WO2019181243A1 - Procédé d'inspection à onde ultrasonore, dispositif d'inspection à onde ultrasonore et procédé de fabrication de pompe d'alimentation en carburant haute pression faisant appel à un procédé d'inspection à onde ultrasonore - Google Patents

Procédé d'inspection à onde ultrasonore, dispositif d'inspection à onde ultrasonore et procédé de fabrication de pompe d'alimentation en carburant haute pression faisant appel à un procédé d'inspection à onde ultrasonore Download PDF

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WO2019181243A1
WO2019181243A1 PCT/JP2019/003951 JP2019003951W WO2019181243A1 WO 2019181243 A1 WO2019181243 A1 WO 2019181243A1 JP 2019003951 W JP2019003951 W JP 2019003951W WO 2019181243 A1 WO2019181243 A1 WO 2019181243A1
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Prior art keywords
laser
wave
ultrasonic
transverse
longitudinal
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PCT/JP2019/003951
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English (en)
Japanese (ja)
Inventor
聡 北澤
菅波 正幸
伸也 中谷
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日立オートモティブシステムズ株式会社
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Publication of WO2019181243A1 publication Critical patent/WO2019181243A1/fr

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00Working by laser beam, e.g. welding, cutting or boring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K31/00Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/44Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04Analysing solids
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/22Details, e.g. general constructional or apparatus details
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/22Details, e.g. general constructional or apparatus details
    • G01N29/24Probes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/22Details, e.g. general constructional or apparatus details
    • G01N29/26Arrangements for orientation or scanning by relative movement of the head and the sensor

Definitions

  • the present invention relates to an ultrasonic inspection method and ultrasonic inspection apparatus for detecting defects in a laser weld with ultrasonic waves by laser irradiation, and a high-pressure fuel supply pump for manufacturing a high-pressure fuel supply pump using the ultrasonic inspection method. And methods.
  • Patent Document 1 Japanese Patent Laid-Open No. 2012-006078
  • Patent Document 2 Japanese Patent Laid-Open No. 2017-161441
  • Patent Document 1 discloses a welding system that detects a welding failure by a laser ultrasonic method. This welding system irradiates the surface of a welding target after welding with a welding mechanism, a transmission laser light source, and a transmission laser light generated by the transmission laser light source while moving with the welding mechanism with respect to the welding target.
  • an interferometer for interferometric measurement of the scattered / reflected laser beam (see summary).
  • the ultrasonic flaw detection method for welded joints in Patent Document 2 is an ultrasonic flaw detection method for flaws in welded joints using ultrasonic waves, including a creeping wave method, a longitudinal wave oblique angle method, a round trip method, The flaw detection is performed by a combination of at least two of the shear wave oblique angle methods (see summary).
  • Patent Document 2 describes that the following (a) to (f) are assumed as the types of defects, and whether or not detection is possible was verified.
  • Patent Document 1 shows welding in a butt joint, and does not consider welding in a lap joint in which two members are overlapped and welded from one side to two members.
  • Patent Document 2 considers welding of lap joints.
  • Patent Document 2 enables detection of different types of defects (above (a) to (f)) using longitudinal waves and transverse waves.
  • the defects (a) to (f) in Patent Document 2 exist above the boundary surface between the two members (the side on which welding is performed). That is, in Patent Document 1 and Patent Document 2, sufficient consideration is given to detecting a defect existing below the boundary surface between two members in a lap joint (on the side opposite to the side on which welding is performed). Absent.
  • Longitudinal and transverse waves used in the ultrasonic method are directional, and longitudinal and transverse waves are reflected at the interface between the two members, so that defects that occur inside narrow welds due to laser welding are eliminated. It is not easy to detect.
  • An object of the present invention is to make it possible to detect defects existing above and below the boundary surface of two members in a laser welded portion of a lap joint.
  • the present invention provides a laser beam for detecting defects in a laser welded portion in which laser welding is performed by irradiating a laser beam on the first member and the second member constituting the lap joint from the first member side. Detect with ultrasound by irradiation. Generate a transverse wave generation laser at a transverse laser generation laser irradiation position located on one side across the weld line, and generate a longitudinal wave located on the one side farther from the welding line than the transverse laser generation laser irradiation position. A laser for longitudinal wave is irradiated to the laser irradiation position.
  • the transverse wave receiving laser is irradiated to the transverse wave receiving laser irradiation position located on the other side across the welding line, and the longitudinal wave receiving is located on the other side farther from the welding line than the transverse wave receiving laser irradiation position.
  • a longitudinal wave receiving laser is irradiated to the laser irradiation position.
  • the transverse wave ultrasonic wave generated by the thermoelastic mode generated by the irradiation of the generation laser for the transverse wave is detected by the receiving laser for the transverse wave, and the ultrasonic wave generated by the thermoelastic mode generated by the irradiation of the generation laser for the longitudinal wave is detected by the reception laser for the longitudinal wave.
  • a defect at a position shallower than the boundary surface between the first member and the second member is detected by longitudinal wave ultrasonic waves, and a defect at a position deeper than the boundary surface is detected by transverse wave ultrasonic waves.
  • FIG. 1 is a conceptual diagram showing a process of detecting a defect De by a laser ultrasonic method.
  • the inspection target A is irradiated with the laser LaT to generate ultrasonic waves in the inspection target A.
