IP Library Granted Patent US 9,708,981
Granted Patent B2
US 9,708,981 · App. 15/233,990 · Granted Jul 18, 2017

Method and device for supplying a lubricant

Inventor: Philippe Alain Francois Augros (Serres-Morlaas, FR)
Assignee: SAFRAN HELICOPTER ENGINES
F02C7/06F01D25/10F01D25/125F01D25/18F01D25/20F01M5/001F01M5/002F16C33/66F05D2220/329F05D2260/98
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Quick Facts
Patent No.
US 9,708,981
App. No.
15/233,990
Granted
Jul 18, 2017
Kind
B2
Abstract

A device and method feeding turbomachines with lubricant, the turbomachine including a first set of bearings and a second set of bearings. Both the first and the second sets of bearings are fed with lubricant, and the second set of bearings operate at a temperature higher than the first set. The second set of bearings is fed with lubricant at a temperature higher than the first set.

Claims (9)

1. A lubricant feed method for feeding a turbomachine with lubricant, said turbomachine having at least a first set of bearings and a second set of bearings, both the first and the second set being fed with lubricant, and the second set of bearings operating at a bearing temperature that is higher than a bearing temperature of the first set, the method comprising a step of heating a lubricant flow upstream from the second set of bearings by exchanging heat with a flow of lubricant returning from the second set of bearings, so that the second set of bearings is fed with lubricant at a lubricant temperature that is higher than a lubricant temperature of lubricant fed to the first set of bearings.

2. The lubricant feed method according to claim 1 , further comprising a step of cooling a flow of lubricant in a heat exchanger upstream from the first set of bearings.

3. The lubricant feed method according to claim 1 , wherein the first set of bearings is fed with lubricant by a first circuit, and the second set of bearings is fed with lubricant by a second circuit branching from the first circuit.

4. A lubricant feed device for feeding a turbomachine with lubricant, said turbomachine comprising a first set of bearings and a second set of bearings, and said second set operating at a bearing temperature that is higher than a bearing temperature of said first set, the lubricant feed device comprising a first circuit for feeding lubricant to the first set of bearings, and a second circuit for feeding lubricant to the second set of bearings, the first circuit having a branch point leading to the second circuit, and the second circuit having a heat exchanger for transmitting heat from at least a flow of lubricant returning from the second set of bearings to a flow of lubricant for feeding the second set of bearings, so as to feed the second set of bearings with lubricant at a lubricant temperature that is higher than a lubricant temperature of lubricant fed to the first set of bearings.

5. The lubricant feed device according to claim 4 , wherein the first circuit includes a heat exchanger between said branch point and the first set of bearings in order to cool a flow of lubricant for the first set of bearings.

6. A turbomachine comprising a first set of bearings, a second set of bearings operating at a temperature higher than the first set of bearings, and a lubricant feed device comprising a first circuit for feeding lubricant to the first set of bearings, and a second circuit for feeding lubricant to the second set of bearings, the first circuit having a branch point leading to the second circuit, and the second circuit having a heat exchanger for transmitting heat from at least a flow of lubricant returning from the second set of bearings to a flow of lubricant for feeding the second set of bearings, so as to feed the second set of bearings with lubricant at a lubricant temperature that is higher than a lubricant temperature of lubricant fed to the first set of bearings.

7. The turbomachine according to claim 6 , wherein the first circuit includes a heat exchanger between said branch point and the first set of bearings in order to cool a flow of lubricant for the first set of bearings.

8. A turbine engine assembly, or a turbine engine assembly for aviation purposes, including a turbomachine comprising a first set of bearings, a second set of bearings operating at a temperature higher than the first set of bearings, and a lubricant feed device comprising a first circuit for feeding lubricant to the first set of bearings, and a second circuit for feeding lubricant to the second set of bearings, the first circuit having a branch point leading to the second circuit, and the second circuit having a heat exchanger for transmitting heat from at least a flow of lubricant returning from the second set of bearings to a flow of lubricant for feeding the second set of bearings, so as to feed the second set of bearings with lubricant at a lubricant temperature that is higher than a lubricant temperature of lubricant fed to the first set of bearings.

9. The turbine engine assembly according to claim 8 , wherein the first circuit includes a heat exchanger between said branch point and the first set of bearings in order to cool a flow of lubricant for the first set of bearings.

Assignments (1)
CHANGE OF NAME Recorded Jun 9, 2017
From: TURBOMECA
To: SAFRAN HELICOPTER ENGINES
Reel/Frame 042755/0202 →
Priority Claims (1)
FR 11 50421 · Jan 19, 2011 · national
Continuity (2)
Division 13980696
Related Publication 20160348583A1 · Dec 1, 2016