Patent Number: 052251489
Section: claims

1. Method for checking a thickness and cohesion of an interface of a duplex tube comprising a tubular core made from a first alloy and covered with a cladding layer made from a second alloy, a base metal of said second alloy being identical to a base metal of said first alloy, said method comprising successive checking operations in various zones around a circumference or along a length of said duplex tube, each operation comprising the steps of: (a) emitting ultrasonic waves in substantially radial directions from outside to inside said tube in said cladding layer and said core of said tube;  (b) detecting reflected ultrasonic waves which have been reflected by surfaces of said tube, by an interface between said core and said cladding layer of said tube and by any flaws at said interface or which are transmitted by said cladding layer;  (c) measuring propagation times of said ultrasonic waves radially of said tube along a total thickness of said duplex tube comprising said core and said cladding layer;  (d) determining amplitudes and shape of the reflected ultrasonic waves;  (e) subjecting said tube from an outer surface of said tube to a magnetic induction created by a multifrequency sinusoidal current;  (f) measuring at least one of a phase and an amplitude of eddy currents induced in said tube;  (g) calculating therefrom the thickness of said cladding layer;  (h) calculating the total thickness of said tube from the measurements of propagation times of said ultrasonic waves and the thickness of said cladding layer; and  (i) determining the cohesion of said interface of said tube by analyzing an amplitude and shape of the reflected waves.  e.sub.p represents the thickness of said cladding layer, measured by eddy currents,  V.sub.p represents the speed of the ultrasonic waves in said cladding layer,  V.sub.a represents the speed of the ultrasonic waves in the material constituting said core of said tube, and  .delta.t represents the propagation time of the ultrasonic waves in the total thickness of said tube. 2. Method according to claim 1, wherein the frequency of said ultrasonic waves lies between 10 and 20 MHz. 3. Method according to claim 1, wherein said multifrequency sinusoidal current has a main frequency which is determined so as to optimize a sensitivity to variations in thickness of said cladding layer and to minimize variations in signals corresponding to the induced currents caused by variations of an air gap, between said tube and an eddy current probe, subjecting said tube to a magnetic induction created by the multifrequency sinusoidal current, and at least one complementary second frequency which is sensitive to a variation in conductivity of at least one of the alloys constituting said core of said cladding layer of said tube and comparatively less sensitive to variations in thickness of the material of said core or of said cladding. 4. Method according to claim 3, wherein the multifrequency sinusoidal current has a complementary second frequency sensitive to a mean variation in conductivity of the alloys constituting said core and said cladding layer of said tube, and comparatively less sensitive to variations in thickness of said core and of said cladding layer. 5. Method according to claim 3, wherein said multifrequency sinusoidal current has first and second complementary second frequencies, said first frequency being sensitive to a variation in conductivity of the alloy constituting said core of said tube and comparatively less sensitive to variations in conductivity of the alloy constituting said cladding layer and to the variations in thickness of said core and of said cladding layer, and said second frequency being sensitive only to variations in the conductivity of the alloy constituting said cladding layer. 6. Method according to claim 3, wherein said multifrequency sinusoidal current has a complementary frequency sensitive to variations in said air gap. 7. Method according to claim 1, wherein the total thickness e.sub.g of the wall of the duplex tube is determined from the formula: EQU e.sub.g =e.sub.p +(.delta.t-e.sub.p /V.sub.p).times.V.sub.a 8. Method according to claim 1, wherein the cohesion of said tube at said interface is determined by detecting flaws by transmitting ultrasonic waves through said cladding layer and said interface, the presence of a flaw at said interface being manifested by a widening of ultrasonic waves reflected on said outer surface of said tube and at said interface, and by weakening or disappearance of a bottom echo obtained by reflection of ultrasonic waves on the inner wall of said tube.