Patent Application
20130170984
The invention relates generally to turbines and, more particularly, to last stage blades of steam turbines.
Last stage blades or “buckets” (LSBs) of steam turbines are designed with tip sections resembling flat plates. The orientation of the tip section is more or less closely aligned, depending on rotational speed and radius ratio, with the tangential direction to match the direction of the flow at outer flow filament radial locations. The precise orientation of the tip section is determined by flow analysis, at or near the design point. However, steam turbines are required to operate at very low flows and high exhaust pressures relative to the design point, to accommodate load demand and atmospheric conditions, respectively. This causes significant deviation in the flow direction and velocity at the bucket tip, resulting in flow induced vibration (FIV), which is potentially damaging and limits operational flexibility once a threshold value of negative incidence is exceeded.
It would be desirable to minimize FIV at turndown conditions, which can be achieved by modifying the tip design for the applicable range of radius ratios and speeds.
A turbine bucket includes a bucket airfoil having a cross-section in an airfoil shape. The bucket is twisted from a root end to a tip end. A degree of twist defines an accumulated angular offset of the tip end in a range of 10-15° relative to a tangential direction, thereby reducing excess negative incidence by 15-20° relative to the tangential direction.
In another exemplary embodiment, a turbine includes a rotor, a rotatable shaft that rotates with the rotor, and a turbine coupled with the rotatable shaft and the rotor. The turbine includes a plurality of axially spaced rotor wheels. A plurality of buckets are coupled with each rotor wheel, where each of the buckets has a cross-section in an airfoil shape. A last stage bucket is twisted from a root end to a tip end, and a degree of twist defines an accumulated angular offset of the tip end in a range of 10-15° relative to a tangential direction, thereby reducing excess negative incidence by 15-20° relative to the tangential direction.
In yet another exemplary embodiment, a method of reducing flow induced vibration in a last stage turbine bucket includes the step of twisting the turbine bucket to a degree that defines an accumulated angular offset of the tip end in a range of 10-15° relative to a tangential direction, thereby reducing excess negative incidence by 15-20° relative to the tangential direction.
In operation, steam 24 enters an inlet 26 of the turbine 10 and is channeled through the nozzles 22. The nozzles 22 direct the steam 24 downstream against the buckets 20. The steam 24 passes through the remaining stages imparting a force on the buckets 20 causing the rotor 12 to rotate. At least one end of the turbine 10 may extend axially away from the rotor 12 and may be attached to a load or machinery (not shown), such as, but not limited to, a generator, and/or another turbine. Accordingly, a large steam turbine unit may actually include several low pressure turbines that are all co-axially coupled to the same shaft 14. Such a unit may, for example, include a high-pressure turbine coupled to an intermediate-pressure turbine, which is coupled to a low-pressure turbine.
The significance of the turndown FIV region is that at conditions of low flow and high exhaust pressure, the flow through the LSB passage separates at the hub and is confined to a filament between approximately 80 and 100% of the radial height (where radial height is defined as 0% at a root end 201 of the bucket and 100% at a tip end 202 of the bucket). Thus it is primarily in this region that turndown FIV flow incidence has meaning. The limiting flow angle is the highest value of flow angle that can be achieved. In order for significant FIV to occur, the difference between the LSB tip optimum entrance angle (OEA), frequently taken as the mean of the distribution over the last 20% of radial height, and 180 degrees must exceed 15 degrees, negative. Thus, an LSB design with a tip OEA of 165 or more should not experience turndown FIV. The 40″ LSB for 3600 rpm applications closely approaches this criterion, while the 33.5″, 30″ and 26″, at the same rotational speed with progressively more excess negative incidence, have increasing potential for FIV at turndown. Data acquired in the field with strain gages demonstrates conclusively that the 30″ LSB vibration amplitudes are significantly greater than those of the 33.5″ at similar conditions of turndown operation thus tending to confirm this theory.
Above approximately 40″ radial height, for 3600 rpm designs, it is generally expected that the required 15 degrees of negative incidence cannot be achieved for buckets designed by state of the art aerodynamic design methods, as such LSBs will have tip OEAs greater than 165 degrees. The same statement is true for full and half speed buckets with active lengths scalable from 3600 rpm designs on the basis of speed. For example, at 3000 rpm a bucket with radial height=(3600/3000)×35″=42″ should also be low in turndown FIV potential.
The design is applicable to LSB designs incorporating pin and finger, dovetails, curved or straight axial entry dovetails or dovetails of the tangential entry type, the latter including a radial notch in the wheel to permit assembly, and a pinned block or notch blade to completely fill the wheel. The design is applicable to LSBs that are of the “freestanding” type (i.e., no connections between adjacent airfoils), as well as LSBs with midspan and/or tip shroud connections. Additionally, the last stage nozzle may remain the same as a design with a LSB of conventional section twist from root to tip, or have adjusted throat openings starting at a location reasonably removed (˜25%) from the root to preserve low root reaction. The adjustment should be such to ensure that the LSB entrance flow angle is as close as possible to the LSB metal section preferred entrance angle at all radial locations. Alternately an entirely redesigned nozzle may be applied. The adjustment or redesigned nozzle will ensure the highest possible stage performance. The LSB design approach described herein can be applied to conventional as well as high exhaust pressure designs, the latter having much higher exhaust pressure limits required for steam turbines in power plants with an air cooled condenser operating in high ambient temperature conditions.
The described embodiments serve to reduce flow induced forces that cause off-design vibration, by airfoil redesign. The airfoil tip section is designed so that stalled flow is greatly mitigated at turndown conditions. Particularly, this is accomplished by specifying a tip section inclination relative to the tangential direction at a specified angle. As a result, a safe operating range is increased, providing customers with more freedom and responding to load demand, particularly in hot weather. Additionally, last stage bucket reliability is increased, particularly in cases where the customer operates the turbine beyond manufacturer recommended limits.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiments, it is to be understood that the invention is not to be limited to the disclosed embodiments, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
