nano-seconds after the input is applied.
  • the tail-biter is defined as a circuit arrangement in which the output comprises the original input signal existing for a short period of time after the application of the input signal. The output is fed to the inputs of a three-input AND-gate 28. Thus irrespective of the subsequent output state of the comparator 26, the effective input to the AND-gate 28 from this tail-biter source occurs only for'20 nano-seconds after the start of the signal.
  • the third input to the AND-gate is the pri- I vmary pulse from the edge slot pulse generator 24.
  • the output of the AND-gate 28 will therefore only be a positive pulse of 20 nano-second duration if the beam image crosses the edge of the web during the period of the edge slot.
  • the output signal from the AND-gate 28 is fed, by way. of an optional delay unit 29, to a counter enabling pulse generator 30.
  • the generator 30, upon receipt of the AND-gate pulse, generates a pulse of duration equal to the time taken for the beam image to cross the known width of the web.
  • the tail-biter 27, AND-gate 28, delay 29 and generator 30 comprise timing means. This pulse permits a counter 31 to function only while the pulse is present. Fault signals are fed directly from the output of the filter 25 to the input of the counter .31.
  • the use of the delay unit 29 and the relationship between the circuit operations may be explained with reference to FIGS. 2(a) and 2(b).
  • the lines 32 indicate the positions of the incident beam at times t to and the waveforms A to H of signals appearing at the points labelled A to H in the circuit at corresponding times are shown in FIG. 2(b). 1
  • the waveform of the output signal of the photomultiplier detection means is shown at A in FIG. 2(b) for one complete scan.
  • the waveform is characterised by a step corresponding to each edge of the web.
  • the waveform B shows the form of the detected signal after passage through the high-pass filter 25 and in which the step at each edge has been replaced by a spike pulse of much greater amplitude than the intermediate fault pulses.
  • the comparator 26 acts to pass only points of the signal above the threshold value shown in waveform B at 26'.
  • the beam commences its scan at time t
  • the beam crosses the photo-diode 19 of the sensing means, actuating the delay unit 23 to initiate the delay pulse shown at 23 in the waveform C of FIG. 2(b).
  • the delay pulse 23' falls to zero and the edge slot generator 24 is triggered producing a positive output pulse 24 for a preset period lasting until a time t as shown in waveform D. The output then returns to zero for the remainder of the scan.
  • the output of the bistable circuit 27 in the tailbiter circuit 27 is depicted in waveform E, the level falling to zero at a time t, shortly after the fault pulse representing the edge hasbeen detected.
  • the waveforms B, D and E are combined in the AND-gate 28 producing the output pulse 28' of the waveform F. If the fault counting circuit was activated in response to the pulse 28' of waveform F then the falling edge of the edge pulse below the level indicated at 26 would be detected as a fault.
  • the output of the AND-gate is delayed in the delay unit 29 until a time t, when the edge pulse of waveform B has fallen to a low value, and is then passed as a pulse 29' see waveform G to the counter enabling generator 30.
  • the counter enabling generator produces an output pulse, as shown as waveform H, of duration equal to the time taken for the beam to cross the known width of the web and which lasts until a time t,,.
  • the circuit arrangement 20 as described may be modified to supply information on the position of the edge of the web to a servo control system whereby the web may be accurately positioned for trimming or printing.
  • FIG. 3 A modified form of the circuit of FIG. 1 is shown in FIG. 3.
  • a scan timing reference signal is detected by the photo-diode 19, amplified and fed as a rectangular pulse into an adjustable delay unit 23.
  • the delay unit 23 provides a rectangular pulse of adjustable duration.
  • the falling edge of the delay pulse triggers a first pulse generator 33 producing a secondary, or preedge pulse, that is, a pulse which ends before the beam engages the web.
  • the falling edge of this pulse triggers a similar generator 34 comprising the primary pulse generator which produces a shorter edge slot pulse, equivalent to the primary pulse of the previous embodiment, that should be present as the beam image crosses the edge of the Web.
  • a second pulse generator 35 produces a further secondary pulse, a postedge pulse, of similar duration to the pre-edge pulse upon being triggered by the falling edge of the edge slot pulse.
  • each of the pulse generators 33, 34 and 35 is fed to switching means and in particular to one input of AND-gates 36, 37 and 38 respectively.
  • the other inputs are common to each gate and comprise the output of the tail-biter circuit 27.
  • the output of the AND-gate 37 is fed by way of a switch 39 to the delay unit 29, counter enabling generator 39 and counter 31 described for FIG. 1.
  • the switch 39 is a three position double-pole switch and is normally in the (centre) position 1.
  • the outputs of AND- gates 36 and 38 are fed respectively to servo control means 40 and 41.
  • FIG. 4(a) is similar to FIG. 2(a) in that it represents the beam positions at time t to t of one scan and the waveforms of FIG. 4(b) on the same time scale represent the signals at positions I to P in FIG. 3.
