Apparatus and Method for Thermal Balancing of the Rotor of a Dynamo-Electric Machine

FIG. 1 is a general view, partly in cross-section, of a dynamo-electric machine.

FIG. 2 is a perspective view of the body portion of the rotor of the dynamo-electric machine shown in FIG. 1.

FIG. 3 is a longitudinal cross-section through the end turn region of the dynamo-electric machine shown in FIG. 1, showing the incorporation of two embodiments of the present invention.

FIG. 4 is a perspective view, with broken-away elements, of the body portion of the rotor in the vicinity of one of its end faces, showing the installation of an orifice disk according to the present invention.

FIG. 5 is a cross-section taken through line V--V of FIG. 3 showing a rotor body slot and its contents, including an orifice disk according to the present invention.

FIGS. 6A and 6B are perspective views of the slot wedge, orifice disk and insulating filler shown in FIGS. 4 and 5, showing the orifice disk in its maximum and minimum flow orientations, respectively.

FIG. 7 is a cross-section taken through line VII--VII of FIG. 3 showing a rotor body slot and its contents in the vicinity of one of the rotor body end faces and showing the installation of a baffle according to the present invention.

FIG. 8 is a cross-section taken through line VIII--VIII of FIG. 7.

FIG. 9 is a perspective view of the baffle according to the present invention.

FIG. 10 is a perspective view of the orifice disk according to the present invention.

FIG. 11 is a diagram of a rotor having a bow.

FIG. 12 is a cross-section through the rotor shown in FIG. 11 taken through line XII--XII.

Referring to the drawings, wherein like numerals represent like elements, there is illustrated in FIG. 1 a dynamo-electric machine, such as a large or medium turbine generator. The generator contains a stator 10 and a centrally disposed rotor. The rotor is composed of a shaft 14 and a body portion 16 having axially opposed end faces 17 and 18.

As shown in FIG. 2, there are a plurality of axially oriented slots spaced around the periphery of the body portion 16 of the rotor. The slots 12 carry field winding conductors, as shown in FIGS. 4 and 5. A portion of each slot forms an axially extending passageway 40 which is partially encased in a channel 32 disposed at the bottom of the slot. A wedge 50 retains the slot contents and an insulating filler 41 is disposed between the conductors 25 and the wedge. An insulating cell 36 lines the inside of the slot, encasing the channel 32, conductors 25 and insulating filler 41. As shown in FIGS. 4 and 8, the insulating cell 36 extends beyond the end face of the rotor to ensure that deposits do not form a conducting path between the shaft 14 and the conductors 25 where the conductors exit the body portion 16 of the rotor at its end face 17. The channel 32, which provides support for the insulating cell 36, extends slightly beyond the cell.

As shown in FIG. 1, the stator and rotor are encased in a housing 13 through which a coolant gas, such as air or hydrogen, circulates. A blower, not shown, may be used to assist in the circulation of the coolant. Coolant, after recirculation through a cooler 26, flows through inlet ducts 28 formed in the housing 13. As shown in FIG. 3, after exiting the inlet duct 28, the coolant flows through the annular chambers formed at each end of the rotor by the end turn portions 24 of the field winding conductors 25 and the shaft 14 and enters the body portion 16 of the rotor at end faces 17 and 18. In the body portion of the rotor, the coolant flows through the axial passageways 40 formed in the slots 12 shown in FIG. 2.

As shown in FIGS. 2 and 3, a plurality of radial passageways 38 spaced along each slot, allow the coolant flowing in the axial passageways 40 to flow radially outward and exit the body portion of the rotor at its periphery. After exiting the rotor the coolant flows through the gap 34 between the rotor and stator, as shown in FIG. 3. After exiting the gap 34 the coolant enters a cooler 26, as shown in FIG. 1, before recirculating back to the inlet duct 28. As shown in FIGS. 4 and 5, each radial passageway 38 in the slots 12 is comprised of a series of radially aligned slots 44 formed in the field winding conductors 25, a slot 46 in the insulating filler 41 and a hole 48 in the wedge 50.

According to one embodiment of the invention, thermal balancing is effected by installing a baffle 20, shown in FIG. 9, into the axial passageway 40 of one or more of the rotor body slots 12. The baffle may be installed into the entrance of the axial passageway at either or both ends of the rotor. The baffles may be retained in the portions of the channels 32 which extend beyond the insulating cells 36, as shown in FIGS. 7 and 8. The amount of coolant flowing axially through each slot and hence the circumferential temperature distribution in the rotor, can be finely and individually adjusted by varying the size of the tab 62 formed in the baffle 20, and thus the portion of the channel flow area restricted by the baffle. The baffle 20 is installed by deforming its legs 60 toward the tab 62 using a tool which engages conveniently located holes 56 in each leg. The baffle may then be placed into the entrance of the channel 32 and the legs 60 released. In its free, undeformed state, the width of the baffle across its legs is greater than the width of the inside of the channel so that the baffle is retained in the channel by means of a spring force exerted by the legs of the baffle against the interior walls of the channel, as shown in FIG. 7. It is not necessary to remove the rotor to install the baffles, although a portion of the inlet duct wall and an end bracket 29, shown in FIG. 3, must be removed to gain access to the channel entrances. Retention of the baffle is further aided by projections 22 emanating from the ends of the baffle legs 60, as shown in FIG. 9. As shown in FIG. 7 and 8 these projections can be inserted into slots 58 formed in opposing walls of the channel 32.

