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

Patent metadata

Field	Value
Publication number	US-10208669-B2
Application number	US-201414770681-A
Country	US
Kind code	B2
Filing date	Feb 24, 2014
Priority date	Feb 27, 2013
Publication date	Feb 19, 2019
Grant date	Feb 19, 2019

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.

First claim

The invention claimed is:

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.

Assignees

• Snecma
• Safran Aircraft Engines

Inventors

• Gameiro Sebastien
• Andre Brice
• Mathon Margueritte Guillaume
• Potel Nicolas

Classifications

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F02C7/14 Primary

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title

• F02C7/00 Primary

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title