US2565725A - Supersonic inspection for flaws lying near the surface of a part - Google Patents
Supersonic inspection for flaws lying near the surface of a part Download PDFInfo
- Publication number
- US2565725A US2565725A US671349A US67134946A US2565725A US 2565725 A US2565725 A US 2565725A US 671349 A US671349 A US 671349A US 67134946 A US67134946 A US 67134946A US 2565725 A US2565725 A US 2565725A
- Authority
- US
- United States
- Prior art keywords
- reflections
- wave
- flaws
- subsidiary
- supersonic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating 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
- G01N29/22—Details, e.g. general constructional or apparatus details
- G01N29/28—Details, e.g. general constructional or apparatus details providing acoustic coupling, e.g. water
Definitions
- This invention relates to the supersonic inspection of materials particularly in those cases where the flaw to be detected lies near the surface of the part to be inspected.
- a supersonic inspection device which consists in sending, by means such as an electro-acoustic transducer, including a quartz crystal, at short supersonic wave traininto the part to be inspected and detecting, by a similar electro-acoustic transducer, the reflection of said wave train from any flaws which may be present in the interior of the solid.
- some difficulty is experienced in those cases where the flaws to be detected lie closer to the sending crystal than /2.
- This desired degree is such increase of time that the reflection from the defeet will be sufliciently spaced in time from the transmission of the wave train to permit the detecting apparatus to recover from the shock of transmission.
- Fig. 1 is a front elevation illustrating one form of intermediate member interposed between a wave transmitting element and the solid part under test.
- Fig. 2 is a view similar to Fig.1 but showing a modified form of intermediate member.
- Fig. 3 is a view similar to Figs. 1 and 2 showing still another modifiedform of intermediate member.
- Fig. 4 is a diagrammatic view illustrating the nature of the problem'which this invention seeks to solve.
- a solid part I0 for flaws such as the one indicated at 'H which may lie adjacent to surface l2 of the solid part.
- a piezo-electric crystal 20 would be applied to surface l2 and a supersonic wave train or pulse would be transmitted into the solid in.
- the receiver may be another crystal such as 20 or the same crystal may be employed for both sending and receiving. Therefore, if flaws lying adjacent the surface H are to be tested, some method and means must be provided for increasing the time interval which flaws such as flaw ll located adjacent the surface of the solid trough through which the transmitted waves enter.
- Fig. 1 wherein the sides of the intermediate member l6 are so formed as to provide a multiplicity of differentreflecting surfaces so that the subsidiary reflections.
- Fig. 4 which returns to the receiving element, has a wide'multiplicity of interfering paths, tending to reduce the subsidiary reflections and thus render it improbable that a sufllcient number of subsidiary reflections willbe received by the receiving element to offer any obscuring effect on the reflections received from the defect.
- the form assumed by the intermediate element ll in Fig. l is that of a wavy or corrugated surface which will entail an infinite number of different reflecting angles so that the subsidiary reflections will be dispersed.
- the intermediate element It has its sides formed in saw-toothed arrangement to provide a multiplicity of reflecting surfaces whose angle of inclination is such as to direct subsidiary reflections away from the surface l2 of the part III.
- FIG. 3 still another form of intermediate member 16'" is disclosed wherein the member is formed with a zigzag contour to provide a multiplicity of reflecting faces of different angular positioning.
- the result in all of these forms is the same, namely, to disperse the subsidiary reflections instead of concentrating them in a beam which can obscure reflections from a defect.
- the shear wave thus generated in these subsidiaries travels only about half as fast as the longitudinal wave, the total time consumed I by the subsidiary wave from the time it is generated until it returns to crystal 20 is considerably increased relative to the main longitudinal beam shown in-the full lines 36 since the latter goes straight down and back.
- the longer time consumed by the subsidiary reflection may pro- 'duce an indication which interferes with the indication from the flaw.
