Apparatus and process for testing a large combustor using a CAES facility
An apparatus, system, and process for testing a gas turbine engine or other test object under a cold condition, such as a compressor of a gas turbine engine, a combustor of a gas turbine engine, or an afterburner of an aero gas turbine engine, using compressed air stored in an underground storage reservoir of a CAES system along with an air turbine or an air injector. High-pressure, but low-volume, compressed air from a CAES system can be converted into a low-pressure, but high-volume, flow of compressed air using an air injector to supply enough compressed air to test a combustor or an afterburner. High pressure compressed air from the CAES system can be used to drive an air turbine that then drives a compressor for testing.
1. A process for testing a compressor using a compressed air energy storage (CAES) system, the process comprising:
storing a compressed air in an underground storage reservoir of the CAES system;
passing the compressed air from the underground storage reservoir into a combustor to burn with a fuel and produce a hot gas flow; and
passing the hot gas flow through a turbine to drive the compressor to be tested.
2. The process of claim 1 , further comprising:
passing the hot gas flow from the combustor through a heat exchanger prior to passing the hot gas flow through the turbine; and
passing the compressed air from the compressor through the heat exchanger such that heat from a flow of the compressed air increases a temperature of the hot gas flow from the combustor prior to entry of the hot gas flow into the turbine.
3. The process of claim 1 , further comprising:
passing the compressed air from the underground storage reservoir through a pre-heater prior to passing the compressed air from the underground storage reservoir into the combustor.
4. A process for testing a combustor using a compressed air energy storage (CAES) system, the process comprising:
storing a high pressure compressed air in an underground storage reservoir of the CAES system;
passing high-pressure but low-volume compressed air from the underground storage reservoir into an air injector to produce low-pressure but high volume compressed air;
passing the low-pressure but high-volume compressed air from the air injector into the combustor; and
burning a fuel with the low-pressure but high-volume compressed air in the combustor for testing of the combustor.
5. A process for testing a combustor using a compressed air energy storage (CAES) system, the process comprising:
storing a high pressure compressed air in an underground storage reservoir of the CAES system;
passing the high pressure compressed air from the underground storage reservoir into an air turbine;
driving a low-pressure but high-volume compressor with the air turbine to produce a low-pressure but high-volume compressed air;
passing the low-pressure but high-volume compressed air from the low pressure but high-volume compressor into the combustor; and
burning a fuel with the low-pressure but high-volume compressed air in the combustor for testing of the combustor.
6. A process for testing an afterburner of an aero gas turbine engine under conditions of high altitude, the process comprising:
storing a high pressure compressed air in an underground storage reservoir of a compressed air energy storage (CAES) system; passing high-pressure compressed air from the underground storage reservoir through an air injector to produce a low-pressure compressed air;
operating the aero gas turbine engine to produce a hot gas flow;
passing the hot gas flow through the afterburner; and
passing the low-pressure compressed air from the air injector at an outlet of the afterburner for testing the afterburner to simulate a high-altitude condition.