# US 2019/0356006 A1 · Pressure Balancing of Anode and Cathode in a Fuel Cell System

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- Number: US 2019/0356006 A1
- Document ID: US20190356006A1
- Status: Published application
- Kind: A1
- Application number: 15/983,005
- Filed: 2018-05-17
- Published: 2019-11-21
- Earliest claimed: 2018-05-17
- Assignees: FuelCell Energy, Inc.
- Applicants: FuelCell Energy, Inc.
- Inventors: Hossein GHEZEL-AYAGH; James B. WALZAK
- Web page: https://patentgrep.com/patent/US20190356006A1

## CPC

- H01M 8/0606: with means for production of gaseous reactants
- H01M 8/04014: Heat exchange using gaseous fluids; Heat exchange by combustion of reactants
- H01M 8/04104: {Regulation of differential pressures}
- H01M 8/04111: using a compressor turbine assembly
- H01M 8/0662: Treatment of gaseous reactants or gaseous residues, e.g. cleaning
- Y02E 60/50: Fuel cells
- H01M: PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- Y02E: REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION

## Abstract

A fuel cell system includes a fuel cell having an anode configured to receive anode feed gas and output anode exhaust, and a cathode configured to receive cathode feed gas and output cathode exhaust. The system further includes a pressurizing assembly downstream from the anode and an oxidizer downstream from the anode. The cathode feed gas is the anode exhaust that has been compressed in the pressurizing assembly and reacted with air in the oxidizer.

## Claims

### Claim 1

A fuel cell system, comprising:
a fuel cell, comprising:
an anode configured to receive anode feed gas and output anode exhaust; and
a cathode configured to receive cathode feed gas and output cathode exhaust;
a pressurizing assembly downstream from the anode; and
an oxidizer downstream from the anode;
wherein the cathode feed gas is the anode exhaust that has been compressed in the pressurizing assembly and reacted with air in the oxidizer.

### Claim 2 (depends on 1)

The system according to claim 1, wherein the pressurizing assembly comprises a blower.

### Claim 3 (depends on 1)

The system according to claim 1, wherein the pressurizing assembly comprises an eductor having an inlet end defining a nozzle, the inlet end configured to receive the anode exhaust and air, and an outlet end defining a diffuser.

### Claim 4 (depends on 3)

The system according to claim 3, wherein the pressurizing assembly further comprising a blower configured to receive air from an air supply, compress or accelerate the air, and feed the compressed air to the nozzle of the eductor for mixture with the anode exhaust.

### Claim 5 (depends on 3)

The system according to claim 3, further comprising a turbine defining a turbine inlet configured to receive and compress air from an air supply and a turbine outlet configured to output the air.

### Claim 6 (depends on 5)

The system according to claim 5, wherein the nozzle of the eductor is configured to receive at least a portion of the air from the turbine outlet for mixture with the anode exhaust.

### Claim 7 (depends on 5)

The system according to claim 5, wherein a slip stream of compressed air is output from the turbine inlet; and
wherein the nozzle of the eductor is configured to receive the slip stream for mixture with the anode exhaust.

### Claim 8 (depends on 5)

The system according to claim 5, further comprising a turbine loop, comprising:
a low-temperature recuperator configured to receive air from the turbine inlet and transfer heat between the air and the cathode exhaust;
a heater configured to receive and heat the air from the low-temperature recuperator; and
a high-temperature recuperator configured to receive the air from the heater and transfer heat from the air to the cathode feed gas;
wherein the turbine outlet is configured to receive the air from the high-temperature recuperator.

### Claim 9 (depends on 5)

The system according to claim 5, wherein:
at least a portion of the air output from the turbine outlet defines a bypass stream; and
the bypass stream is mixed directly with at least one of the cathode feed gas or the cathode exhaust.

### Claim 10

A fuel cell system, comprising:
a fuel cell, comprising:
an anode configured to receive anode feed gas and output anode exhaust; and
a cathode configured to receive cathode feed gas and output cathode exhaust;
a blower configured to receive the anode exhaust from the anode and to compress or accelerate the anode exhaust; and
an oxidizer configured to receive the anode exhaust from the blower, react the anode exhaust with air, and output the cathode feed gas to the cathode.

### Claim 11 (depends on 10)

The system according to claim 10, further comprising a turbine defining a turbine inlet configured to receive air from an air supply and a turbine outlet configured to output the air.

### Claim 12 (depends on 11)

The system according to claim 11, wherein:
at least a portion of the air output from the turbine outlet defines a bypass stream; and
the bypass stream is mixed directly with at least one of the cathode feed gas or the cathode exhaust.

### Claim 13

A method of balancing pressure between an anode and a cathode in a fuel cell, comprising:
providing a fuel cell having an anode outputting anode exhaust, and a cathode outputting cathode exhaust;
oxidizing the anode exhaust in the oxidizer to form a cathode feed gas;
increasing pressure of the anode exhaust or the cathode feed gas in a pressurizing assembly downstream from the anode; and
feeding the cathode feed gas to the cathode.

### Claim 14 (depends on 13)

The method according to claim 13, wherein the pressurizing assembly is a blower.

### Claim 15 (depends on 13)

The method according to claim 13, wherein the pressurizing assembly is an eductor having a nozzle at an inlet end and a diffuser at an outlet end; and further comprising:
feeding air and the anode exhaust to the nozzle;
mixing the air and the anode exhaust in the eductor; and
feeding the air and the anode exhaust from the eductor to an oxidizer.

### Claim 16 (depends on 15)

The method according to claim 15, further comprising providing a turbine having a turbine inlet configured to receive air from an air supply and a turbine outlet configured to output air.

### Claim 17 (depends on 15)

The method according to claim 15, further comprising feeding at least a portion of the air output from the turbine outlet to the nozzle.

### Claim 18 (depends on 15)

The method according to claim 15, further comprising:
providing a blower;
feeding ambient air to the blower;
compressing or accelerating the ambient air in the blower;
feeding the air from the blower to the nozzle for mixture with the anode exhaust.

### Claim 19 (depends on 15)

The method according to claim 15, further comprising feeding at least a portion of the air output from the turbine outlet directly to the oxidizer.

### Claim 20 (depends on 15)

The method according to claim 15, further comprising:
outputting a portion of the air in the turbine inlet as a slip stream;
feeding the slip stream directly from the turbine inlet to the nozzle.