  • the ultrasonic wave UT generated in the inspection object A is reflected by the defect De, and a displacement (surface displacement) Di is generated on the surface of the inspection object A.
  • the laser LaR is irradiated to the surface where the surface displacement Di is generated, the surface displacement Di is detected by the detector Det, and the defect De is detected.
  • the laser LaT that generates the ultrasonic UT in the inspection target A is referred to as a generation laser or a transmission laser.
  • the laser LaR that detects the surface displacement Di is called a reception laser or a detection laser.
  • a method for performing defect detection using a laser ultrasonic method is referred to as an ultrasonic inspection method
  • an apparatus for performing defect detection using a laser ultrasonic method is referred to as an ultrasonic inspection device.
  • the ultrasonic inspection method and the ultrasonic inspection apparatus detect the defect De of the welded portion We in laser welding. Examples of the defect (scratch) De of the welded portion We include a crack and a blow hole.
  • the welded portion We is a portion where the molten metal is solidified by welding.
  • a swell (weld bead) is formed on the surface side of the welded portion We. This weld bead may be removed.
  • FIG. 2 is a diagram showing a concept of an in-process inspection apparatus 1000 using the ultrasonic inspection apparatus 1 according to the present invention.
  • the ultrasonic inspection apparatus 1 of this embodiment constitutes an in-process inspection apparatus 1000 that works in conjunction with the laser welding apparatus 2. That is, the ultrasonic inspection apparatus 1 of this embodiment is applied to a manufacturing apparatus for the high-pressure fuel supply pump 100, and laser welding is performed on the high-pressure fuel supply pump 100 by the laser welding apparatus 2 while simultaneously performing laser welding by the ultrasonic inspection apparatus 1. A defect De generated in the portion We is detected. For this purpose, the ultrasonic inspection apparatus 1 and the laser welding apparatus 2 are arranged around the high-pressure fuel supply pump 100.
  • the laser welding device 2 is controlled by a control device 3 in the laser welding process.
  • the defect detection process (flaw detection process) is controlled by the control device 3.
  • the laser welding apparatus 2 and the ultrasonic inspection apparatus 1 are rotationally driven in the Ar direction around the rotation axis AR by the driving device 4.
  • the inspection target A is a welding target.
  • the object A to be welded is rotated around the rotation axis, and in accordance with this rotation, the laser welding apparatus 2 performs laser welding, and the ultrasonic inspection apparatus 1 performs non-contact inspection (flaw detection) using a laser ultrasonic method.
  • the laser welding part We is comprised as a welding line which comprises a linear form.
  • the high-pressure fuel supply pump 100 is described as an object to be welded (inspected object) A, but it may be a fuel injection valve or the like. Further, it is not always necessary to configure the in-process inspection apparatus, and welding and inspection may be performed separately, or the ultrasonic inspection apparatus 1 that performs only inspection may be configured. However, an in-process inspection apparatus is configured using the ultrasonic inspection apparatus 1 and inspection is performed while welding is performed. By re-welding when a defect is found, the occurrence of a defective product can be prevented in advance. Productivity can be improved.
  • FIG. 3 is a block diagram showing the configuration of an in-process inspection apparatus 1000 that combines the ultrasonic inspection apparatus 1 and the laser welding apparatus 2 according to the present invention.
  • the in-process inspection apparatus 1000 includes an ultrasonic inspection apparatus 1, a laser welding apparatus 2, and a control apparatus 3.
  • the laser welding apparatus 2 is a welding apparatus that performs laser welding on the high-pressure fuel supply pump 100 that is the workpiece (workpiece) A.
  • the laser welding apparatus 2 shows an example in which the pump body 101 and the damper cover 111 are welded.
  • the pump main body 101 and the damper cover 111 constitute a lap joint, and the laser LaW is irradiated from the damper cover 111 side.
  • the object A to be welded is rotated about the rotation axis AR. Therefore, the welded portion constitutes a weld line extending in the circumferential direction around the rotation axis AR.
  • the object A to be welded is rotated, but the laser welding apparatus 2 may be rotated around the rotation axis AR.
  • the ultrasonic inspection apparatus 1 is also rotated around the rotation axis AR. That is, the drive device 4 is configured to relatively displace (relatively move) the ultrasonic inspection device 1, the laser welding device 2, and the welding target A in the direction along the welding line We.
  • the ultrasonic inspection apparatus 1 As the welding apparatus, an apparatus using a welding method other than laser welding can be used.
  • the ultrasonic inspection apparatus 1 according to the present embodiment exhibits excellent flaw detection performance with respect to a welding method in which the welding depth is deeper than the line width of the welding line We, such as laser welding. It works more effectively as the welding depth becomes deeper than the width.
  • the ultrasonic inspection apparatus 1 includes a generation laser irradiation unit (first laser irradiation unit) 11 for irradiating a welding target (inspected target) A with a generation laser (first laser) LaT that generates ultrasonic waves, a surface A receiving laser irradiation unit (second laser irradiation unit) 12 for irradiating a receiving laser (second laser) LaR for detecting displacement Di, interferometer side units 13B and 13C, and a data recording / analyzing device 14 Prepare.
  • a generation laser irradiation unit (first laser irradiation unit) 11 for irradiating a welding target (inspected target) A with a generation laser (first laser) LaT that generates ultrasonic waves
  • second laser irradiation unit 12 for irradiating a receiving laser (second laser) LaR for detecting displacement Di
  • interferometer side units 13B and 13C for detecting displacement Di
  • data recording / analyzing device 14 Prepare.
