BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a cross sectional view of a DLE combustor;
FIG. 2 is a graphical representation of a premixer staging sequence showing five operating modes of a combustor;
FIG. 3 is a flowchart depicting a method for automatic mapping of a combustor in a gas turbine engine system;
FIG. 4 is a flowchart depicting a procedure to determine if bulk combustor flame temperature requires adjustment, for use in block 1.6 of FIG. 3;
FIG. 5 is a flowchart depicting a procedure for adjusting bulk combustor flame temperature as used in block 1.7 of FIG. 3;
FIG. 6 is a flowchart depicting a procedure to determine which dome is to be adjusted, as implemented in block 1.8 of FIG. 3;
FIG. 7 is a flow chart depicting a procedure to determine the maximum ring temperature boundary for a given operating mode and bleed level, as is used in block 1.9 of FIG. 3;