IP Library Granted Patent US 10,069,150
Granted Patent B2
US 10,069,150 · App. 14/697,368 · Granted Sep 4, 2018

Alternative path cooling of a high temperature fuel cell

Inventors: Marianne E. Mata (Dana Point, CA); Tina R. Stoia (Rancho Santa Margarita, CA); Chellappa Balan (Niskayuna, NY)
Assignee: The Boeing Company
H01M8/04014H01M8/04074H01M8/04111H01M8/04708H01M2008/1293H01M2250/20H01M2250/402Y02B90/12Y02E60/50Y02E60/525Y02T90/32
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Quick Facts
Patent No.
US 10,069,150
App. No.
14/697,368
Granted
Sep 4, 2018
Kind
B2
Abstract

Systems and methods provide for the thermal management of a high temperature fuel cell. According to embodiments described herein, a non-reactant coolant is routed into a fuel cell from a compressor or a ram air source. The non-reactant coolant absorbs waste heat from the electrochemical reaction within the fuel cell. The heated coolant is discharged from the fuel cell and is vented to the surrounding environment or directed through a turbine. The energy recouped from the heated coolant by the turbine may be used to drive the compressor or a generator to create additional electricity and increase the efficiency of the fuel cell system. A portion of the heated coolant may be recycled into the non-reactant coolant entering the fuel cell to prevent thermal shock of the fuel cell.

Claims (22)

1. A method for thermally managing a fuel cell provided on a vehicle, with an ambient environment surrounding the vehicle, the method comprising:

directing oxygen to a reactant portion of the fuel cell from an oxygen source continuously closed from the ambient environment surrounding the vehicle;

directing fuel to the reactant portion of the fuel cell from a fuel source continuously closed from the ambient environment surrounding the vehicle;

utilizing the oxygen and fuel in a chemical reaction within the reactant portion of the fuel cell to create a product and waste heat;

capturing a non-reactant ambient coolant from the ambient environment surrounding the vehicle;

directing an entire portion of the non-reactant ambient coolant to a non-reactant portion of the fuel cell, wherein the non-reactant portion of the fuel cell is thermally coupled to, and isolated from direct fluid communication with, the reactant portion of the fuel cell, so that the non-reactant ambient coolant is completely isolated from the oxygen and fuel, the non-reactant ambient coolant absorbing a portion of the waste heat from the reactant portion of the fuel cell to create heated coolant; and

directing the heated coolant from the non-reactant portion of the fuel cell.

2. The method of claim 1 , wherein directing an entire portion of the non-reactant ambient coolant to the non-reactant portion of the fuel cell comprises directing ram air through the non-reactant portion of the fuel cell to create heated air.

3. The method of claim 1 , wherein directing an entire portion of the non-reactant ambient coolant to the non-reactant portion of the fuel cell comprises directing ambient airflow through a compressor configured to pressurize the ambient airflow and to direct the ambient airflow to the non-reactant portion of the fuel cell.

4. The method of claim 3 , further comprising directing the heated coolant from the non-reactant portion of the fuel cell, in the form of heated ambient airflow, through a turbine configured to drive the compressor.

5. The method of claim 1 , further comprising directing the heated coolant from the non-reactant portion of the fuel cell through a turbine configured to create mechanical energy from a flow of the heated coolant, wherein the turbine is coupled to a generator, enabling production of electricity from the mechanical energy created by the turbine.

6. The method of claim 1 , further comprising directing a portion of the heated coolant from the non-reactant portion of the fuel cell to the non-reactant ambient coolant prior to directing the non-reactant ambient coolant to the non-reactant portion of the fuel cell to increase a temperature of the non-reactant ambient coolant and decrease a temperature differential between the non-reactant ambient coolant and the reactant portion of the fuel cell.

7. A method for thermally managing a fuel cell provided on a vehicle, with an ambient environment surrounding the vehicle, the method comprising:

directing oxygen to a reactant portion of the fuel cell from an oxygen source continuously closed from the ambient environment surrounding the vehicle;

directing fuel to the reactant portion of the fuel cell from a fuel source continuously closed from the ambient environment surrounding the vehicle, wherein the oxygen and fuel chemically react within the reactant portion of the fuel cell to create a product and waste heat;

directing a non-reactant airflow, from the ambient environment surrounding the vehicle through a compressor operative to pressurize the non-reactant airflow;

directing an entire portion of the non-reactant airflow pressurized in the compressor to a non-reactant portion the fuel cell, wherein the non-reactant portion of the fuel cell is thermally coupled to, and isolated from direct fluid communication with, the reactant portion of the fuel cell, so that the non-reactant ambient coolant is completely isolated from the oxygen and fuel;

transferring waste heat from the reactant portion of the fuel cell to the non-reactant airflow via the non-reactant portion of the fuel cell to create a waste heat airflow;

directing the waste heat airflow out of the non-reactant portion of the fuel cell to a turbine to create mechanical energy; and

utilizing the mechanical energy from the turbine to drive the compressor.

8. The method of claim 7 , further comprising utilizing the mechanical energy from the turbine to drive a generator.

9. The method of claim 7 , further comprising recirculating a portion of the waste heat airflow to the non-reactant airflow prior to directing an entire portion of the non-reactant airflow from the compressor to the non-reactant portion of the fuel cell to increase a temperature of the non-reactant airflow and decrease a temperature differential between the non-reactant airflow and the reactant portion of the fuel cell.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 15, 2017
From: MATA, MARIANNE E.; STOIA, TINA R.; BALAN, CHELLAPPA
To: THE BOEING COMPANY
Reel/Frame 041263/0127 →
Continuity (3)
Division 12401262 · Mar 10, 2009
Provisional Application 61046052 · Apr 18, 2008
Related Publication 20150244005A1 · Aug 27, 2015
Cited By (11)
US 12,202,616 US 12,240,613 US 12,261,334 US 12,270,340 US 12,301,002 US 12,351,329 US 12,412,914 US 12,428,164 US 12,567,595 US 12,573,647 US 12,584,445