  • the generation laser irradiation unit 11 includes a generation laser light source (first laser light source) 11A, a generation laser optical system for longitudinal waves (first laser optical system for longitudinal waves) 11B, and a generation laser optical system for transverse waves (first laser optical for transverse waves).
  • System 11C.
  • the reception laser irradiation unit 12 includes a reception laser light source (second laser light source) 12A, a reception laser optical system for longitudinal waves (second laser optical system for longitudinal waves) 12B, and a reception laser optical system for transverse waves (second laser optics for transverse waves). System) 12C.
  • the generation laser light source 11A generates a generation laser LaT.
  • the generation laser optical system 11B for longitudinal waves and the generation laser optical system 11C for transverse waves are optical systems for irradiating the welding target A with the generation laser LaT, and are composed of optical components such as a lens, a reflecting mirror, and an optical fiber.
  • the generation laser optical system 11B for longitudinal waves and the generation laser optical system 11C for transverse waves irradiate the welding target A with the generated laser LaT generated by the generated laser light source 11A which is a common laser light source.
  • a configuration may be adopted in which individual generation laser light sources 11A are provided in each of the longitudinal wave generation laser optical system 11B and the transverse wave generation laser optical system 11C.
  • the reception laser light source 12A generates a reception laser LaR.
  • the longitudinal wave receiving laser optical system 12B and the transverse wave receiving laser optical system 12C are optical systems for irradiating the welding target A with the receiving laser LaR, and collect reflected light and scattered light from the irradiation point of the receiving laser LaR. It is an optical system that emits light.
  • the longitudinal wave receiving laser optical system 12B and the transverse wave receiving laser optical system 12C are configured by optical components such as a lens, a reflecting mirror, and an optical fiber.
  • the longitudinal wave receiving laser optical system 12B and the transverse wave receiving laser optical system 12C irradiate the welding target A with the receiving laser LaT generated by the receiving laser light source 12A which is a common laser light source.
  • a configuration may be adopted in which individual reception laser light sources 12A are provided in each of the longitudinal wave reception laser optical system 12B and the transverse wave reception laser optical system 12C.
  • the generation laser light source 11A and the reception laser light source 12A various known laser light sources as described in Patent Document 1 can be used.
  • Interferometer side portions 13B and 13C include an interferometer, and perform interference measurement using reflected light and scattered light from the irradiation point of the reception laser LaR.
  • the reflected light and scattered light are affected by the surface displacement Di of the workpiece A to be welded by the ultrasonic wave UT.
  • the ultrasonic signals 13Bs and 13Cs including the information on the defect De can be detected by detecting the surface displacement Di of the workpiece A by interference measurement.
  • Interferometer side parts 13B and 13C output ultrasonic signals 13Bs and 13Cs obtained by the interference measurement as electric signals.
  • the ultrasonic signals 13Bs and 13Cs output from the interferometer side portions 13B and 13C are recorded as ultrasonic signal data in the data recording / analyzing device 14, and information on the defect De is analyzed based on the ultrasonic signal data.
  • the interferometer side unit 13B constitutes a first interference measurement unit (longitudinal wave interference measurement unit) that performs interference measurement of the longitudinal wave WL and outputs the ultrasonic signal 13Bs.
  • the interferometer side unit 13C constitutes a second interference measurement unit (a transverse wave interference measurement unit) that performs interference measurement of the transverse wave WT and outputs the ultrasonic signal 13Cs.
  • the position of the defect De is specified based on the irradiation positions of the generation laser LaT and the reception laser LaR corresponding to the ultrasonic signals 13Bs and 1Cs.
  • the position of the defect De is specified as a circumferential position along the weld line We.
  • a circumferential reference position is set for the welding target A. This reference position may be set to an arbitrary structure provided on the welding target A, or may be set regardless of the structure of the welding target A.
  • the intake valve mechanism 114, the discharge joint 116, etc. can be used as an arbitrary structure for setting the reference position.
  • a defect De at a shallow position in the welding depth direction is detected by a longitudinal wave
  • a defect De at a deep position is detected by a transverse wave. For this reason, it is possible to relatively distinguish the defect De at the shallow position from the defect De at the deep position.
  • the depth information of the defect De may be recorded in the data recording / analyzing device 14.
  • Patent Document 1 can be applied to the detection principle of the defect De using laser ultrasonic waves.
  • Patent Document 2 is different from the present embodiment in that no laser is used, the content described in Patent Document 2 can be applied to the detection principle of the defect De using ultrasonic waves.
  • FIG. 4A is a diagram showing the directivity of ultrasonic waves generated by laser irradiation, and is a diagram showing the directivity in the thermoelastic mode.
  • FIG. 4B is a diagram showing the directivity of ultrasonic waves generated by laser irradiation, and is a diagram showing the directivity in the ablation mode.
  • thermoelastic mode is a mode that occurs when the laser irradiation energy is low
  • ablation mode is a mode that occurs when the laser irradiation energy is high. Even when a contact type sensor that is not a laser ultrasonic type is used, the directivity of the ultrasonic wave has the same directivity as in FIG. 4B.
  • thermoelastic mode is used.
