Background of the Invention
This invention relates in general to lubricant supply systems for thrust bearings of the type used in large rotating shaft machines; and, in particular, to means responsive to axial thrust within the machine which apportion the lubricant supply to either an active or inactive bearing.
Rotating shaft machines such as turbines include stationary thrust bearings for preventing excess axial movement of the rotating shaft. The rotating shaft has a thrust collar which is rotatable with the shaft and which is positioned axially between an "active" and an "inactive" thrust bearing. Lubricating fluid is sent to both bearings to provide a lubrication film on the face of each thrust bearing which then supports the thrust collar as the shaft moves in either axial direction. The "active" thrust bearing is the bearing expected to ordinarily carry the higher loads most of the time whereas the "inactive" bearing would carry loads part of the time.
The problem which the present invention solves is to minimize the total lubricant flow rate to the two thrust bearings while still providing for a variety of operating conditions which may cause the normally inactive thrust bearing to become loaded.
In the prior art, it is a common practice in turbomachinery thrust bearing design to establish the size of the required normally active thrust bearing based upon some assumed steady-state operating condition of the machine. Axial thrust forces acting upon various components of a rotor are estimated, including, for example; the blades, wheel disks etc. and a net axial thrust is determined for this steady-state condition. The net axial thrust is typically the small difference between two large values thrusting the rotor in the fore and aft directions. It is well known to designers that this net axial thrust calculation may be subject to considerable error. Nevertheless, the normally active thrust bearing is generally sized based upon such a calculation of net thrust load and the allowable load per square inch of thrust bearing area. The lubricant flow rate to this normally active bearing is then established from considerations of its size, load and rubbing velocity.
In the design of heavy duty gas turbines, it is a usual practice to provide a normally inactive bearing smaller than the normally active bearing based upon the presumption that the inactive thrust will not exceed 50 percent of the design point active thrust load. The inactive thrust bearing size and the required flow rates are therefore based upon this premise. A total flow to the thrust bearings is supplied based upon the needs of the full-size active thrust bearing and the reduced capacity of the inactive thrust bearing. The usual thrust bearing lubricant supply arrangement includes a common header which supplies a journal bearing and two thrust bearings. The flow rate to each of the thrust bearings is controlled by different size orifices or drilled holes in the castings through which the lubricant must pass from the inlet header.
The design assumption for sizing the inactive thrust bearing does result in the benefits of reduced lubricant flow. Under certain conditions, however, the lubricant supplied to the inactive bearing may be inadequate or marginal for the imposed thrust load. As previously noted, the calculation of net thrust load is inherently subject to error even at the machine design point condition. Under off-design machine operation, or under transient machine operation, or with the wear of some critical components, it is possible for the normally inactive bearing to become subject to a high thrust force. In such a case, it is desirable to have more flow to the inactive bearing than is normally provided.
It is a universal practice to have both active and inactive thrust bearings on a turbomachine rotor. In cases where turbomachines have equally-sized active and inactive, it is common practice to supply lubricant at a rate sufficient for both bearings.
Object of the Invention
The object of the invention is to minimize the required total lubricant flow rate to the two thrust bearings, whether or not those thrust bearings are of equal size. In the case of two equally sized bearings, the total flow rate required is the minimum amount required for a single bearing. In the case of unequally sized bearings, the total flow rate required is that needed for the larger bearing.
Summary of the Invention
The present invention is practiced upon a rotating shaft machine which includes a shaft mounted thrust collar positioned between an active thrust bearing and an inactive thrust bearing. A supply of lubrication fluid is sent to a distribution means which includes a spool valve. The position of the spool valve is determined by pilot fluid ports which communicate shaft position to the distribution means whereas the position of the spool valve determines lubricant flow through distribution ports of the distribution means which is connected to both the active and inactive thrust bearings. In this way, the position of the thrust collar relative to the active and inactive thrust bearings is transmitted to the lubrication distribution means whereupon the proper amount of lubrication is then flowed to the thrust bearings as required.
Brief Description of the Drawings
FIG. 1 is an elevation cross section view of a rotating shaft machine taken generally in the area of the thrust bearings.
FIG. 2 is a schematic showing the present invention in combination with a thrust bearing.
FIG. 3 is a cross section of a spool valve used in the distribution means of the present invention, when the valve is in neutral position.
FIG. 4 is a cross section of a spool valve used in the distribution means of the present invention, when the valve is diverting more flow to one bearing than the other.
FIG. 5 is a load diagram illustrative of the forces present which are useful in determining the position of the rotating shaft.
Detailed Description of the Invention
A rotating machine intake end 1 is shown in FIG. 1 as a cross-section. The intake end 1 includes an intake annulus 3 which draws inlet gases into the machine. A rotor or rotating shaft 5, of which the end portion is shown, is positioned within the machine and includes a thrust collar 7 which is fixed to the rotating shaft. An inner casing 9 surrounds the end of the rotor and generally supports an active thrust bearing 11 and an inactive thrust bearing 13. The active and inactive thrust bearings are generally determined by the direction of thrust of the motive fluid which is indicated by the arrow 15. In FIG. 1, the active bearing 11 is larger than the inactive bearing 13 in order to absorb the thrust in the direction of the arrow 15.
