IP Library Granted Patent US 8,153,317
Granted Patent B2
US 8,153,317 · App. 12/286,473 · Granted Apr 10, 2012

Preheating heat exchanger for 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 8,153,317
App. No.
12/286,473
Granted
Apr 10, 2012
Kind
B2
Abstract

The invention relates to a heat exchanger for a hot fuel cell. The heat exchanger includes a first flow circuit for receiving a cool air stream and a second flow circuit for receiving a hot fluid coming from the cell, the first and second flow circuits having common surfaces for heat exchange. In accordance with the present invention, each of the first and second flow circuits comprises a plurality of concentric annular ducts that are interconnected. The two walls of each duct are mechanically decoupled from each other, thereby enabling them to expand independently of one another and avoiding mechanical stresses within the heat exchanger.

Claims (10)

1. A heat exchanger comprising a first flow circuit for receiving a cold fluid and a second flow circuit for receiving a hot fluid, the first and second flow circuits having common surfaces for heat exchange, the first and second flow circuits each comprising a plurality of interconnected concentric annular ducts each annular duct having a corresponding first wall and corresponding opposing, second wall, the first and second walls of each annular duct lacking a mechanical coupling to each other;

the heat exchanger presenting pairs of adjacent annular ducts belonging to the first flow circuit for the cold fluid successively alternating with pairs of adjacent annular ducts belonging to the second flow circuit for the hot fluid, each pair of adjacent annular ducts belonging to the first or second flow circuit forming a distribution baffle and having a layer of thermal insulation between each of the annular ducts of the pair.

2. A heat exchanger according to claim 1 , wherein one of the first and second walls of each annular duct includes a free end.

3. A heat exchanger according to claim 1 , including spacer studs disposed between the walls of the annular ducts of the first and second flow circuits.

4. A heat exchanger according to claim 1 , including a first layer of thermal insulation material placed around an outer periphery of said heat exchanger and a second layer of thermal insulation material placed on a top portion of said heat exchanger.

5. A heat exchanger according to claim 1 , including a first duct extending over an entire outer periphery of said heat exchanger, and a second duct extending substantially over a top portion of said heat exchanger so as to form a cooling circuit around said heat exchanger.

6. A heat exchanger according to claim 1 , wherein each of said first and second flow circuits has a length that is a function of at least one of the number and the height of the annular ducts.

7. A fuel cell device comprising:

a solid oxide fuel cell; and

a heat exchanger according to claim 1 , said heat exchanger including a central recess in which said cell is placed, the first flow circuit of said heat exchanger being suitable for feeding the fuel cell with a flow of preheated cool air, and the second flow circuit of said heat exchanger being suitable for exhausting a flow of hot depleted air coming from the fuel cell, the cool air stream being preheated by exchanging heat with the depleted air stream in said heat exchanger.

Assignments (2)
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 →