  • the ultrasonic transverse wave WT generated when laser irradiation is performed has a directivity DR1 in a direction inclined by 30 ° with respect to an axis line (0 ° axis) along the irradiation direction.
  • the longitudinal wave WL has directivity DR2 in a direction inclined by 65 ° with respect to an axis line (0 ° axis) along the irradiation direction.
  • the directivity DR1 of the transverse wave WT is different from the directivity DR2 of the longitudinal wave WL.
  • the transmission path of the transverse wave WT and the transmission path of the longitudinal wave WL are different.
  • the defect De existing at different depths of the welded portion We is detected by using the difference between the directivities DR1 and DR2 of the transverse wave WT and the longitudinal wave WL (difference in propagation path).
  • the directivity DR1 ′ and DR2 ′ are expanded with respect to the thermoelastic mode, and the defect De using the difference between the directivity DR1 ′ and DR2 ′ of the transverse wave WT and the longitudinal wave WL (difference in propagation path). Is difficult to detect.
  • FIG. 5 is a conceptual diagram for explaining the ultrasonic inspection method according to the present embodiment, and is a view showing the characteristics of the ultrasonic inspection method using the transverse wave WT.
  • FIG. 5 shows a state in which the first member 201 and the second member 202 are joined by a welded portion We by laser welding in a state where a lap joint is formed.
  • the first member 201 and the second member 202 are laser welded in a state where the surface 201A of the first member 201 and the surface 202A of the second member 202 are pressure-bonded, and the first member 201 and the second member 202 are bonded.
  • a boundary surface SB is formed between the two.
  • FIG. 5 shows a cross section perpendicular to the weld line We.
  • the weld depth D_We is formed larger than the line width ⁇ We of the weld line We.
  • the line width ⁇ We of the welding line We is a line width that appears on the surface of the first member 201.
  • the thickness dimension of the first member 201 is 1.2 mm
  • the line width ⁇ We of the welding line We is formed to be 1.0 mm or less, which is smaller than the thickness dimension of the first member 201.
  • the width ⁇ We_SB of the melted portion We in the boundary surface SB is not more than half (1 ⁇ 2 or less) of the line width ⁇ We, and is formed to be 0.5 mm or less.
  • the generated laser LaTT for generating the transverse wave WT is irradiated to the irradiated laser irradiation position PTT for the transverse wave positioned on one side of the welding line We with the weld line We interposed therebetween.
  • the transverse wave generation laser LaTT irradiated to the transverse wave generation laser irradiation position PTT generates a transverse wave WT of the ultrasonic wave UT.
  • the transverse wave WT propagates in a direction inclined by 30 ° with respect to the laser irradiation axis Ax_LaTT, is reflected by the defect De2, and propagates to the detection position (lateral laser receiving laser irradiation position) PRT located on the other side of the welding line We. To do.
  • the detection position PRT is irradiated with the transverse wave receiving laser LaRT, and a minute displacement Di (see FIG. 1) generated at the detection position PRT is detected.
  • the transverse wave generation laser LaTT is irradiated to the transverse wave generation laser irradiation position PTT that is separated from the center (center line) C_We in the width direction of the welding line We by a distance ltt in a direction orthogonal to the welding line We.
  • the transverse wave receiving laser LaRT is irradiated to the transverse wave receiving laser irradiation position separated from the center (center line) C_We in the width direction of the welding line We by a distance lrt in a direction orthogonal to the welding line We.
  • FIG. 6 is a diagram showing a range in which the defect De can be detected by the transverse wave WT and a range in which the detection is difficult.
  • FIG. 7 is a diagram illustrating a time change of the ultrasonic signal due to the transverse wave WT.
  • the transverse wave WT it is possible to detect the defect De2 at the depth of the boundary surface SB and the defect De1 at a position deeper than the boundary surface SB. This is because a difference appears in the time domain II of the ultrasonic signal (from 0.9 ⁇ s, more specifically from 0.9 to 1.2 ⁇ s) depending on whether the defects De1 and De2 are present or not. .
  • the ultrasonic signal 13Cs1 when the defect De1 located deeper than the boundary surface SB and the defect De3 located shallower than the boundary surface SB exist, and the ultrasonic signal 13Cs2 when no defect De exists. Is expressed conceptually.
  • the ultrasonic signal 13Cs1 has a peak PkWS caused by the surface wave WS, a peak PkDe1 caused by the defect De1, and a peak PkDe3 caused by the defect De3.
  • the peak PkWS generated by the surface wave WS and the peak PkDe3 generated by the defect De3 exist in the time domain I (before 0.9 ⁇ s), and the peak PkWS and the peak PkDe3 are difficult to distinguish from each other.
  • the peak PkDe1 generated by the defect De1 exists in the time domain II (0.9 ⁇ s or later), and the peak PkWS and the peak PkDe1 can be distinguished. Even when there is a defect De2 at the depth of the boundary surface SB, a peak occurs in the time domain II (0.9 ⁇ s or later), and the peak due to the defect De2 can be distinguished from the peak PkWS.
  • the defect De2 at the depth of the boundary surface SB and the defect De1 at a position deeper than the boundary surface SB can be detected by the transverse wave WT.
  • the transverse wave generation laser irradiation position PTT and the transverse wave reception laser irradiation position PRT may be changed in a direction perpendicular to the welding line We.
