The manufacturer of the generator should be able to provide the performance of the unit for different cooling gas temperature. In absence of better information the following could help to obtain an approx. adjusted generator reactive capability performance.
Let’s use the following as example to describe an approximate procedure:
Ex. 250 MVA air-cooled generator, 15oC inlet air and 85% PF lagging. Determine the reactive capability curve for 40oC at rated power factor.
1- From the Generator MW vs. Gas Temperature curve, determine the normalized MW increment factor, K.
Ex. K= 1- MW40oC/Rate MW15oC = 0.80.
NOTE: In absence of any data for K, use the following approximation:
MW(T) = 180-1.44. T. T = Ambient Temp (oC)
2- Maintain fix the under excited point witch is the point (MW=0, -MVAR). This point does not set by thermal limits because is determined by the minimum excitation and stability limits requirements.
MVAR40oC @ 0 MW = MVAR15oC @ 0 MW.
3- Determine a set of points Adjust set of points
For MW: MW40oC = K . MW15oC.
For MVAR: MVAR40oC = [K+(1+K).(1-MW15oC/Tarted max MW15oC)].MVAR15oC.
4- Draw the new reactive capability curve for 40 oC with the new values determined in 2 & 3 above.
References:
1- IEEE 67-1990, “IEEE Guide for Operation & Maintenance of Turbine Generator”
2- Siemens/Westinghouse: Technical Appendix, “Adjustment of Generator Capability Curves-General Guideline”.