- the time of travel of the subsidiary reflection may be sub-
- a system for testing material by supersonic waves in which supersonic wave trains are transmitted from an electro acoustic transducer toward said material and reflections of the wave trains are received by said transducer, characterized by means for increasing the time of travel of the .wave trai'hs between the transducer and the material, said means comprising an intermediate wave-conducting member for transmitting wave energy between the transducer and the material, said member having corrugated side walls to reflect at a plurality of angles those supersonic waves within the member which strike said walls, each of said corrugations having its linear dimensions greater than the wave length of said supersonic waves.
Description
1951 J. R. FREDERICK ETAL 2,565,725
' SUPERSONIC INSPECTION FOR FLAWS LYING NEAR V THE SURFACE OF A PART Filed lay 21, 1946 I F2 16' I 40 I k INVENTORS' J54 /AN 1? FEDER/Ck flax .014. was TONE ATTORNEY Patented Aug. 28, 1951 SUPERSONIC INSPECTION FOR FLAWS LYING NEAR THE SURFACE OF A PART Julian R. Frederick, Ann Arbor, Mich., and Floyd A. Firestone, Washington, D. (J., assignors to Sperry Products, Inc., Hoboken, N. J a corporation of New York Application May 21, 1946, Serial No. 621,349
This invention relates to the supersonic inspection of materials particularly in those cases where the flaw to be detected lies near the surface of the part to be inspected. In the patent to Firestone, No. 2,280,226, granted April 21, 1942, there is disclosed one form of supersonic inspection device which consists in sending, by means such as an electro-acoustic transducer, including a quartz crystal, at short supersonic wave traininto the part to be inspected and detecting, by a similar electro-acoustic transducer, the reflection of said wave train from any flaws which may be present in the interior of the solid. In the form of the invention disclosed in said patent, some difficulty is experienced in those cases where the flaws to be detected lie closer to the sending crystal than /2. The reason for thisdifliculty lies in the fact that the waves reflected back .to the sending point by a defect lying near the surface 2 Claims. (CI. 7367) member of substantial width so that the subsidiary reflections from the sides of the interposed member would have a considerably longer path to travel and, therefore, would arrive sufliciently later than reflections from a defect within the part under test so that distinction could be made the wave train.
, close to the surface of the solid part is increased to the desired degree. This desired degree is such increase of time that the reflection from the defeet will be sufliciently spaced in time from the transmission of the wave train to permit the detecting apparatus to recover from the shock of transmission.
When it is attempted to interpose a member as described above for the purpose of increasing the time interval between transmission of the pulse and reception of reflections from a defect within the object of the test,.it is found that difiiculty arises due to the fact that certain of the waves strike the sides of the interposed memher and eventually, by a series of reflections find their way back to the receiving element. These subsidiary reflections frequently arrive while the reflections from reflecting surfaces within the solid part are still being received and thus tend to obscure reflections which may be an indication of the presence of a defect within the material. In said co-pending application it was sought to overcome this difiiculty by making the interposed between the defect and the subsidiary reflections. However, it is not always feasible to provide an intermediate member of such substantial width and usually it is desirable to have the interposed member of minimum width and usually no greater width than the crystal transducer.
It is one of the principal objects of this invention, therefore, to provide an interposed member between the sending crystal and the part under test which may be of no greater width than the crystal transducer and which will, nevertheless, not deliver to the receiving element any substantial quantity of subsidiary reflections which can interfere with reflections from a defect within the part under test.
Further objects and advantages of this invention will become apparent in the following detailed description thereof.
In the accompanying drawings,
Fig. 1 is a front elevation illustrating one form of intermediate member interposed between a wave transmitting element and the solid part under test.
Fig. 2 is a view similar to Fig.1 but showing a modified form of intermediate member.
Fig. 3 is a view similar to Figs. 1 and 2 showing still another modifiedform of intermediate member.
Fig. 4 is a diagrammatic view illustrating the nature of the problem'which this invention seeks to solve.