  • FIG. 8 is a conceptual diagram for explaining the ultrasonic inspection method according to the present embodiment, and shows the characteristics of the ultrasonic inspection method using the longitudinal wave WL.
  • the longitudinal wave generation laser LaTL for generating the longitudinal wave WL is irradiated to the longitudinal wave generation laser irradiation position PTL located on one side of the welding line We across the welding line We.
  • the longitudinal wave generation laser LaTL irradiated to the longitudinal wave generation laser irradiation position PTL generates a longitudinal wave WL of the ultrasonic wave UT.
  • the longitudinal wave WL propagates in a direction inclined by 65 ° with respect to the laser irradiation axis Ax_LaTL, is reflected by the defect De2, and is detected at the detection position (vertical wave receiving laser irradiation position) PRL located on the other side of the welding line We. Propagate.
  • the detection position PRL is irradiated with a longitudinal wave reception laser LaRL, and a minute displacement Di (see FIG. 1) generated at the detection position PRL is detected.
  • Longitudinal wave generation laser LaTL is irradiated to a longitudinal wave generation laser irradiation position PTL separated from the center (center line) C_We of the welding line We in the direction orthogonal to the welding line We by an interval of ltl.
  • the longitudinal wave reception laser LaRL is irradiated to the longitudinal wave reception laser irradiation position PRL which is separated from the center (center line) C_We in the width direction of the welding line We by a distance lrl in a direction orthogonal to the welding line We.
  • the interval ltl is larger than the interval ltt
  • the interval lrl is larger than the interval lrt.
  • the longitudinal wave generating laser LaTL is irradiated to a position away from the center (center line) C_We of the welding line We with respect to the transverse wave generating laser LaTT
  • the longitudinal wave receiving laser LaRL is irradiated with respect to the transverse wave receiving laser LaRT. Irradiated to a position away from the center (center line) C_We of the welding line We.
  • the longitudinal wave generation laser LaTL and the longitudinal wave reception laser LaRL are irradiated from the outside of the transverse wave generation laser LaTT and the transverse wave reception laser LaRT.
  • FIG. 9 is a diagram showing a range in which the defect De can be detected by the longitudinal wave WL and a range in which the detection is difficult.
  • FIG. 10 is a diagram illustrating a time change of the ultrasonic signal due to the longitudinal wave WL.
  • the longitudinal wave WL it is possible to detect the defect De2 at the depth of the boundary surface SB and the defect De3 at a position shallower than the boundary surface SB. This is because a difference appears in the time domain I of the ultrasonic signal (before 0.9 ⁇ s, more specifically 0.6 to 0.9 ⁇ s) depending on whether there is a defect De2 or De3 and no defect De. .
  • the ultrasonic signal 13Bs1 when the defect De1 located deeper than the boundary surface SB and the defect De3 located shallower than the boundary surface SB exist, and the ultrasonic signal 13Bs2 when no defect De exists. Is expressed conceptually.
  • the ultrasonic signal 13Bs1 has a peak PkWS caused by the surface wave WS and a peak PkDe3 caused by the defect De3. Since the longitudinal wave WL propagates in a direction inclined by 65 ° with respect to the laser irradiation axis Ax_LaTL, it is reflected by the boundary surface SB and it is difficult to enter a position deeper than the depth of the boundary surface SB. For this reason, the longitudinal wave WL cannot detect the defect De1 distributed at a position deeper than the depth of the boundary surface SB.
  • the peak PkWS generated by the surface wave WS appears in the time domain II (from 0.9 ⁇ s, more specifically from 0.9 to 1.2 ⁇ s).
  • the peak PkDe3 caused by the defect De3 appears in the time domain I, and the peak PkWS and the peak PkDe1 can be distinguished.
  • a peak is generated in the time domain II (after 0.9 ⁇ s), but is shifted from the peak PkWS at a time earlier than the peak PkWS, so the peak due to the defect De2 is the peak PkWS. And can be distinguished.
  • the defect De2 at the depth of the boundary surface SB and the defect De3 at a position shallower than the boundary surface SB can be detected by the longitudinal wave WL.
  • the longitudinal wave generation laser irradiation position PTL and the longitudinal wave reception laser irradiation position PRL are changed in a direction orthogonal to the welding line We. Good.
  • FIG. 11 is a conceptual diagram showing a laser ultrasonic inspection method according to the present invention using both a transverse wave WT and a longitudinal wave WL.
  • the cross-sectional shape of the welded portion We of the present embodiment has a narrow cross-sectional shape with a small width ⁇ We and a large length D_We in the depth direction.
  • the ultrasonic detection method of the present embodiment detects the defect De3 at a position shallower than the boundary surface SB by the longitudinal wave WL and detects the defect De1 at a position deeper than the boundary surface SB. Detect with transverse wave ultrasonic WT.
  • the defect De2 at the depth of the boundary surface SB may be detected by either the longitudinal wave ultrasonic wave WL or the transverse wave ultrasonic wave WT, or by both the longitudinal wave ultrasonic wave WL and the transverse wave ultrasonic wave WT.
  • the longitudinal wave generation laser LaTL and the longitudinal wave reception laser LaRL are irradiated from the outside of the transverse wave generation laser LaTT and the transverse wave reception laser LaRT. That is, the transverse wave generation laser irradiation position PTT and the transverse wave reception laser irradiation position PRT are located on the inner side (closer to the welding line We) than the longitudinal wave generation laser irradiation position PTL and the longitudinal wave reception laser irradiation position PRL.
