Inspection vehicle for a turbine disk
View Patent ↗An inspection vehicle structured to inspect a portion of the turbine disk, preferably the blade attachment hubs, while the turbine disk is disposed within a turbine housing assembly is provided. A turbine disk is generally planar but includes a inner hub and an outer blade attachment hub. The inner hub is coupled to a shaft and the blade attachment hub provides a surface to which removable blades are attached. The area between the inner hub and outer blade attachment hub is substantially planar. The inner and blade attachment hubs are the “inspection areas” that the inspection vehicle is structured to inspect. The inspection vehicle travels over, and is magnetically coupled to the planar surface between the two hubs.
1. An inspection vehicle structured to inspect a turbine disk while said turbine disk is in situ, said inspection vehicle comprising:
a body structured to support a plurality of components;
a magnetic coupling assembly coupled to said body and structured to movably couple said body to said turbine disk;
a motion assembly structured to move said body over said turbine disk; and
an inspection assembly structured to inspect said turbine disk.
2. The inspection vehicle of claim 1 wherein:
said motion assembly includes a plurality of wheel assemblies, a plurality of wheel drive assemblies, and a plurality of turning assemblies;
each said wheel assembly rotatably coupled to said body and having a housing assembly and a wheel;
each turning assembly structured to rotate a wheel assembly relative to said body; and
each said drive assembly structured to rotate the associated wheel.
3. The inspection vehicle of claim 2 wherein:
each said wheel assembly wheel includes an outer surface; and
each said wheel outer diameter surface having a rigid portion extending about the circumference of said outer surface and a pliable portion extending about the circumference of said outer surface.
4. The inspection vehicle of claim 3 wherein:
said body has a wheel side;
said magnetic coupling assembly includes a plurality of magnets coupled to said body wheel side; and
wherein when said body is coupled to said turbine disk, each said magnet is operatively spaced from said turbine disk.
5. The inspection vehicle of claim 4 wherein at least one magnet in said plurality of magnets is coupled to said body by an adjustable coupling device whereby the spacing between said turbine disk and said at least one magnet coupled to said body by an adjustable coupling device may be altered.
6. The inspection vehicle of claim 3 wherein:
each said wheel assembly wheel has a body;
each said wheel assembly wheel body and outer surface rigid portion being steel; and
each said wheel assembly wheel outer surface pliable portion being rubber.
7. The inspection vehicle of claim 2 wherein:
each said wheel drive assembly includes a motor having an output shaft and a bevel gear assembly;
each said wheel drive assembly bevel gear assembly operatively engaging said wheel drive assembly motor output shaft and an associated said wheel;
whereby each said wheel rotates upon the actuation of the associated wheel drive assembly motor; and
whereby each wheel acts as a drive wheel.
8. The inspection vehicle of claim 2 wherein:
said inspection assembly includes a gimble frame assembly extending from said body and an inspection ultrasonic transducer;
said gimble frame assembly having a plurality of rigid members, said rigid members rotatably coupled to each other whereby said gimble frame assembly provides three axes of rotation;
said gimble frame assembly structured to support an inspection ultrasonic transducer; and
said inspection ultrasonic transducer coupled to said gimble frame assembly.
9. The inspection vehicle of claim 8 wherein:
said inspection ultrasonic transducer has an inspection face structured to extend generally parallel to the surface of said turbine disk;
said gimble frame assembly includes drive assembly structured to rotate said inspection ultrasonic transducer about an axis extending generally normal to said inspection ultrasonic transducer inspection face.
10. The inspection vehicle of claim 9 wherein:
said gimble assembly includes an axle extending generally perpendicular to the plane of said turbine disk, said axle having a gear thereon;
said gimble frame assembly drive assembly includes a motor, an output shaft and a worm gear;
said gimble drive assembly motor shaft extending generally parallel to the plane of said turbine disk;
said gimble drive assembly worm gear disposed on said gimble drive assembly output shaft;
said gimble drive assembly worm gear operatively engaging said axle gear; and
said inspection ultrasonic transducer fixed to said axle.
11. The inspection vehicle of claim 8 wherein said gimble frame assembly includes a spring structured to bias said inspection ultrasonic transducer inspection face towards the surface of said turbine disk.
12. An inspection vehicle structured to inspect a turbine disk while said turbine disk is in situ, said inspection vehicle comprising:
a movable body structured to support a plurality of components;
a magnetic coupling assembly coupled to said body and structured to movably couple said body to said turbine disk;
a motion assembly structured to move said body over said turbine disk; and
an inspection assembly structured to inspect said turbine disk.
13. The inspection vehicle of claim 12 wherein:
said motion assembly includes a plurality of wheel assemblies and a plurality of turning assemblies;
each said wheel assembly rotatably coupled to said body; and
each turning assembly structured to rotate a wheel assembly relative to said body.
14. The inspection vehicle of claim 12 wherein:
said motion assembly includes a plurality of wheel drive assemblies;
each said wheel assembly having a housing assembly and a wheel; and
each said drive assembly structured to rotate the associated wheel.
15. The inspection vehicle of claim 14 wherein:
said body has a wheel side;
said magnetic coupling assembly includes a plurality of magnets coupled to said body wheel side; and
wherein when said body is coupled to said turbine disk, each said magnet is operatively spaced from said turbine disk.
16. The inspection vehicle of claim 15 wherein at least one magnet in said plurality of magnets is coupled to said body by an adjustable coupling device whereby the spacing between said turbine disk and said at least one magnet coupled to said body by an adjustable coupling device may be altered.
17. An inspection vehicle structured to inspect a turbine disk while said turbine disk is in situ, said inspection vehicle comprising:
a body structured to support a plurality of components;
a magnetic coupling assembly coupled to said body and structured to movably couple said body to said turbine disk;
a motion assembly structured to move said body over said turbine disk;
said motion assembly includes a plurality of wheel assemblies and a plurality of turning assemblies;
each said wheel assembly rotatably coupled to said body;
each turning assembly structured to rotate a wheel assembly relative to said body; and
an inspection assembly structured to inspect said turbine disk.
18. The inspection vehicle of claim 17 wherein:
said body has a wheel side;
said magnetic coupling assembly includes a plurality of magnets coupled to said body wheel side; and
wherein when said body is coupled to said turbine disk, each said magnet is operatively spaced from said turbine disk.
19. The inspection vehicle of claim 18 wherein at least one magnet in said plurality of magnets is coupled to said body by an adjustable coupling device whereby the spacing between said turbine disk and said at least one magnet coupled to said body by an adjustable coupling device may be altered.
20. The inspection vehicle of claim 17 wherein:
said inspection assembly includes a gimble frame assembly extending from said body and an inspection ultrasonic transducer;
said gimble frame assembly having a plurality of rigid members, said rigid members rotatably coupled to each other whereby said gimble frame assembly provides three axes of rotation;
said gimble frame assembly structured to support an inspection ultrasonic transducer; and
said inspection ultrasonic transducer coupled to said gimble frame assembly.