  • the beam begins to scan at a time t and crosses the photo-diode 19 at t,, at which time the delay unit pulse 23' is triggered (waveform I).
  • the duration of the pulse is adjustable but is shown as ending at time t
  • the preedge pulse shown at 33' in waveform J, is triggered at the time t and continues until time t;,.
  • the edge slot pulse is generated (34' in waveform K) and continues until time t,,.
  • the post-edge pulse is generated (35' in waveform L) which continues untiltime Normally the web is positioned such that the beam image engages the web at a time t.,, between times t;,
  • the beam leaves the web at a time t, and the scan ends at a time
  • the waveform M represents the detected signal (after filtering) and the threshold value 26' that above which the comparator 26 provides an output.
  • the waveform N represents the output of the bistable circuit 27' in the tail-biter circuit 27.
  • the signals having the waveforms L, M and N are fed into the AND-gate 37 which produces a short pulse output (37' in waveform After a suitable delay the pulse is used to trigger a pulse (waveform P) from the counter enabling generator 30.
  • the AND-gates 36 and 38 have no inputs from the generators 33 and 35 between the time i and t and so give no output. If, however, the web is displaced from its normal position, say to the left in FIG. 4(a), such that the beam crosses the edge of the web at a time between and then there will be no output from the AND-gate 37, but a pulse will be produced at the output of the AND-gate 36.
  • the servo control system 41 will operate to move the web to the right so that on the next scan, the edge of the web will be detected during the edge slot pulse. Thus no fault count will be made unless the web is in the correct position.
  • the edge slot is required to prevent the servo system hunting about the correct position.
  • the pre-edge and post-edge pulse generators 33 and 35 are replaced by clock pulse generators 42 and 43 respectively each capable of emitting a predetermined number of clock pulses.
  • the edge slot generator is not required as far as the positioning mechanism is concerned, that is, no dead-band is required, and is omitted from the circuit as shown.
  • a fault signal greater than the level set by the comparator 26 is used to trigger gate control means comprising a pulse generator 44.
  • the generator produces a pulse which extends for a period of time in excess of the sum of the clock pulse generator emitting periods of the clock generators 42 and 43, and is fed to an input of each of the gates 45 and 46.
  • the trains of clock pulses are fed to gates 45 and 46 which have outputs connected to the triggers of monostable circuits 47 and 48 respectively such that a train of clock pulses passed by either gate produces, from the associated monostable circuit, an effective do. output for the duration of the pulse train.
  • the passage of the beam across the photo-detector 19 initiates a pulse, delayed until a time shortly before the beam is expected to engage the surface.
  • the delayed pulse triggers the clock generator 42 which produces a train of clock pulses until the time when the beam is expected to engage the surface, after which the clock generator 43 produces a pulse train of equal duration.
  • the train of clock pulses from the clock generator 42 are fed to the gate 45. If during the generating period the edge of the surface is detected then the output from the comparator 26 triggers the gate control generator 44 which produces an output pulse to open the gate 45. This permits passage of the pulse train to the monostable circuit 47 and the production of a dc. output signal, which signal is used directly as a position servo driving signal to move the surface in the direction of scan of the beam. The signal lasts until the clock pulse train stops, that is, when the edge of the surface is in the desired expected position.
  • the clock pulse generator 43 produces a train of clock pulses immediately after the pulse train from generator 42 has ceased and the pulses are fed to gate 46.
  • This gate is normally open but passage is inhibited by the output signal from the gate control generator 44.
  • the edge is detected before its correct position none of the clock pulses from the generator 43 will reach the monostable circuit 48. If the edge is not detected the clock pulses reach the monostable circuit 48 and a dc. signal for servo correction of the position of the surface is produced.
  • This signal causes the surface to be moved in the opposite direction to the scanning beam until the edge is detected, when the generator 44 produces an output and inhibits formation of the servo signal.
  • the edge slot no longer is essential to provide a servo dead-band so far as positioning of the web is concerned, but is still useful as an edge slot for controlling the commencement of fault counting, and may be made as short as desired.
  • the web positioning system as described may be used with advantage to position a web in relation to a pattern on the web, for example, when slitting a web parallel to the pattern, or some other known discontinuity in the light absorbing properties of the surface.
  • the switch 39 is retained in position 1.
