IP Library Granted Patent US 8,377,602
Granted Patent B2
US 8,377,602 · App. 12/171,554 · Granted Feb 19, 2013

System and a method for regulating the temperature of a fuel cell

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,377,602
App. No.
12/171,554
Granted
Feb 19, 2013
Kind
B2
Abstract

The invention relates to a system for regulating the temperature of a fuel cell that is cooled by a cooling fluid traveling through the cell, the system including both first control means for measuring the temperature of the cooling fluid and for controlling the flow rate of the controlling fluid as a function of said measured temperature of said cooling fluid, comprising second control means for measuring the flow rate of the cooling fluid and for controlling the temperature of the cooling fluid as a function of a flow rate difference between the command flow rate specified by said first control means and said corresponding measured flow rate of the cooling fluid such that said command temperature specified by the second control means compensates for said flow rate difference.

Claims (20)

1. A method of regulating the temperature of a fuel cell that is cooled by a cooling fluid passing through the cell via a cooling circuit, the method comprising the following steps:

measuring a temperature Tsm of the cooling fluid within the cooling circuit at an outlet of the fuel cell;

specifying a command flow rate Qc for said cooling fluid in said cooling circuit as a function of said temperature measurement;

applying the command flow rate Qc in said cooling circuit;

measuring an actual flow rate Qm of the cooling fluid within the cooling circuit;

comparing the measured flow rate Qm to the applied command flow rate Qc to determine a difference therebetween; and

establishing a command temperature Tec of the cooling fluid in the cooling circuit as a function of the difference between the measured actual flow rate Qm of the cooling fluid within the cooling circuit and the applied command flow rate Qc, to compensate for failure of fuel cell temperature regulation caused by said flow rate difference.

2. A method according to claim 1 , including a temperature correction step for correcting the command temperature Tec of the cooling fluid as a function of a difference between the command temperature Tec and a measured temperature Tem of the cooling fluid at the inlet of the fuel cell.

3. A method of regulating a temperature of a fuel cell that is cooled by a cooling fluid passing through the fuel cell via a cooling circuit, the method comprising:

providing a first control loop in the cooling circuit that is capable of:

measuring a temperature Tsm of the cooling fluid within the cooling circuit at an outlet of the fuel cell;

specifying a command flow rate Qc for said cooling fluid in said cooling circuit as a function of said temperature measurement; and

applying the command flow rate Qc in said cooling circuit; and

providing a second control loop in the cooling circuit that is capable of:

measuring an actual flow rate Qm of the cooling fluid within the cooling circuit; and

establishing a command temperature Tec of the cooling fluid in the cooling circuit as a function of a difference between the measured actual flow rate Qm of the cooling fluid within the cooling circuit and the applied command flow rate Qc, to compensate for failure of fuel cell temperature regulation caused by said flow rate difference.

4. A method according to claim 3 further comprising comparing the measured flow rate Qm to the applied command flow rate Qc to determine a difference therebetween.

5. A method according to claim 3 , including a temperature correction step for correcting the command temperature Tec of the cooling fluid as a function of a difference between the command temperature Tec and a measured temperature Tem of the cooling fluid at the inlet of the fuel cell.

6. A method according to claim 3 , wherein the second control loop is coupled to the first control loop.

7. A method according to claim 3 , wherein the temperature Tsm of the cooling fluid is measured at an outlet of the fuel cell and the command flow rate Qc is applied at an inlet of the fuel cell.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 26, 2008
From: LE GONIDEC, SERGE
To: SNECMA
Reel/Frame 021604/0736 →