IP Library Granted Patent US 10,208,669
Granted Patent B2
US 10,208,669 · App. 14/770,681 · Granted Feb 19, 2019

Method and device for regulating the cooling of oil in a turbomachine

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Quick Facts
Patent No.
US 10,208,669
App. No.
14/770,681
Granted
Feb 19, 2019
Kind
B2
Abstract

A method for regulating oil cooling within an oil cooling device of a turbomachine including a first heat exchanger mounted in series with a second heat exchanger, the first heat exchanger being an oil/air exchanger while the second heat exchanger is an oil/fuel exchanger, each heat exchanger having an oil inlet and an oil outlet, a bypass directly connecting the oil inlet of the first heat exchanger to the oil outlet of the first heat exchanger, and a flow regulator to regulate the flow rate of oil flowing through the bypass. Circulation of oil though the bypass is allowed by means of the flow regulator when the oil temperature is less than or equal to a predetermined temperature comprised between 70° C. and 90° C., preferably equal to about 80° C.

Claims (17)

1. A method for regulating oil cooling within an oil cooling device of a turbomachine including a first heat exchanger mounted in series with a second heat exchanger, the first heat exchanger being an oil/air exchanger and the second heat exchanger being an oil/fuel exchanger, each heat exchanger having an oil inlet and an oil outlet, a bypass directly connecting the oil inlet of the first heat exchanger to the oil outlet of the first heat exchanger, and a flow regulator to regulate a flow rate of oil flowing through the bypass, the flow regulator including a thermal valve and a pressure valve arranged in parallel, the method comprising:

opening the thermal valve when temperature of the oil is less than or equal to a predetermined temperature comprised between 70° C. and 90° C. so that the oil circulates through the bypass;

opening the pressure valve when a ratio between a nominal head loss of the first heat exchanger and an effective head loss between the oil inlet and the oil outlet of the first heat exchanger is less than or equal to a predetermined ratio comprised between 0.7 and 0.9 so that the oil circulates through the bypass; and

closing the thermal valve when the temperature of the oil is greater than the predetermined temperature and closing the pressure valve when the ratio is greater than the predetermined ratio so that the oil circulates through the first heat exchanger.

2. The method according to claim 1 , wherein the flow rate of oil circulating through the bypass when the ratio is less than or equal to the predetermined ratio and the temperature of the oil is greater than the predetermined temperature is less than the flow rate of oil circulating through the bypass when the temperature of the oil is less than the predetermined temperature.

3. The method according to claim 1 , wherein the predetermined temperature is equal to 80° C.

4. The method according to claim 1 , wherein the predetermined ratio is equal to 0.8.

5. An oil cooling device for a turbomachine comprising:

a first heat exchanger mounted in series with a second heat exchanger, the first heat exchanger being an oil/air exchanger and the second heat exchanger being an oil/fuel exchanger, each heat exchanger having an oil inlet and an oil outlet;

a bypass directly connecting the oil inlet of the first heat exchanger to the oil outlet of the first heat exchanger; and

a flow regulator to regulate a flow rate of oil flowing through the bypass,

wherein the flow regulator includes

a thermal valve which is open when an oil temperature is less than a predetermined temperature comprised between 70° C. and 90° C., and which is closed when the oil temperature is greater than the predetermined temperature, and

a pressure valve arranged in parallel with the thermal valve, the pressure valve is open when a ratio between a nominal head loss of the first heat exchanger and an effective head loss between the oil inlet and the oil outlet of the first heat exchanger is less than or equal to a predetermined ratio comprised between 0.7 and 0.9, and which is closed when the ratio is greater than the predetermined ratio.

6. A turbomachine including an oil cooling device according to claim 5 .

7. The device according to claim 5 , wherein the predetermined temperature is equal to 80° C.

8. The device according to claim 5 , wherein the predetermined ratio is equal to 0.8.

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 Aug 26, 2015
From: GAMEIRO, SEBASTIEN; ANDRE, BRICE; MATHON MARGUERITTE, GUILLAUME; POTEL, NICOLAS
To: SNECMA
Reel/Frame 036428/0660 →