Referring first to Fig. 1, it is desired to test a solid part I0 for flaws such as the one indicated at 'H which may lie adjacent to surface l2 of the solid part. In applying the invention shown in the Firestone Patent No. 2,280,226 a piezo-electric crystal 20 would be applied to surface l2 and a supersonic wave train or pulse would be transmitted into the solid in. Such an arrangement, however, -would cause the wave train to be reflected back from the flaw II in such short time interval that the transmission of the wave train will not have been completed by the time the reflected wave train has reached the receiver. The receiver may be another crystal such as 20 or the same crystal may be employed for both sending and receiving. Therefore, if flaws lying adjacent the surface H are to be tested, some method and means must be provided for increasing the time interval which flaws such as flaw ll located adjacent the surface of the solid trough through which the transmitted waves enter. p
Onesolution of this problem is disclosed in the said co-pending application of Firestone wherein there isv interposed between the surface I! and the sending crystal iii an intermediate member of some material which conducts supersonic waves. It will now be apparent that the wave I train generated by sending crystal Ill must traverse the intermediate member before entering the solid l0 and before reaching the flaw H. The length of the intermediate member is so selected that the time interval which elapses between the sending of a wave train and the receiving of reflections thereof from the flaw II will be sufflcient to permit the transmitted wave train to be completed before reflections from flaw H are.
.will radiate longitudinally as indicated by the dash lines and on striking the side walls of the I interposed member i6 will give rise to a shear wave .40 which on striking the opposite wall is again transformed in part into a longitudinal form of which is shown in Fig. 1 wherein the sides of the intermediate member l6 are so formed as to provide a multiplicity of differentreflecting surfaces so that the subsidiary reflections. instead of having a well defined path as disclosed in Fig. 4, which returns to the receiving element, has a wide'multiplicity of interfering paths, tending to reduce the subsidiary reflections and thus render it improbable that a sufllcient number of subsidiary reflections willbe received by the receiving element to offer any obscuring effect on the reflections received from the defect. The form assumed by the intermediate element ll in Fig. l is that of a wavy or corrugated surface which will entail an infinite number of different reflecting angles so that the subsidiary reflections will be dispersed.
In Fig. 2 the intermediate element It" has its sides formed in saw-toothed arrangement to provide a multiplicity of reflecting surfaces whose angle of inclination is such as to direct subsidiary reflections away from the surface l2 of the part III.
In Fig. 3 still another form of intermediate member 16'" is disclosed wherein the member is formed with a zigzag contour to provide a multiplicity of reflecting faces of different angular positioning. The result in all of these forms is the same, namely, to disperse the subsidiary reflections instead of concentrating them in a beam which can obscure reflections from a defect.
wave 4| which strikes the surface I! of the solid part l0 and is again reflected back in the form of a beam 42 to the crystal 20. The reflections shown by the dash line represent only one subsidiary reflection and other subsidiary reflections will arise from shear waves having travelled across the member I6 two, three or more times.
Since the shear wave thus generated in these subsidiaries travels only about half as fast as the longitudinal wave, the total time consumed I by the subsidiary wave from the time it is generated until it returns to crystal 20 is considerably increased relative to the main longitudinal beam shown in-the full lines 36 since the latter goes straight down and back. The longer time consumed by the subsidiary reflection may pro- 'duce an indication which interferes with the indication from the flaw. In'other words, the time of travel of the subsidiary reflection may be sub-,
stantially' the same as the time of travel of the main beam from the crystal-20 to the flaw and return.
In said co-pending application, one solution for this difliculty is disclosed, i. e. by making the lateral dimension of the intermediate member l6 large. .In this way the time interval required by the subsidiary reflection to return to the crystal 20 is increased suiflciently so that said sub- Theforegoing description of the invention is merely illustrative and changes may be made within the scope of the appended claims.
Having described our invention, what we claim and desire to secure by Letters Patent is:
1. In, a system for testing material by supersonic waves, in which supersonic wave trains are transmitted from an electro acoustic transducer toward said material and reflections of the wave trains are received by said transducer, characterized by means for increasing the time of travel of the .wave trai'hs between the transducer and the material, said means comprising an intermediate wave-conducting member for transmitting wave energy between the transducer and the material, said member having corrugated side walls to reflect at a plurality of angles those supersonic waves within the member which strike said walls, each of said corrugations having its linear dimensions greater than the wave length of said supersonic waves.
