The present invention relates generally to a miniature robotic device and more particularly relates to a miniature robotic device for performing in-situ ultrasonic inspections of a generator field.
The visual inspection of a generator field and stator should be performed on a periodic basis. Conventional generator/stator inspection and testing procedures typically require the complete disassembly of the stator and the removal of the generator field from the stator before any inspections or tests can be performed on the unit. The cost of the disassembly and the removal of the field, the time it takes for this process, and the dangers of field removal have led to the occasional omission of the generator and stator examinations from outage schedules.
In-situ inspections of generators have been performed employing poles, trolleys, and field turning techniques. These procedures have not accomplished the inspection task in a satisfactory manner.
Miniature air gap inspection crawlers are disclosed in commonly owned U.S. Pat. Nos. 5,650,579 and 6,100,711, the contents of which are hereby incorporated by reference. These crawlers are designed to pass through the radial air gap between the core iron and the retaining ring for in-situ inspection of the field and stator core.
Video cameras and other inspection tools attached to the crawler may be used to perform generator field and stator core inspections. For example, a high-resolution video camera provides the operator with a clear view of the stator core laminations, stator wedges, field wedges, and the in-board ends of the retaining rings. The device thus provides detection capability for loose stator wedges, vibration bar sparking, core lamination damage due to foreign objects, motoring and hot spots, field wedge arcing, and surface heating damage. Through the generator in-situ inspection, information is gathered on the condition of the generator that can help determine if field removal is necessary.
Although these known devices are adequate for visual inspection, these visual systems cannot detect internal defects such as cracks or pits in the field teeth. Rather, such cracks can only be found by ultrasonic inspection. Currently, however, the rotor must be pulled out of the stator before an ultrasonic inspection can be performed.
There is a desire therefore for a device and method to perform in-situ ultrasonic inspection of a generator stator and field. The device preferably should be sized to pass through the radial air gap.
The present application thus describes an inspection head for an air gap inspection device. The inspection head may include a pair of expandable shoes, an inspection device attached to the pair of shoes, and a transducer assembly attached to one of the pair of shoes.
The transducer assembly may include an ultrasonic transducer. The ultrasonic transducer may be attached to the base by a number of arms. The arms may include a lever arm and a straight arm. The transducer assembly also may include a motor thread connected to the lever arm. The transducer assembly may include an ultrasonic transducer and the transducer assembly may include means for pivoting the ultrasonic transducer. The inspection device may include a camera or a number of cameras.
The present application further describes an inspection head for an air gap inspection device. The inspection head may include a pair of expandable shoes, an inspection device attached to the pair of shoes, an ultrasonic transducer, and the ultrasonic transducer may be attached to one of the pair of shoes via a pivot assembly.
The pivot assembly may include a base and the ultrasonic transducer may be attached to the base by a number of arms. The arms may include a lever arm and a straight arm. The pivot assembly may include a motor thread connected to the lever arm. The inspection device may include a camera or a number of cameras.
These and other features of the present invention will become apparent to one of ordinary skill in the art upon review of the following detailed description when taken in conjunction with the drawings and the appended claims.
Clockwise and counterclockwise motion of the device along the tracks 22 and circumferential speed about the retaining ring is controlled by the operator at a control panel (not shown). The control panel has a series of switches and displays that help the operator control the air pressure for the track tensioners and the circumferential position of the device.
With reference to
One of the cables, e.g., cable 44, is wound over the drum 34 while the other of the cables, e.g., cable 46, is wound under the drum 34. As such, while winding the drum 34 in either direction, one of the cables 44, 46 is driving the mast while the other is idle. In this context, as the drum turns in one direction, one of the cables rolls off the drum as the other of the cables rolls on the drum. The cables 44, 46 extend over a first pulley 48 to a pulley system 50 that drives an extendible mast 52. The mast 52 may include a number of telescoping sections 54, preferably three flat rods that slide within one another allowing the mast 52 to become longer and shorter. As the drum 34 is driven in a first direction, the first cable 44 extends the mast 52 in an axial direction along the generator. Reversing the motor causes the second cable 46 to retract the mast 52.
The sled 64 may include two shoes 68A, 68B that are expandable and contractable by any suitable structure such as gears and levers or the like. Preferably, the shoes 68A, 68B sit flat together in the center of the inspection head 16 and are attached to two pneumatic spring return air rams 100 acting on links 101. When air is applied to the pneumatic rams 100, the shoes 68A, 68B separate to expand the sled 64 with one shoe coming in contact with the generator field, and the other extending into the stator slots. Links 102A are arranged parallel to each other so that the shoe 68A expands parallel to the central support member 62. Similarly, links 102B cause shoe 68B to expand parallel to the central support member 62. In a fully contracted position, the inspection head is sized to fit into a 0.5 inch (about 12.7 millimeters) gap. The shoes 68A, 68B serve to stabilize the inspection tool(s) in the gap and center the camera assembly 66. The camera assembly 66 is attached to the central support member 62 at a position that is axially forward of the sled 64.