  • the .delay of unit 23 is extended onto the web such that the pre-edge pulse becomes the pre-pattern pulse, the edge slot and edge slot pulse become the pattern slot" and pattem slot pulse, and the post-edge pulse becomes the postpattern pulse. Operation is as previously described with servo correction being undertaken each time that the pattern is detected other than during the pattern slot pulse.
  • the AND-gate 37 and the fault counter may be retained and may be used to keep account of stability of the web position by counting the number of times that the pattern is detected within the pattern slot. If counting is not required then the switch 39 is moved to the (lower) position 2 to disconnect the counter 31 and the enabling generator 30.
  • the fault counting may still be undertaken independently of the detection of the edge of the web.
  • the switch 39 is moved to the (upper) position 3.
  • the enable circuit 30 is operated by the pulse of the delay unit 23 and effectively activates the counter 31 from the start of the scan. Counting, however, is inhibited for the duration of the delay pulse by a gate 42 so that faults are not counted until at least the pre-edge pulse is present. Thus all faults will be counted for all possible web positions and correction of the web position undertaken.
  • Edge triggering of the fault counting means described above in detail deals satisfactorily with the leading edge of the photomultiplier detector signal but not with the trailing edge because a constant web width is assumed. Variation in width of the web may lead to faults being detected from outside the web if it should decrease, or miss faults near to the edge if it should increase.
  • the trailing edge of the web may be detected in a manner similar to that employed for the leading edge in the circuit arrangements of FIGS. 1 and 3.
  • a photodiode (not shown), similar to the photo-diode 19, is positioned in the path of the beam at some point near to the end of the scan and is used to trigger a delay pulse which extends until just before the trailing edge of the web is reached in the next scan.
  • An edge slot pulse is then generated in the vicinity of the trailing edge, the associated circuitry (not shown) responding to the detection of a large negative going signal in this edge slot to stop the fault counting means 31.
  • a fresh delay pulse is triggered at the end of that scan.
  • the trailing edge may be dealt with by having a scanning edge detector at each edge of the web and arranged to detecteach edge as a leading edge.
  • the principle of scanning the webat each edge may be adapted to the supply of web position signals and may be extended to measurement of the width of the web.
  • the scanning mirrors 15 of each scanning station 10 may be placed an accurately known distance apart near each edge of the web 11.
  • the durations of the various pulses in the circuit are modulated according to the position of the mirror in the scan such that the position of the image, when detected, may be directly related to the rotational position of the reflecting mirror.
  • the exact width of the web may be found for that particular scan.
  • Fault detection may be carried out simultaneously and the faults may be counted for defined regions near the web edges. If it is, found that most of the faults occur in regions close to one or both edges, then the web may be slit along the one or both edges at such a All the above arrangements may be adapted, with suitable alterations to polarity of detected signal, for detection of faults by transmission of the beam through a transparent or partially transparent web.
  • a circuit arrangement for use with a detector of faults in a moving surface, which surface is permitted to undergo limited displacement transversely to the direction of said movement comprising a source of a beam of optical radiation, means to scan the beam repetitively across the surface transversely to the direction of motion of the surface and detection means to collect optical radiation emanating from the surface to produce, in response to a change in the radiation collected, a fault signal
  • the circuit arrangement including sensing means operable to detect the passage of the beam past a point to produce, in each scan, a timing reference signal, primary pulse means responsive to each timing reference signal to generate a primary pulse which exists for the time taken by the beam to cross a region of permitted surface displacement within which region lies a discontinuity in the radiation absorbing properties of the surface, timing means responsive to the occurrence of a fault signal greater than a predetermined threshold value during the existence of the primary pulse to produce a counter enabling signal, and a counter, enabled by the counter enabling signal, to count subsequent fault signals.
  • sensing means comprises a photodetector in the path of the beam at the start of the scan.
  • timing means comprises a two-input AND gate arranged to have as inputs the primary pulse and the fault signal greater than a predetermined value, and a pulse generator arranged to be triggered by the AND gate to produce an output for a predetermined period of time.
  • a circuit arrangement as claimed in claim 3 which also includes a tail-biter circuit, as herein defined, in series with the fault signal input to the AND gate.
  • a circuit arrangement as claimed in claim 4 which also includes delay means between the AND gate and the pulse generator.