  • the longitudinal-wave generating laser irradiation position PTL and the longitudinal-wave receiving laser irradiation position PRL are located on the outer side (side away from the welding line We) with respect to the transverse-wave generating laser irradiation position PTT and the transverse-wave receiving laser irradiation position PRT. To be provided.
  • the longitudinal wave generating laser LaTL and the longitudinal wave receiving laser LaRL are irradiated at different positions in the direction orthogonal to the welding line We. Thereby, the defect De can be detected without receiving the influence (noise) of the surface wave.
  • both longitudinal wave WL and transverse wave (not shown) ultrasonic waves are generated at the irradiation position PTL of the longitudinal wave generation laser LaTL (see FIG. 8) by the longitudinal wave generation laser optical system 11B.
  • the longitudinal wave and the transverse wave generated by the irradiation of the longitudinal wave generating laser LaTL from the longitudinal wave generating laser optical system 11B are used to detect the defect De using the longitudinal wave WL. Detection is performed.
  • ultrasonic waves of both a longitudinal wave (not shown) and a transverse wave WT are generated at the irradiation position PTT of the transverse wave generation laser LaTT (see FIG.
  • the defect De is detected by using the transverse wave WT among the longitudinal wave and the transverse wave generated by the irradiation of the transverse laser generating laser LaTT from the transverse wave generating laser optical system 11C. .
  • the longitudinal wave WL is used in addition to the transverse wave WT by utilizing the directivity characteristic of the laser ultrasonic wave.
  • the transverse wave WT of the laser ultrasonic wave has directivity in a direction of about 30 degrees, and the transverse wave generation laser LaTT and the transverse wave reception laser LaRT are arranged at transmission / reception positions determined by the directivity (directivity angle 30 °) and the plate thickness of the first member 201. Irradiate.
  • the longitudinal wave WL of the laser ultrasonic wave has directivity in a direction of about 65 degrees, and the longitudinal wave generation laser LaTL and the longitudinal wave are at the transmission / reception position determined by the directivity (directivity angle 65 °) and the plate thickness of the first member 201.
  • the receiving laser LaRL is irradiated.
  • the position of the defect De3 shallower than the boundary surface SB can be detected based on the directivity angle (65 °) of the longitudinal wave WL. Further, the position of the defect De1 at a position deeper than the boundary surface SB can be detected based on the directivity angle (30 °) of the transverse ultrasonic wave WT.
  • the welded portion We that forms the weld bead constitutes a linear weld line, and the line width ⁇ We of the weld line We has a narrow cross-sectional shape that is smaller than the thickness dimension of the first member 201. We are formed.
  • the defect De existing in the upper and lower regions including the boundary surface SB can be reliably inspected.
  • the longitudinal wave ultrasonic wave WL propagates from the longitudinal wave generation laser irradiation position PTL to the defect De3 at a position shallower than the boundary surface SB without being reflected by the boundary surface SB.
  • the transverse wave ultrasonic wave WT propagates from the transverse wave generation laser irradiation position PTT to the defect De1 at a position deeper than the boundary surface SB without being reflected by the boundary surface SB. For this reason, it is not necessary to consider a complicated propagation path related to reflection, and the positions of the defects De1, De2, and De3 can be easily calculated.
  • FIG. 12 is a conceptual diagram showing an irradiation state of the longitudinal wave generating laser LaTL, the longitudinal wave receiving laser LaRL, the transverse wave generating laser LaTT, and the transverse wave receiving laser LaRT.
  • the longitudinal wave generation laser LaTL and the transverse wave generation laser LaTT are irradiated so as to form a linear focal point having a longitudinal direction in the direction along the welding line We, and the longitudinal wave reception laser LaRL and the transverse wave reception are obtained.
  • the laser LaRT is irradiated so as to form a point-like focus.
  • the longitudinal wave ultrasonic wave WL and the transverse wave ultrasonic wave WT propagate in a narrowed range with respect to the length of the line-shaped focal point in the direction along the welding line We.
  • the focal point arrangement described above allows the point-like focal point of the longitudinal wave receiving laser LaRL and the point-like focal point of the transverse wave receiving laser LaRT to be arranged close to each other, thereby making the apparatus compact. it can.
  • FIG. 13 is a diagram showing a manufacturing process of the high-pressure fuel supply pump 100 according to the present invention.
  • FIG. 13 only the process part which concerns on laser welding and ultrasonic inspection is shown, and the manufacturing method by the in-process inspection which performs ultrasonic inspection by the ultrasonic inspection apparatus 1 while performing laser welding by the laser welding apparatus 2 is shown. Yes.
  • the laser welding apparatus 2 performs laser welding on the high-pressure fuel supply pump 100, and at the same time, the ultrasonic inspection apparatus 1 detects a defect De generated in the laser welded portion We.
  • welding data is set based on the welding specification data.
  • the welding specification data data such as a welding position and laser power of laser welding are set in the control device 3.
  • the control device 3 controls the laser welding device 2 on the basis of the welding data to perform laser welding on the welding target A, and executes an inspection of the welded portion We by the ultrasonic inspection device 1. That is, the ultrasonic inspection process S3 is performed while performing the laser welding process S2. With the execution of the ultrasonic inspection step S3, the presence or absence of a defect De in the welded portion We is determined in step S4. When the presence of the defect De is determined, the welding data is corrected and the laser welding process S2 is repeated. The ultrasonic inspection process S3 is also executed when the laser welding process S2 is re-executed.