2. In a system for testing material by supersonic waves. in which supersonic wave trains are transmitted from an electro-acoustic transducer toward said material and reflections of the wave trains are received by said transducer, characterized by means for increasing the time of travel of the waveftrains between the transducer and the material, said means comprising an intermediate wave-conducting member for trans- 'mitting wave energy between the transducer and the material, said member having saw-tooth side walls to reflect at a plurality of. angles those supersonic waves within the member which strike said walls, each of said saw teeth having its linear dimensions greater than the wave length of said supersonic waves.
. JULIAN R. FREDERICK.
FLOYD A. FIRESTONE.
Noreferences cited.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US671349A US2565725A (en) | 1946-05-21 | 1946-05-21 | Supersonic inspection for flaws lying near the surface of a part |
GB11848/47A GB633144A (en) | 1946-05-21 | 1947-05-02 | Improvements in or relating to supersonic inspection apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US671349A US2565725A (en) | 1946-05-21 | 1946-05-21 | Supersonic inspection for flaws lying near the surface of a part |
Publications (1)
Publication Number | Publication Date |
---|---|
US2565725A true US2565725A (en) | 1951-08-28 |
Family
ID=24694150
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US671349A Expired - Lifetime US2565725A (en) | 1946-05-21 | 1946-05-21 | Supersonic inspection for flaws lying near the surface of a part |
Country Status (2)
Country | Link |
---|---|
US (1) | US2565725A (en) |
GB (1) | GB633144A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2779880A (en) * | 1951-03-19 | 1957-01-29 | Acec | Ultra-sonic wave transducers |
US2787158A (en) * | 1953-07-23 | 1957-04-02 | Sperry Prod Inc | Static scanning device in ultrasonic inspection of materials |
US2803129A (en) * | 1951-05-28 | 1957-08-20 | Council Scient Ind Res | Apparatus for testing of elastic materials |
US2913680A (en) * | 1955-08-18 | 1959-11-17 | Sperry Rand Corp | Acoustic delay lines |
US2920294A (en) * | 1954-10-14 | 1960-01-05 | Raytheon Co | Sonic delay lines |
US2922966A (en) * | 1953-11-30 | 1960-01-26 | Marconi Wireless Telegraph Co | Ultrasonic delay devices |
US2998723A (en) * | 1956-06-15 | 1961-09-05 | Acoustica Associates Inc | Sonic wave conductor |
US3070761A (en) * | 1953-05-07 | 1962-12-25 | Smith & Sons Ltd S | Ultrasonic delay lines |
US3133258A (en) * | 1960-10-21 | 1964-05-12 | Bell Telephone Labor Inc | Ultrasonic strip delay line |
US3177381A (en) * | 1962-03-22 | 1965-04-06 | Shell Oil Co | Apparatus for ultrasonic wall thickness measurements |
US3898840A (en) * | 1974-01-30 | 1975-08-12 | Automation Ind Inc | Multi-frequency ultrasonic search unit |
US4297608A (en) * | 1979-05-10 | 1981-10-27 | Danfoss A/S | Measuring equipment for acoustic determination of the specific gravity of liquids |
US5828274A (en) * | 1996-05-28 | 1998-10-27 | National Research Council Of Canada | Clad ultrasonic waveguides with reduced trailing echoes |
US20090314088A1 (en) * | 2008-06-09 | 2009-12-24 | Materials And Sensors Technologies, Inc. | Differential Ultrasonic Waveguide Cure Monitoring Probe |
-
1946
- 1946-05-21 US US671349A patent/US2565725A/en not_active Expired - Lifetime
-
1947
- 1947-05-02 GB GB11848/47A patent/GB633144A/en not_active Expired
Non-Patent Citations (1)
Title |
---|
None * |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2779880A (en) * | 1951-03-19 | 1957-01-29 | Acec | Ultra-sonic wave transducers |
