Apparatus for searching for and detecting defects in parts by endoscopy
View Patent ↗Apparatus for searching for and detecting defects on parts that are substantially inaccessible, being located behind a wall, the apparatus comprising a first endoscope for illumination in visible light and for observation, the first endoscope and pipes for feeding and spraying penetration test substances being housed together in a rod which can be passed through an orifice in the wall in order to examine a part, the apparatus further comprising a second endoscope independent of the first endoscope and the rod for illuminating in ultraviolet light and for observing the portion of the part that has been treated by the penetration test substances.
1. A method of detecting defects in a turbojet part by endoscopy comprising:
providing a rod with a first diameter and including
at least one pipe, and
a first endoscope including a visible light guide received in the rod and a first image transmission assembly received in the rod, the first endoscope being free of any means for producing ultraviolet light;
providing a second endoscope with a second diameter, the second endoscope being free of any pipes configured to feed gas or fluid and free of any means for producing visible light, the second endoscope including an ultraviolet light guide and a second image transmission assembly;
inserting the rod through an orifice in a wall of the turbojet;
after inserting the rod through the orifice and while the first endoscope is disposed within the orifice, exposing the turbojet part to visible light transmitted via the visible light guide and produced by a dedicated visible light source, and applying a penetration test substance to a surface of the turbojet part by sending the penetration test substance through the at least one pipe;
withdrawing the rod from the orifice after applying the penetration test substance to the turbojet part;
inserting the second endoscope through the orifice after withdrawing the rod;
exposing the turbojet part to ultraviolet light with the ultraviolet light guide while the second endoscope is in the orifice; and
viewing the turbojet part exposed to ultraviolet light through the second image transmission assembly while the second endoscope is in the orifice.
2. The method according to claim 1 , wherein the turbojet is mounted on an airplane.
3. The method according to claim 1 , further comprising configuring the second diameter to be substantially equal to the first diameter.
4. The method according to claim 3 , further comprising configuring the first diameter to be about 8 mm.
5. The method according to claim 1 , further comprising configuring the orifice in the wall of the turbojet to have a diameter of about 9 mm.
6. The method according to claim 1 , further comprising reflecting light received from the turbojet part with a prism that is included in the first image transmission assembly.
7. The method according to claim 1 , further comprising reflecting light received from the turbojet part with a prism that is included in the second image transmission assembly.
8. The method according to claim 1 , wherein the turbojet part is not exposed to visible light via the second endoscope during said exposing the turbojet part to ultraviolet light with the ultraviolet light guide while the second endoscope is in the orifice.
9. The method according to claim 1 , wherein the applying a penetration test substance includes applying a fluorescent liquid.
10. The method according to claim 9 , wherein the applying a penetration test substance includes applying a washing liquid after applying the fluorescent liquid.
11. The method according to claim 9 , wherein the applying a penetration test substance includes applying a developer powder that reveals the presence of penetrating test substance that has infiltrated into a surface discontinuity in the turbojet part.
12. The method according to claim 1 , wherein the at least one pipe includes a first pipe through which air is supplied, a second pipe through which liquid is supplied, and a third pipe through which powder is supplied.
13. A method of detecting defects in a turbojet part by endoscopy comprising:
inserting a first endoscope through an orifice in a wall of the turbojet, the first endoscope being free of any means for producing ultraviolet light;
while the first endoscope is disposed within the orifice, exposing the turbojet part to visible light transmitted via a visible light guide while the first endoscope is coupled to a dedicated visible light source;
while the first endoscope is disposed within the orifice, applying a penetration test substance to a surface of the turbojet part by sending the penetration test substance through at least one pipe coupled to the first endoscope;
withdrawing the first endoscope from the orifice after applying the penetration test substance;
inserting a second endoscope, free of any pipe for depositing substances on the turbojet part and free of any means for producing visible light, through the orifice after withdrawing the first endoscope;
exposing the turbojet part to ultraviolet light with an ultraviolet light guide while the second endoscope is in the orifice and is coupled to a dedicated ultraviolet light source; and
viewing the turbojet part exposed to ultraviolet light through an image transmission assembly while the second endoscope is in the orifice.
14. The method of detecting defects in a turbojet part according to claim 13 , further comprising reflecting an image of the turbojet part with a prism while the turbojet part is exposed to ultraviolet light; and
viewing the reflected image of the turbojet part after the image is reflected with the prism.
15. The method according to claim 13 , wherein the turbojet is mounted on an airplane.
16. The method according to claim 13 , further comprising configuring the orifice in the wall of the turbojet to have a diameter of about 9 mm.
17. The method according to claim 13 , further comprising
reflecting light received from the turbojet part with a prism that is included in the first endoscope; and
viewing the reflected image.
18. The method according to claim 13 , further comprising
reflecting light received from the turbojet part with a prism that is included in the second endoscope; and
viewing the reflected image.
19. The method according to claim 13 , wherein the applying a penetration test substance includes applying a fluorescent liquid.
20. The method according to claim 19 , wherein the applying a penetration test substance includes applying a washing liquid after applying the fluorescent liquid.
21. The method according to claim 19 , wherein the applying a penetration test substance includes applying a developer powder that reveals the presence of fluorescent liquid that has infiltrated into a surface discontinuity in the turbojet part.
22. The method according to claim 13 , further comprising configuring the first and second endoscopes to each have an outside diameter of about 9 mm.
23. A method of detecting defects in a turbojet by endoscopy including inserting first and second endoscopes in sequence, one after another, through an orifice in a wall of the turbojet, the method comprising:
inserting a first endoscope through an orifice in a wall of the turbojet, the first endoscope being free of any means for producing ultraviolet light;
while the first endoscope is disposed within the orifice, exposing the turbojet part to visible light transmitted via a visible light guide while the first endoscope is coupled to a dedicated visible light source;
while the first endoscope is disposed within the orifice, applying a penetration test substance to a surface of the turbojet part by sending the penetration test substance through at least one pipe coupled to the first endoscope;
withdrawing the first endoscope from the orifice after applying the penetration test substance;
inserting a second endoscope, free of any pipe for depositing substances on the turbojet part and free of any means for producing visible light, through the orifice after withdrawing the first endoscope;
exposing the turbojet part to ultraviolet light with an ultraviolet light guide while the second endoscope is in the orifice and is coupled to a dedicated ultraviolet light source; and
viewing the turbojet part exposed to ultraviolet light through an image transmission assembly while the second endoscope is in the orifice.