  • the determination of the presence or absence of the defect De in step S4 may be performed when the laser welding process S2 is completed, or may be performed during the execution of the laser welding process S2.
  • laser welding by the laser welding apparatus 2 and ultrasonic inspection by the ultrasonic inspection apparatus 1 can be performed at the same time. If there is a defect in laser welding, the defect is detected by the ultrasonic inspection apparatus 1. Immediate detection and re-welding can improve the yield of the high-pressure fuel supply pump 100 in the manufacturing process.
  • FIG. 14 is a cross-sectional view showing an embodiment of the high-pressure fuel pump 100 according to the present invention.
  • the high-pressure fuel supply pump 100 is a pump that supplies high pressure fuel pumped from a fuel tank by a feed pump (not shown) to the fuel injection valve.
  • the high-pressure fuel supply pump 100 is used for an internal combustion engine (engine) mounted on a vehicle.
  • engine the high-pressure fuel supply pump 100 will be referred to as a pump 100 and will be described.
  • a pressurizing chamber 107 is formed in the pump main body 101, and an upper end portion (tip portion) of the plunger 104 is inserted into the pressurizing chamber 107.
  • the plunger 104 reciprocates in the pressurizing chamber 107 to pressurize the fuel.
  • the pump body (pump housing) 101 has a mounting flange 102 for fixing to the engine.
  • the mounting flange 102 is welded to the pump body 101 by laser welding on the entire circumference.
  • a welding portion 301 between the mounting flange 102 and the pump main body 101 is referred to as a first welded portion.
  • the pump body 101 is provided with a suction valve mechanism 114 and a discharge valve mechanism 115.
  • the body 114c of the suction valve mechanism 114 is fixed to the pump body 101 by laser welding.
  • This weld location 302 is referred to as a second weld.
  • the outer periphery of the body 114c of the suction valve mechanism 114 is welded over the entire periphery.
  • a discharge joint 116 is provided on the downstream side of the discharge valve mechanism 115.
  • the discharge joint 116 is fixed to the pump body 101 by laser welding 303.
  • This weld location 303 is referred to as a third weld.
  • the outer periphery of the discharge joint 116 is welded over the entire circumference.
  • a damper cover 111 is attached to the top of the pump body 101.
  • the damper cover 111 is fixed to the pump body 101 by laser welding.
  • This weld location 304 is referred to as a fourth weld.
  • the fourth welded portion 304 is welded over the entire circumference.
  • a suction joint 112 is fixed to the damper cover 111 by laser welding.
  • This weld location 305 is referred to as a fifth weld.
  • the outer periphery of the suction joint 112 is welded over the perimeter.
  • the weld joints of the first welded portion 301, the second welded portion 302, and the third welded portion 303 have a butt weld structure. It is also possible to apply the in-process inspection process of this embodiment to these welds.
  • the laser 400 (LaW) is irradiated to the welding object surface perpendicularly.
  • the laser 400 (LaW) is irradiated with an inclination of ⁇ ° from the direction perpendicular to the surface of the welding object.
  • the weld joint of the fourth welded part 304 and the fifth welded part 305 has a lap weld structure, and the fourth welded part 304 and the fifth welded part 305 are welded by applying the in-process inspection process of this embodiment.
  • a laser 400 (LaW) is irradiated perpendicularly to the surface of the welding object.
  • the fuel leakage is not allowed in the pump 100.
  • the pump body 101, the body 114c of the suction valve mechanism 114, the discharge joint 116, the damper cover 111, and the suction joint 112 are components that constitute a fuel passage through which fuel flows.
  • the second welded portion 302 to the fifth welded portion 305 also serve as a fuel seal. For this reason, it is desirable to ensure a sufficient effective weld length for welding of the parts in which the fuel flow path is formed.
  • the pump 100 is used in a severe environment. By using a welding process having excellent robustness, the reliability of the pump 100 can be increased.
  • laser welding is performed by irradiating the laser LaW from the first member 201 side to the first member 201 and the second member 202 constituting the lap joint.
  • the ultrasonic inspection method for detecting the defect De in the welded part We with the ultrasonic wave UT by laser irradiation it operates with the following steps. (1) A step of irradiating the transverse wave generation laser LaTT to the transverse wave generation laser irradiation position PTT located on one side of the weld bead.
  • (1) and (3) are executed in conjunction with each other, and (2) and (4) are executed in conjunction with each other.
  • (5) is executed after (1) and (3), and (6) is executed after (2) and (4).
  • (7) is executed after (5), and (8) is executed after (6).
  • the ultrasonic inspection apparatus includes a laser welding part We in which laser welding is performed by irradiating a laser from the first member 201 side to the first member 201 and the second member 202 constituting the lap joint.
  • the defect De is detected by ultrasonic UT by laser irradiation.
  • the following configuration is provided. (1)
  • the transverse wave generation laser LaTT is irradiated to the transverse wave generation laser irradiation position PTT located on one side of the welding bead, and the one side away from the welding bead than the transverse wave generation laser irradiation position PTT.