  • a circuit arrangement for use with a detector of faults in a moving surface comprising a source of a beam of optical radiation, means to scan the beam repetitively across the surface transversely to the direction of motion of the surface and detection means to collect optical radiation emanating from the surface to produce, in response to a change in the radiation collected, a fault signal
  • the circuit arrangement including sensing means operable to detect the passage of the beam past a point to produce, in each scan, a timing reference signal, primary pulse means responsive to the timing reference signal to generate a primary pulse extending from some time before the beam engages a known discontinuity in the radiation absorbing properties of the surface untilsome time after the engagement, timing means responsive to the occurrence of a fault signal greater than a predetermined threshold value during the presence of the primary pulse to produce a counter enabling signal, and a counter enabled by the counter enabling signal to count subsequent fault signals, secondary pulse means responsive to the timing reference signal for providing a plurality of secondary pulses, at least one immediately preceding and at least one immediately succeeding the primary pulse,
  • the secondary pulse means comprises a first pulse generator arranged to be triggered by said timing reference signal to produce a secondary pulse of predetermined duration and to cause, at the termination of said secondary pulse, operation of the primary pulse generator and the generation of said primary pulse, and a second pulse generator arranged to be triggered at the termination of said primary pulse to produce a further secondary pulse of predetermined duration.
  • the switching means comprises a plurality of AND gates, different AND gates being arranged to be supplied with different secondary pulses and all gates being arranged to be supplied with a fault signal greater than said predetermined value.
  • the secondary pulse means comprises a first clock pulse generator arranged to be operated by said timing reference signal to produce a predetermined number of secondary pulses and to cause, after the generation of the last pulse of said predetermined number, operation of the primary pulse generator and the generation of said primary pulse, and a second clock pulse generator adapted to be operated at the termination of said primary pulse to produce a predetermined number of further secondary pulses.
  • the switching means includes gate control means responsive to said fault signal to produce an output signal of predetermined duration, a first gate between the first clock pulse generator and the servo control means, said first gate being arranged to be opened by the output signal of the gate control means to allow passage to the servo control means of the remainder of the secondary pulses from the first clock pulse generator, and a second gate between the second clock pulse generator and the servo control means, said second gate being arranged to be closed by the output signal of the gate control means to prevent passage of the remainder of the secondary pulses from the second clock pulse generator to the servo control means.
  • a detector of faults in a moving surface comprising a source of a beam of optical radiation, means to scan the beam repetitively across the surface transversely to the direction of motion of the surface, which surface is permitted to undergo limited displacement transversely to the direction of said movement, and detection means to collect optical radiation emanating from the surface to produce, in response to a change in the radiation collected, a fault signal, and a circuit arrangement including sensing means operable to detect the passage of the beam past a point to produce, in each scan, a timing reference signal, primary pulse means responsive to each timing reference signal to generate a primary pulse which exists for the time taken by the beam to cross a region of permitted surface displacement within which region lies a discontinuity in the radiation absorbing properties of the surface, timing means responsive to the occurrence of a fault signal greater than a predetermined threshold value during the existence of the primary pulse to produce a counter enabling signal, and a counter, enabled by the counter enabling signal, to count subsequent fault signals.
  • a detector of faults in a moving surface comprising a source of a beam of optical radiation means to scan the beam repetitively across the surface transversely to the direction of motion of the surface and detection means to collect optical radiation emanating from the surface to produce, in response to a change in the radiation collected, a fault signal and a circuit arrangement including sensing means operable to detect the passage of the beam past a point to produce, in each scan, a timing reference signal, primary pulse means responsive to the timing reference signal to generate a primary pulse extending from some time before the beam engages a known discontinuity in the radiation absorbing properties of the surface until some time after the engagement, timing means responsive to the occurrence of a fault signal greater than a predetermined threshold value during the presence of the primary pulse to produce a counter enabling signal, a counter, enabled by the counter enabling signal, to count subsequent fault signals, secondary pulse means responsive to the timing reference signal for providing a plurality of secondary pulses, at least one immediately preceding and at least one immediately succeeding the primary pulse, switching means responsive to a fault signal greater