US2803129A (en) * | 1951-05-28 | 1957-08-20 | Council Scient Ind Res | Apparatus for testing of elastic materials |
US3070761A (en) * | 1953-05-07 | 1962-12-25 | Smith & Sons Ltd S | Ultrasonic delay lines |
US2787158A (en) * | 1953-07-23 | 1957-04-02 | Sperry Prod Inc | Static scanning device in ultrasonic inspection of materials |
US2922966A (en) * | 1953-11-30 | 1960-01-26 | Marconi Wireless Telegraph Co | Ultrasonic delay devices |
US2920294A (en) * | 1954-10-14 | 1960-01-05 | Raytheon Co | Sonic delay lines |
US2913680A (en) * | 1955-08-18 | 1959-11-17 | Sperry Rand Corp | Acoustic delay lines |
US2998723A (en) * | 1956-06-15 | 1961-09-05 | Acoustica Associates Inc | Sonic wave conductor |
US3133258A (en) * | 1960-10-21 | 1964-05-12 | Bell Telephone Labor Inc | Ultrasonic strip delay line |
US3177381A (en) * | 1962-03-22 | 1965-04-06 | Shell Oil Co | Apparatus for ultrasonic wall thickness measurements |
US3898840A (en) * | 1974-01-30 | 1975-08-12 | Automation Ind Inc | Multi-frequency ultrasonic search unit |
US4297608A (en) * | 1979-05-10 | 1981-10-27 | Danfoss A/S | Measuring equipment for acoustic determination of the specific gravity of liquids |
US5828274A (en) * | 1996-05-28 | 1998-10-27 | National Research Council Of Canada | Clad ultrasonic waveguides with reduced trailing echoes |
US20090314088A1 (en) * | 2008-06-09 | 2009-12-24 | Materials And Sensors Technologies, Inc. | Differential Ultrasonic Waveguide Cure Monitoring Probe |
US8291744B2 (en) * | 2008-06-09 | 2012-10-23 | Materials And Sensors Technologies, Inc. | Differential ultrasonic waveguide cure monitoring probe |
US9297789B2 (en) | 2008-06-09 | 2016-03-29 | Materials And Sensors Technologies, Inc. | Differential ultrasonic waveguide cure monitoring probe |
Also Published As
Publication number | Publication date |
---|---|
GB633144A (en) | 1949-12-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2565725A (en) | Supersonic inspection for flaws lying near the surface of a part | |
US2527986A (en) | Supersonic testing | |
US2592134A (en) | Method of supersonic inspection | |
US2467301A (en) | Supersonic inspection for flaws lying near the surface of apart | |
KR870000590A (en) | Defect detection method and apparatus of metal | |
US4022055A (en) | Pulse-echo method and system for testing wall thicknesses | |
US2912854A (en) | Ultrasonic surface testing device | |
WO1996036874A1 (en) | Ultrasonic inspection | |
US2525861A (en) | Delay system for supersonic inspection | |
US2592135A (en) | Inspecting solid parts by supersonic shear waves | |
US4641531A (en) | Ultrasonic inspection apparatus and method for locating multiple defects in eccentric wall tubular goods | |
US2649550A (en) | Reflection absorbing ultrasonic wedge | |
US2937522A (en) | Ultrasonic rail weld scanner | |
US2458581A (en) | Supersonic inspection | |
US3592052A (en) | Ultrasonic crack depth measurement | |
US5677489A (en) | Distributed structural characteristic detection system using a unidirectional acoustic waveguide | |
US3192418A (en) | Ultrasonic transducers | |
WO2019150953A1 (en) | Ultrasonic probe | |
US11054399B2 (en) | Inspection method | |
US2683821A (en) | Unwanted reflection absorbing shear wave transducer | |
US3218845A (en) | Ultrasonic inspection method for inaccessible pipe and tubing | |
RU172992U1 (en) | DEVICE FOR ULTRASONIC PIPE END CONTROL | |
SU771540A1 (en) | Method of ultrasonic testing of joining of metallic articles with non-metallic coating | |
US3433059A (en) | Coupling member for ultrasonic scanning device | |
JPH08313496A (en) | Ultrasonic probe |