Operation of dual gas turbine fuel system

A method of operating a fuel delivery system comprising (a) a low energy gas delivery system comprising a low energy gas inlet, a manifold split, a low energy gas primary manifold outlet, and a low energy gas secondary manifold outlet;

• (b) a high-energy gas delivery system comprising a high-energy gas inlet and a high-energy gas primary manifold outlet;
• (c) a primary manifold comprising a primary manifold nozzle outlet;
• (d) a secondary manifold comprising a secondary manifold nozzle outlet;
• and (e) a compressor discharge pressure system comprising a compressor discharge pressure inlet and a compressor discharge pressure outlet, wherein the low energy gas primary manifold outlet and the high-energy gas primary manifold outlet are coupled to the primary manifold, the low energy gas secondary manifold outlet and the compressor discharge pressure outlet are coupled to the secondary manifold, the low energy gas delivery system further comprises a primary low energy gas control valve between the gas split and the low energy gas primary manifold outlet, the low energy gas delivery system further comprises a secondary low energy gas control valve between the gas split and the low energy gas secondary manifold outlet, the high-energy gas delivery system further comprises a high-energy gas control valve between the high-energy gas inlet and the high-energy gas primary manifold outlet, and the compressor discharge pressure system further comprises a compressor discharge pressure valve between the compressor discharge pressure inlet and the compressor discharge pressure outlet, the method of operating comprising:
• closing the primary low energy gas control valve;
• measuring the primary manifold nozzle pressure ratio across the primary manifold nozzle outlet;
• comparing the primary manifold nozzle pressure ratio against a primary manifold specification limit;
• adjusting the stroke of the high-energy gas control valve to maintain the pressure ratio across the primary manifold nozzle outlet within the primary manifold specification limit;
• closing the secondary low energy gas control valve;
• measuring the secondary manifold nozzle pressure ratio across the secondary manifold nozzle outlet;
• comparing the secondary manifold nozzle pressure ratio against a secondary manifold specification limit;
• and
• adjusting the stroke of the compressor discharge pressure valve to maintain the pressure ratio across the secondary manifold nozzle outlet within the secondary manifold specification limit.

A method of operating a fuel delivery system comprising (a) a low energy gas delivery system comprising a low energy gas inlet, a manifold split, a low energy gas primary manifold outlet, and a low energy gas secondary manifold outlet;

• (b) a high-energy gas delivery system comprising a high-energy gas inlet and a high-energy gas primary manifold outlet;
• (c) a primary manifold comprising a primary manifold nozzle outlet;
• and (d) a secondary manifold comprising a secondary manifold nozzle outlet, wherein the low energy gas primary manifold outlet and the high-energy gas primary manifold outlet are coupled to the primary manifold, the low energy gas secondary manifold outlet is coupled to the secondary manifold, the low energy gas delivery system further comprises a primary low energy gas control valve between the manifold split and the low energy gas primary manifold outlet, the low energy gas delivery system further comprises a secondary low energy gas control valve between the manifold split and the low energy gas secondary manifold outlet, and the high-energy gas delivery system further comprises a high-energy gas control valve between the high-energy gas inlet and the high-energy gas primary manifold outlet, the method of operating comprising:
• closing the high-energy gas control valve;
• measuring the primary manifold nozzle pressure ratio across the primary manifold nozzle outlet;
• comparing the primary manifold nozzle pressure ratio against a primary manifold specification limit;
• adjusting the stroke of the primary low energy gas control valve to maintain the pressure ratio across the primary manifold nozzle outlet within the primary manifold specification limit;
• adjusting the stroke of the primary low energy gas control valve to maintain equal nozzle pressure ratio across the primary and secondary manifold nozzle outlets;
• measuring the secondary manifold nozzle pressure ratio across the secondary manifold nozzle outlet;
• comparing the secondary manifold nozzle pressure ratio against a secondary manifold specification limit;
• and
• adjusting the stroke of the secondary low energy gas control valve to maintain the pressure ratio across the secondary manifold nozzle outlet within the secondary manifold specification limit.