IP Library Granted Patent US 8,470,168
Granted Patent B2
US 8,470,168 · App. 12/920,182 · Granted Jun 25, 2013

Heat exchanger system

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Quick Facts
Patent No.
US 8,470,168
App. No.
12/920,182
Granted
Jun 25, 2013
Kind
B2
Abstract

A heat exchanger system through which a liquid can flow, including a heat exchanger including a liquid inlet and a liquid outlet, a bypass valve including a liquid inlet and a liquid outlet, and a self-cleaning filter including a liquid inlet and two liquid outlets, one being an outlet for filtered liquid and one being an outlet for non-filtered liquid. The outlet for filtered liquid is connected to the inlet of the exchanger and the outlet for non-filtered liquid is connected to the inlet of the valve. The outlet of the heat exchanger is connected downstream of the outlet of the valve. A fuel circuit of an airplane jet engine can include such a system.

Claims (13)

1. A heat exchanger system through which a liquid can flow, comprising:

a heat exchanger including a liquid inlet and a liquid outlet;

a bypass valve including a liquid inlet and a liquid outlet; and

a self-cleaning filter including a filtering membrane, a liquid inlet, and first and second liquid outlets, the first outlet being an outlet for filtered liquid and the second outlet being an outlet for non-filtered liquid, the first outlet for filtered liquid being connected to the inlet of the exchanger and the second outlet for non-filtered liquid being connected to the inlet of the valve, and the outlet of the exchanger being connected downstream of the outlet of the valve,

wherein the bypass valve is open when a pressure at the second outlet for non-filtered liquid is greater than a predetermined value due to impurities in the filter, the impurities being removed by a flow of liquid when the bypass value us open.

2. The heat exchanger system according to claim 1 , wherein the filtering membrane has a tubular shape around an axis, liquid withdrawn through the first outlet for filtered liquid passes through the filtering membrane, and liquid withdrawn through the second outlet for non-filtered liquid passes inside the filtering membrane along the axis.

3. The heat exchanger system according to claim 2 , wherein the inlet of the self-cleaning filter is situated at a first end of the filtering membrane, the second outlet for non-filtered liquid is situated at a second end of the filtering membrane, and the first outlet for filtered liquid is situated on a side of the filtering membrane.

4. The heat exchanger system according to claim 1 , wherein the heat exchanger is a plate exchanger.

5. A fuel circuit of a turbomachine, the fuel circuit comprising a heat exchanger system according to claim 1 .

6. The fuel circuit according to claim 5 , wherein the heat exchanger system is situated upstream of a main filter of the circuit.

7. The fuel circuit according to claim 5 , wherein the heat exchanger system is situated downstream of a low-pressure fuel pump of the circuit.

8. The fuel circuit according to claim 5 , wherein the self-cleaning filter includes a weave between 55 and 75 microns.

9. A turbomachine comprising a fuel circuit according to claim 5 .

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 →