According to another embodiment of the invention, thermal balancing is effected by inserting an orifice created by a slot 54 formed in a disk 52, as shown in FIG. 10, into each radial passageway 38 in the rotor body slots 12, as shown in FIG. 3, 4 and 5. Each disk 52 is disposed between the wedge 50 and insulating filler 41. As shown in FIG. 5, a counter bore in the hole 48 through the wedge serves to retain the disk. The slot 54 in the disk 52 is aligned with the slots 44 in the field winding conductors 25, the slot 46 and the insulating filler 41 and the hole 48 in the wedge 50.

The length of the slot 54 in the disk 52 is equal to the diameter of the hole 48 in the wedge 50. The width of the slot 54 in the disk 52 is equal to the width of the slot 46 in the insulating filler 41. Thus, when the major axis of the slot 54 is aligned with the major axis of the slot 46 in the insulating filler 41, as shown in FIG. 6A, the effective flow area of the radial passageway 38 remains that of the common area of the slot 46 in the insulating filler and the hole 48 in the wedge, hence the flow area is not effected by the presence of the orifice, and the coolant flow through the radial passageway is at its maximum. As the disk is rotated, the flow area of the radial passageway, and hence the flow of coolant through it, is reduced as a result of the presence of the orifice. When the disk is rotated so that the major axis of its slot 54 is aligned with the minor axis of slot 46, as shown in FIG. 6B, the flow area becomes that of the common area in the slot 46 in the insulating filler and the slot 54 in the disk. With the disk in this orientation the flow area of the radial passageway, and hence the flow of coolant through it, is at its minimum. Thus, the coolant flow through each radial passageway can be finely adjusted to any value between these minimum and maximum flow rates. Further, since the radial passageways are spaced throughout the rotor in both the axial and circumferential directions, both axial and circumferential temperature non-uniformities can be eliminated.

The diameter of the counterbore in the hole 48 in which the disk 52 is retained is slightly smaller than the diameter of the disk. At installation, the disk is cooled, for example by immersing it in liquid nitrogen, to allow insertion into the counterbore. After the disk warms up to the temperature of the wedge, the resulting shrink fit prevents inadvertent rotation of the disk. Rotation of the disk to adjust the coolant flow requires removal of the rotor from the stator and recooling of the disk. Rotation of the disk can be facilitated by a tool, such as a screw driver, inserted into the slot 54 through the hole 48 in the wedge.

In practice the method of thermally balancing the rotor may involve measuring the temperature of the rotor body portion at various circumferential and axial locations and adjusting the flow of coolant, as previously described, accordingly.

Alternatively, adjustments to the coolant flow necessary to thermally balance the rotor may be based on measurements of the rotor vibration. Referring to FIG. 11, note that if unbalance in a rotor was caused by a permanent bow, then, using the prior art balancing methods previously discussed, it would be compensated for by adding weight to the periphery of the rotor 72 at the concave side 76 of the bow, thereby shifting the mass centerline 68 of the rotor back toward to the bearing centerline 66. Using the thermal balancing method disclosed by the present invention, if the bow in the rotor depicted in FIG. 11 were caused by an asymmetric temperature distribution such that the portion of the rotor denoted 74 is hotter than the portion denoted 76, then the bow could be eliminated by reducing the coolant flow in slot 78, located in the cooler portion 76 of the rotor, by inserting a baffle into the channel in slot 78 or rotating the disks containing the orifices in the radial passageways in the center portion of slot 78, depending on the embodiment of the invention utilized.

Since, in reality, the bow in the rotor is not visually apparent, the amount and location of the coolant flow adjustment necessary to eliminate the bow is based on measurements of the amplitude and phase angle of vibration. The method is similar to that previously discussed for the field balancing procedure, except that instead of adding a trial weight, a predetermined trial adjustment in the cooling flow is made at a location which experience indicates will have a beneficial effect on the vibration. The amount and location of coolant flow adjustment necessary to eliminate the thermal unbalance, and hence minimize the vibration, is then determined based on the effect of the trial adjustment.

Many modifications and variations of the present invention are possible in light of the above techniques. It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.