Bearing lubrication is supplied through a bearing lubrication supply pipe 19 which provides lubrication to the active bearing 11 through pipe 21; to the inactive bearing 13 through pipe 23; and to the journal bearing 27 through the pipe 25. Note that each of the supply pipes 21, 23 or 25 may be sized differently or contain different size flow restrictors so as to supply the appropriate amount of bearing fluid to each respective bearing.
FIG. 2 shows a thrust bearing lubrication system 30 in accordance with the present invention. A rotating shaft 31, of a rotating shaft machine (not shown) includes a thrust collar 33 which is made integral with the rotating shaft so as to be rotatable therewith. Active and inactive or first and second thrust bearings 35 and 37 each surround the rotating shaft and are depicted as being of equal size; although as previously explained, they could be of unequal size with the active bearing being larger than the inactive bearing. Thrust bearing construction is well known in the art and therefore does not need to be further explained here except to say that each bearing generally comprises an annular cage which supports a plurality of bearing pads. Thus the bearing itself is an annular structure comprised of a plurality of arcuate segments or bearing pads.
The thrust bearing lubrication system of the present invention includes a means for distributing the lubrication fluid 41 which further includes an input bearing lubrication fluid indicated by flow arrow 43. The means for distributing the lubrication fluid 41 is basically a manifold having inputs and outputs in accordance with the following description. Assuming a thrust direction in FIG. 2, the same as in FIG. 1; ie, right to left, the active thrust bearing is bearing 35 while the inactive thrust bearing is bearing 37. Each thrust bearing is monitored for lubrication film pressure between the face of the thrust bearing and the surface of the thrust collar. Thus the fluid film pressure at the active thrust bearing is monitored on line 45; and, the fluid film pressure at the inactive thrust bearing is monitored on line 47 both of which provide a kind of feedback or control signal to the lubrication fluid distribution means 41 as indicated by the arrows to provide a means for sensing the direction and position of axial thrust. There are also outbound fluid distribution lines 49 and 51, which connect the fluid distribution means 41 with the active bearing 35 and the inactive bearing 37 respectively.
FIG. 3 shows a cross-section of the fluid distribution means 41; and, in particular, shows a spool valve 55 which is slidable within the fluid distribution means. The fluid distribution means 41 further includes first and second fluid distribution ports 59 and 61 which are connected to the active and inactive cutbound fluid distribution lines 49 and 51 respectively. The fluid distribution means 41 also includes first and second pilot ports 65 and 67 which are connected to the inbound active pressure line 45 and the passive pressure line 47 respectively.
FIG. 5 shows a pressure distribution curve taken between the active and inactive bearings 35 and 37 respectively with the active bearing face 75 of the thrust collar 33 and the inactive bearing face 77 of the thrust collar 33. It can be appreciated from the inactive pressure distribution diagram 81 that the closer the thrust collar is to the bearing, the greater the pressure sensed in the line 47. Likewise, the further the bearing from the thrust collar the less pressure that will be sensed in the normally active line 45 as demonstrated in pressure diagram 83.
Referring back to FIG. 4, the total flow 43 into the lubrication fluid distribution means (manifold) is apportioned as a result of the pressures sensed at the respective bearings which, in turn, depends upon the axial position of the thrust collar and hence the rotor itself. In accordance with FIG. 5, the rotor has moved toward the inactive bearing thereby causing increased fluid pressure in line 47 which is connected into pilot pressure port 67. The increased pressure drives the spool valve 55 toward the left as shown, which uncovers fluid distribution port 61 to provide a greater share of the total fluid flow 43 into the fluid distribution line 51. The foregoing is accomplished by pressure bearing against the double sided piston 90 to provide a resultant force in one or the other direction which then moves the plugs 95 and 97 which extend in opposite directions from the piston to uncover either the active fluid distribution port 59 or the passive fluid distribution port 61 respectively.
Further in accordance with the invention, it is anticipated that where the two thrust bearings are of equal size, the total lubrication flow 43 to be apportioned will be equal to the maximum anticipated flow for one bearing. In the case where the two bearings are of unequal size, it is anticipated that the total lubrication flow 43 to be apportioned will be equal to the maximum flow anticipated for the larger bearing.
While there has been shown what is considered to be a preferred embodiment of the invention, it should be kept in mind that other embodiments will occur to those of ordinary skill in the art. For example, there are equivalent ways of determining the position of the thrust collar relative to the bearing surfaces other than by sensing pressures including the use of electronic load cells to provide a positioning signal to the spool valve within the lubrication fluid distribution means. It is intended to cover in the appended claims, all such modifications as will fall within the true spirit and scope of the claims.