Fuel cell system and aircraft having an inerting system
US-2024379984-A1 · Nov 14, 2024 · US
US10230116B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10230116-B2 |
| Application number | US-201414567210-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 11, 2014 |
| Priority date | Dec 30, 2013 |
| Publication date | Mar 12, 2019 |
| Grant date | Mar 12, 2019 |
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An air supply apparatus and method for a fuel cell, which supplies high-pressure air while avoiding a surge phenomenon of a turbo type compressor in a fuel cell system to which the turbo type compressor is applied is provided. In particular, a portion of air from an outlet of a compressor to an inlet of the compressor is recirculated to the supply of air supplied from the compressor to a stack. This recirculated air and external air introduced from the outside are mixed and supplied to the inlet of the compressor at a sufficiently high air pressure, allowing the compressor to avoid a surge region and enabling the supply of air with a high pressure and a low flow rate.
Opening claim text (preview).
What is claimed is: 1. An air supply apparatus for a fuel cell comprising: a compressor configured to supply air to a stack of a fuel cell; a bypass line connected between an outlet and an inlet of the compressor; a bypass valve disposed within the bypass line; and an ejector that mixes bypass air and external air to increase a pressure of air within the stack and then supplies mixed air to the inlet of the compressor, the ejector being connected between the inlet of the compressor and a rear side of the bypass valve, wherein the ejector suctions atmospheric air to supply air increased in pressure to the inlet of the compressor while recirculating a portion of air from the outlet of the compressor back to the inlet of the compressor, wherein the objector includes; a bypass air inflow aperture that receives the bypass air; a chamber inlet that receives the external air; a suction chamber in which the bypass air and the external air mixed; and a throat increasing in diameter, and wherein the bypass line is connected to the bypass air inflow aperture formed at a side surface of the ejector, and the throat of the ejector is connected to the inlet of the compressor. 2. The air supply apparatus of claim 1 , comprising a sensor disposed on one side of an inlet of the ejector to measure a flow rate of air introduced from the outside and filter out foreign substances. 3. The air supply apparatus of claim 1 , wherein the bypass valve disposed within the bypass line is controlled by a controller configured to control whether or not to recirculate compressed air and an air flow rate. 4. The air supply apparatus of claim 1 , wherein the compressor comprises a turbo type compressor. 5. An air supply method for a fuel cell, comprising: recirculating a portion of air from an outlet of a compressor back to an inlet of the compressor to be supplied by the compressor to a fuel cell stack, wherein the recirculated air and external air introduced from the outside are mixed and supplied to the inlet of the compressor at a sufficient air pressure by an ejector to allow the compressor to avoid a surge region and provide the fuel cell stack with a supply of air at a high pressure and a low flow rate; wherein the ejector suctions atmospheric air to supply air increased in pressure to the inlet of the compressor while recirculating a portion of air from the outlet of the compressor back to the inlet of the compressor, wherein the ejector includes: a bypass air inflow aperture that receives the bypass air; a chamber inlet that receives the external air; a suction chamber in which the bypass air and the external air are mixed; and a throat increasing in diameter, and wherein a bypass line is connected to the bypass air inflow aperture formed at a side surface of the ejector, and the throat of the ejector is connected to the inlet of the compressor. 6. The air supply method of claim 5 , wherein air supplied to the inlet of the compressor is increased in pressure inside the ejector using a Venturi effect, and then is supplied to the inlet of the compressor.
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