PRESSURIZED AIR SUPPLY SYSTEM, FUEL CELL SYSTEM COMPRISING THE PRESSURIZED AIR SUPPLY SYSTEM, AND STARTING METHOD OF THE PRESSURIZED AIR SUPPLY SYSTEM
A pressurized air supply system includes a turbocharger including a turbine and a compressor, a recuperator for heat exchange between discharged air from the compressor and flue gas exhausted from the turbine, a start-up heater for heating the air, that includes at least either of start-up air or pressurized air from the compressor, which is supplied to discharged air line between the compressor outlet and the recuperator, and a catalytic combustor for supplying, to the turbine, combustion gas which is generated by combustion of fuel with the flowing air heated by the start-up heater.
1 . A pressurized air supply system, comprising:
a turbocharger including a turbine and a compressor;
a recuperator for heat exchange between discharged air from the compressor and flue gas exhausted from the turbine;
a start-up heater for heating the air, that includes at least either of start-up air or the discharged air from the compressor, which is supplied to discharged air line between the compressor outlet and the recuperator; and
a catalytic combustor for supplying, to the turbine, combustion gas which is generated by combustion of fuel with the flowing air heated by the start-up heater.
2 . The pressurized air supply system according to claim 1 ,
further comprising a motor for driving the compressor,
wherein the start-up air is supplied by the compressor driven by the motor.
3 . The pressurized air supply system according to claim 2 ,
wherein the motor is connected to the compressor via a speed increasing gear.
4 . The pressurized air supply system according to claim 1 , further comprising recuperator bypass line for a part of the discharged air from the compressor to bypass the recuperator.
5 . The pressurized air supply system according to claim 4 ,
wherein the discharged air flowing through the recuperator bypass line joins the air flowing into the catalytic combustor.
6 . The pressurized air supply system according to claim 4 ,
wherein the discharged air flowing through the recuperator bypass line joins the flue gas flowing out of the recuperator.
7 . The pressurized air supply system according to claim 1 , comprising:
pressurized air line through which the air heated by the recuperator flows;
branch line branching from the pressurized air line and joining the exhaust air line after flowing through the start-up heater; and
fuel cell heating bypass air line further branching from downstream of the start-up heater on the branch line and rejoining the pressurized air line.
8 . The pressurized air supply system according to claim 7 , comprising, upstream of the start-up heater, a flow regulating valve for regulating the flow rate of the air flowing into the start-up heater.
9 . The pressurized air supply system according to claim 8 ,
wherein the start-up heater includes:
a first heater for heating the flowing air supplied to the catalytic combustor; and
a second heater for heating the air flowing through the pressurized air line.
10 . A fuel cell system, comprising:
the pressurized air supply system according to claim 1 ; and
a fuel cell having cathode and anode,
wherein the fuel cell system is configured such that pressurized air supplied from the pressurized air supply system flows into the cathode.
11 . A starting method of the pressurized air supply system according to claim 1 , the method comprising:
a step of supplying at least either of the start-up air or the discharged air to a discharged air line between the compressor outlet and the recuperator;
a step of heating the flowing air by starting the start-up heater;
a step of generating a combustion gas by combustion of fuel with the flowing air by starting the catalytic combustor, after a catalyst temperature of the catalytic combustor is increased to preset temperature or higher with the heated flowing air; and
a step of stopping the start-up heater or decreasing the load of the start-up heater, after the compressor is driven by rotation of the turbine with the combustion gas.