With the shoes 68A, 68B expanded, axial movement can be initiated to begin the inspection. At least the shoe on the field side of the sled 64 is coated with Teflon or the like to facilitate sliding of the expanded sled in the gap.
When the gap has been completely inspected, the mast 52 is retracted to return the inspection head 16 to its starting position, the shoes 68A, 68B of the sled 64 are contracted, and the inspection head 16 is moved circumferentially to the next slot by the tractor section 12. The process is then repeated until all slots have been inspected.
Similar to the camera assembly disclosed in the above-noted '579 patent, the camera assembly 66 contains a forward view camera of fixed focus used for navigation and detection and a variable view camera with a power focus assembly and a right angle prism to allow for viewing of stator and rotor surfaces. The details of the camera are not pertinent to the present application and will not be further described. Other types of inspection devices may be used herein.
When wedge tightness inspections are performed, a separate shoe assembly is used that includes a wedge tapping module.
The inspection head 16 may alternatively or additionally carry an ELCID coil for inspecting shorted stator punchings. The ELCID coil is conventional and will not be further described. Those of ordinary skill in the art will appreciate that alternative inspection tools may also be supported by the inspection head, and the invention is not meant to be limited to the disclosed embodiments.
The miniature air gap inspection device according to the present application permits in-situ inspection of the generator field and stator core with entrance gaps of as little as 0.5 inches (about 12.7 millimeters) and larger. The inspection can be performed without rotation of the generator field, and valuable information can be gathered on the generator condition without requiring removal of the field. As noted, the inspection device is also designed to carry an auxiliary inspection tool such as a wedge tapping device and/or an ELCID coil for measuring the tightness of stator slot wedges and for inspection of shorted stator punchings, respectively.
The transducer head 240 may include an ultrasonic transducer of conventional design. The transducer head 240 may detect cracks as small as 0.025 inches (about 0.635 millimeters). The transducer assembly 210 also may have means for spreading couplant before the transducer head 240 and/or a means to vacuum the couplant after use. The couplant can be any desired fluid, including water. Any other type of inspection means also may be used herein.
It should be apparent that the foregoing relates only to the preferred embodiments of the present invention and that numerous changes and modifications may be made herein by one of ordinary skill in the art without departing from the general spirit and scope of the invention as defined by the following claims and the equivalents thereof.
Number | Name | Date | Kind |
---|---|---|---|
3602036 | Peterson | Aug 1971 | A |
3930942 | Thome | Jan 1976 | A |
4010636 | Clark et al. | Mar 1977 | A |
4285242 | Braithwaite | Aug 1981 | A |
4285243 | Collingwood | Aug 1981 | A |
4581938 | Wentzell | Apr 1986 | A |
4585610 | Andersson et al. | Apr 1986 | A |
4716271 | Hulsizer et al. | Dec 1987 | A |
4803563 | Dailey et al. | Feb 1989 | A |
4876672 | Petermann et al. | Oct 1989 | A |
4889000 | Jaafar et al. | Dec 1989 | A |
5285689 | Hapstack et al. | Feb 1994 | A |
5408883 | Clark et al. | Apr 1995 | A |
5557216 | Dailey et al. | Sep 1996 | A |
5563357 | Longree | Oct 1996 | A |
5650579 | Hatley et al. | Jul 1997 | A |
5969531 | Murakami et al. | Oct 1999 | A |
6100711 | Hatley | Aug 2000 | A |
6404189 | Kwun et al. | Jun 2002 | B2 |
6578424 | Ziola et al. | Jun 2003 | B1 |
6672413 | Moore et al. | Jan 2004 | B2 |
6883386 | Osone et al. | Apr 2005 | B2 |
6888143 | Vogt et al. | May 2005 | B2 |
6889783 | Moore et al. | May 2005 | B1 |
6959603 | Knight et al. | Nov 2005 | B2 |
7077020 | Langley et al. | Jul 2006 | B2 |
7201055 | Bagley et al. | Apr 2007 | B1 |
7249512 | Kennedy et al. | Jul 2007 | B2 |
20020017140 | Georgeson et al. | Feb 2002 | A1 |
20020074965 | Hatley et al. | Jun 2002 | A1 |
20080196504 | Johnson et al. | Aug 2008 | A1 |
20090000379 | Rath et al. | Jan 2009 | A1 |
Number | Date | Country |
---|---|---|
61160090 | Jul 1996 | JP |
2002209363 | Jul 2002 | JP |
Number | Date | Country | |
---|---|---|---|
20080087113 A1 | Apr 2008 | US |