IP Library › Granted Patent US 11,181,322
Granted Patent B2
US 11,181,322 · App. 16/719,571 · Granted Nov 23, 2021

Fuel-oil heat exchanger

Inventors: Roxane Koeune (Herstal, BE); Nicolas Fellin (Herstal, BE)
Assignee: SAFRAN AERO BOOSTERS SA
F28D7/10
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Quick Facts
Patent No.
US 11,181,322
App. No.
16/719,571
Granted
Nov 23, 2021
Kind
B2
Abstract

A turbine engine heat exchanger for exchanging heat between a first fluid and a second fluid includes a reference axis, a network of tubular meshes having a plurality of meshes each of which is formed, successively in a reference direction, of at least two curvilinear branches, called anterior branches, of a junction where the two anterior branches meet, and of at least two curvilinear branches, called posterior branches, diverging from the junction, wherein the meshes are stacked in staggered rows.

Claims (18)

1. A heat exchanger between a first fluid and a second fluid, the heat exchanger comprising:

a reference direction; and

a network of tubes delimiting an inner passage for the first fluid, the network comprising:

a plurality of meshes, each of the meshes, being formed, successively according to the reference direction, of at least two curvilinear branches, called anterior branches, of a junction where the two anterior branches meet, and of at least two curvilinear branches, called posterior branches, diverging from the junction;

wherein the plurality of meshes includes at least one first mesh, at least one second mesh and at least one third mesh distinct from the second mesh;

wherein at least one anterior branch of the first mesh is connected to at least one posterior branch of the second mesh and at least one other anterior branch of the first mesh is connected to at least one posterior branch of the third mesh; and

wherein the network of tubular meshes is arranged between an inlet manifold and an outlet manifold.

2. The heat exchanger according to claim 1 , wherein the plurality of meshes comprises:

a stack of 5 to 40 meshes successively arranged in the reference direction.

3. The heat exchanger according to claim 1 , wherein the plurality of meshes comprises:

between 200 and 3000 meshes.

4. The heat exchanger according to claim 1 , wherein the branches and junctions are formed by walls having a thickness of between 0.4 and 0.8 mm.

5. The heat exchanger according to claim 1 , wherein at least one of the meshes comprises:

a number of anterior branches that is different from the number of its posterior branches.

6. The heat exchanger according to claim 1 , wherein the number of branches of each mesh is 6.

7. The heat exchanger according to claim 1 , wherein at least one of the meshes supports at least one internal or external fin.

8. The heat exchanger according to claim 1 , wherein the heat exchanger is a one-piece part made by additive manufacturing based on aluminium powder.

9. The heat exchanger according to claim 1 , wherein the first fluid is fuel and the second fluid is oil.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 31, 2020
From: KOEUNE, ROXANE
To: SAFRAN AERO BOOSTERS SA
Reel/Frame 051688/0818 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 31, 2020
From: FELLIN, NICOLAS
To: SAFRAN AERO BOOSTERS SA
Reel/Frame 051688/0953 →
Priority Claims (1)
BE 2018/5931 · Dec 21, 2018 · national
Continuity (1)
Related Publication 20200200482A1 · Jun 25, 2020