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US00309719A 1971-11-30 1972-11-27 Detection of blemishes on surfaces Expired - Lifetime US3803474A (en)

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Application Number Priority Date Filing Date Title
GB5562671A GB1366369A (en) 1971-11-30 1971-11-30 Detection of faults on surfaces
US00309719A US3803474A (en) 1971-11-30 1972-11-27 Detection of blemishes on surfaces
DE2258158A DE2258158C3 (de) 1971-11-30 1972-11-28 Schaltungsanordnung für einen Detektor zum Feststellen von Fehlern in einer bewegten Materialbahn
FR7242397A FR2163148A5 (de) 1971-11-30 1972-11-29

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GB5562671A GB1366369A (en) 1971-11-30 1971-11-30 Detection of faults on surfaces
US00309719A US3803474A (en) 1971-11-30 1972-11-27 Detection of blemishes on surfaces

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DE (1) DE2258158C3 (de)
FR (1) FR2163148A5 (de)
GB (1) GB1366369A (de)

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DE2620599A1 (de) * 1975-05-10 1976-11-25 Fujitsu Ltd Chip-bond-vorrichtung
US4054824A (en) * 1975-05-10 1977-10-18 Fujitsu Ltd. Wire bonding unit using infra-red ray detector
US4217053A (en) * 1977-04-20 1980-08-12 Robert Bosch Gmbh Apparatus and method to test workpieces for size, relative position, material integrity, and the like
EP0020880A1 (de) * 1979-06-26 1981-01-07 Erwin Sick GmbH Optik-Elektronik Optische Vorrichtung zur Fehlerprüfung von bahnförmigen Materialien
EP0069061A1 (de) * 1981-06-17 1983-01-05 Ciba-Geigy Ag Verfahren und Vorrichtung zum Überprüfen von Bahnmaterial
US5867099A (en) * 1997-11-24 1999-02-02 Keeter; Daniel R. Motion sensing, lighting and alarming system

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Publication number Priority date Publication date Assignee Title
DE2952885C2 (de) * 1978-06-20 1986-01-30 Sumitomo Metal Industries, Ltd., Osaka Vorrichtung zur berührungslosen Ultraschallfehlerprüfung
SE456532B (sv) * 1985-10-18 1988-10-10 Asea Ab Arrangemang for ytavsokning av ett provobjekt
DE19803085A1 (de) * 1998-01-28 1999-08-05 Metz Albert Ria Electronic Anschlußklemme

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL259070A (de) * 1959-12-22
NL279098A (de) * 1961-05-31

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2620599A1 (de) * 1975-05-10 1976-11-25 Fujitsu Ltd Chip-bond-vorrichtung
US4054824A (en) * 1975-05-10 1977-10-18 Fujitsu Ltd. Wire bonding unit using infra-red ray detector
US4217053A (en) * 1977-04-20 1980-08-12 Robert Bosch Gmbh Apparatus and method to test workpieces for size, relative position, material integrity, and the like
EP0020880A1 (de) * 1979-06-26 1981-01-07 Erwin Sick GmbH Optik-Elektronik Optische Vorrichtung zur Fehlerprüfung von bahnförmigen Materialien
EP0069061A1 (de) * 1981-06-17 1983-01-05 Ciba-Geigy Ag Verfahren und Vorrichtung zum Überprüfen von Bahnmaterial
US4522497A (en) * 1981-06-17 1985-06-11 Ciba Geigy Ag Web scanning apparatus
US5867099A (en) * 1997-11-24 1999-02-02 Keeter; Daniel R. Motion sensing, lighting and alarming system

Also Published As

Publication number Publication date
GB1366369A (en) 1974-09-11
DE2258158B2 (de) 1980-10-23
DE2258158A1 (de) 1973-06-07
DE2258158C3 (de) 1981-09-17
FR2163148A5 (de) 1973-07-20

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