Gas turbine efficiency and regulation speed improvements using supplementary air system continuous and storage systems and methods of using the same

1. A method of providing a source of heated compressed air to a gas turbine, comprising:

operating a fueled engine to produce hot exhaust gases and mechanical work to drive a supplemental compressor, where the supplemental compressor produces a supply of compressed air;

storing a first portion of the supply of compressed air in an air storage tank after the first portion of the supply of compressed air has been cooled by an intercooler, and routing a second portion of the supply of compressed air to a mixer, the second portion of the supply of compressed air bypassing the air storage tank and the intercooler;

selectively mixing at the mixer the first portion of the supply of compressed air with the second portion of the supply of compressed air to form mixed air;

heating the mixed air with heat from the hot exhaust gases of the fueled engine;

wherein:

the supplemental compressor draws in air separately from the fueled engine, where air drawn in by the fueled engine is ambient air; and

the supplemental compressor and the fueled engine are mechanically coupled to each other.

2. The method of claim 1 , further comprising returning a part of the supply of compressed air to the supplemental compressor for additional compression.

3. The method of claim 1 further comprising directing the mixed air and hot exhaust gases through a recuperator.

4. The method of claim 3 further comprising the step of directing the mixed air from the recuperator to an external source.

5. The method of claim 1 , wherein the fueled engine is a reciprocating engine.

6. A system for heating compressed air for a gas turbine comprising:

a fueled engine producing hot exhaust and mechanical power;

a supplemental compressor mechanically coupled to the fueled engine;

a recuperator in fluid communication with the supplemental compressor and the fueled engine;

an air storage tank and an intercooler, each in selective fluid communication with the supplemental compressor; and

a mixer upstream of the recuperator fluidly coupled to each of the air storage tank and the supplemental compressor, the mixer being configured to mix air compressed by the supplemental compressor, cooled by the intercooler, and stored in the air storage tank with air compressed by the supplemental compressor and bypassing the air storage tank and the intercooler;

wherein:

the recuperator receives the mixed air and hot exhaust from the fueled engine and uses the hot exhaust to raise the temperature of the mixed air passing through the recuperator;

the supplemental compressor draws in air separately from the fueled engine; and

air drawn in by the fueled engine is ambient air.

7. The system of claim 6 , wherein the fueled engine operates on natural gas.

8. The system of claim 7 , wherein the supplemental compressor is a multi-stage axial compressor.

9. The system of claim 6 further comprising a flow control valve positioned between the supplemental compressor and the recuperator for regulating the mixed air to the recuperator.

10. The method of claim 6 , wherein the fueled engine is a reciprocating engine.

11. A method of providing a heated compressed air supply to a gas turbine comprising:

providing a fueled engine coupled to a supplemental compressor;

operating the fueled engine to produce a hot exhaust gas and mechanical output to power the supplemental compressor, where the supplemental compressor produces a compressed air supply;

storing a first portion of the compressed air supply in an air storage tank after the first portion of the compressed air supply has been cooled by an intercooler, and routing a second portion of the compressed air supply to a mixer, the second portion of the compressed air supply bypassing the air storage tank and the intercooler;

selectively mixing at the mixer the first portion of the compressed air supply with the second portion of the compressed air supply to form mixed air;

heating the mixed air with heat from the hot exhaust gas of the fueled engine; and,

directing the heated mixed air to an output location;

wherein:

the supplemental compressor draws in air separately from the fueled engine, where air drawn in by the fueled engine is ambient air; and

the supplemental compressor and the fueled engine are mechanically coupled to each other.

12. The method of claim 11 , wherein the output location is a compressor discharge plenum of a gas turbine engine.

13. The method of claim 11 , wherein the fueled engine is a reciprocating internal combustion engine.

14. The method of claim 11 , wherein the heating of the mixed air occurs in a recuperator.

15. The method of claim 14 , wherein the hot exhaust gases are at a lower temperature at an exit of the recuperator than at an entry to the recuperator.

16. The method of claim 11 , wherein the fueled engine is a reciprocating engine.

17. A method of providing a source of heated compressed air to a gas turbine, comprising:

operating a fueled engine to produce hot exhaust gases and mechanical work to drive a supplemental compressor, where the supplemental compressor produces a supply of compressed air;

providing a pathway, the pathway comprising a mixer and a recuperator; the recuperator adapted to heat a fluid using hot exhaust gases from the fueled engine;

storing a first portion of the supply of compressed air in an air storage tank after the first portion of the supply of compressed air has been cooled in an intercooler;

routing a second portion of the supply of compressed air through the pathway such that it bypasses the air storage tank and the intercooler, and heats up in the recuperator;

routing a mixture of the first portion and the second portion to an output; wherein, the supplemental compressor draws in air separately from the fueled engine, where air drawn in by the fueled engine is ambient air.