  • the transverse wave receiving laser LaRT is irradiated to the transverse wave receiving laser irradiation position PRT located on the other side across the welding bead, and the other side away from the welding bead from the transverse wave receiving laser irradiation position PRT.
  • the receiving laser irradiation unit 12 that irradiates the longitudinal wave receiving laser LaRL to the longitudinal wave receiving laser irradiation position PRL positioned at (3)
  • a longitudinal wave interference measurement unit 13B that detects longitudinal wave ultrasonic waves WL generated by the thermoelastic mode by irradiation of the longitudinal wave generation laser LaTL with the longitudinal wave reception laser LaRL.
  • a transverse wave interference measurement unit 13C that detects a transverse wave ultrasonic wave WT generated by a thermoelastic mode by irradiation of the transverse wave generation laser LaTT with the transverse wave reception laser LaRT.
  • the defect De3 at a position shallower than the boundary surface SB between the first member 201 and the second member 202 is detected by the longitudinal wave WL and the defect De1 at a position deeper than the boundary surface SB. Is detected by a transverse ultrasonic WT.
  • the laser welding process S2 in which laser welding is performed by irradiating the first member 201 and the second member 202 constituting the lap joint from the first member 201 side.
  • an ultrasonic inspection step S3 for detecting a defect De in the laser welded portion We with an ultrasonic wave UT by laser irradiation.
  • the ultrasonic inspection step S3 includes the following steps. (1) A step of irradiating the transverse wave generating laser LaTT to the transverse wave generating laser irradiation position PTT located on one side of the weld bead. (2) A step of irradiating the longitudinal wave generation laser LaTL to the longitudinal wave generation laser irradiation position PTL located on the one side away from the welding bead than the transverse wave generation laser irradiation position PTT. (3) A step of irradiating the transverse wave receiving laser LaRT to the transverse wave receiving laser irradiation position PRT located on the other side with the weld bead interposed therebetween.
  • the manufacturing method of the high-pressure fuel supply pump which concerns on this invention performs the defect detection in the laser welding part We by ultrasonic inspection process S3, performing laser welding by laser welding process S2.
  • (1) and (3) are executed in conjunction with each other, and (2) and (4) are executed in conjunction with each other.
  • (5) is executed after (1) and (3), and (6) is executed after (2) and (4).
  • (7) is executed after (5), and (8) is executed after (6).
  • this invention is not limited to an above-described Example, Various modifications are included.
  • the above-described embodiments have been described in detail for easy understanding of the present invention, and are not necessarily limited to those having all the configurations.
  • 201 First member constituting lap joint
  • 202 Second member constituting lap joint
  • De1 Defect at position deeper than boundary surface SB
  • De3 Defect at position shallower than boundary surface SB
  • LaRL Reception for longitudinal wave Laser, LaRT ... Laser wave receiving laser, LaTL ... Longitudinal wave generating laser, LaTT ... Lateral wave generating laser, PRL ... Vertical wave receiving laser irradiation position, PRT ... Lateral wave receiving laser irradiation position, PTL ... Longitudinal wave generating laser Irradiation position, PTT ... Laser wave generation laser irradiation position, SB ... Boundary surface between the first member 201 and the second member 202, WL ... longitudinal wave ultrasonic wave, WT ... transverse wave ultrasonic wave.

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Abstract

L'objet de la présente invention est de détecter un défaut qui est présent au-dessus ou sous une interface de deux éléments dans une partie de soudage au laser d'un assemblage à recouvrement. À cet effet, un laser de génération d'ondes transversales (LaTT) et un laser de génération d'ondes longitudinales (LaTL) sont émis vers différents emplacements d'un côté d'une ligne de soudure (We). Un laser de réception d'ondes transversales (LaRT) et un laser de réception d'ondes longitudinales (LaRL) sont émis vers différents emplacements d'un autre côté de la ligne de soudure (We). Un défaut (De1) à un emplacement qui est plus profond qu'une interface (SB) entre un premier élément (201) et un second élément (202) est détecté par détection d'une onde ultrasonore transversale (WT) au moyen du laser de réception d'ondes transversales (LaRT). Un défaut (De3) à un emplacement qui est moins profond que l'interface (SB) est détecté par détection d'une onde ultrasonore longitudinale (WL) au moyen du laser de réception d'onde longitudinale (LaRL).
PCT/JP2019/003951 2018-03-20 2019-02-05 Procédé d'inspection à onde ultrasonore, dispositif d'inspection à onde ultrasonore et procédé de fabrication de pompe d'alimentation en carburant haute pression faisant appel à un procédé d'inspection à onde ultrasonore WO2019181243A1 (fr)

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JP2018052237A JP6934440B2 (ja) 2018-03-20 2018-03-20 超音波検査方法、超音波検査装置及び超音波検査方法を用いた高圧燃料供給ポンプの製造方法
JP2018-052237 2018-03-20

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CN111174894B (zh) * 2020-01-19 2021-06-04 山东省科学院激光研究所 一种激光超声横波声速测量方法

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JP2002213936A (ja) * 2000-11-16 2002-07-31 Kawasaki Steel Corp 材料厚さの非接触測定方法及び装置
JP2004191088A (ja) * 2002-12-09 2004-07-08 Kawasaki Heavy Ind Ltd 超音波探傷方法及びその装置
US20060260403A1 (en) * 2002-12-18 2006-11-23 Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V. Method for evaluating a weld joint formed during a welding process
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