Heat exchanger limiting the risk of contamination between two fluids and aircraft comprising at least one such heat exchanger

Patent metadata

Field	Value
Publication number	US-12078428-B2
Application number	US-202217879869-A
Country	US
Kind code	B2
Filing date	Aug 3, 2022
Priority date	Aug 5, 2021
Publication date	Sep 3, 2024
Grant date	Sep 3, 2024

Abstract

A heat exchanger including a sealed housing and a body positioned inside the housing, the body including a stack of least one first assembly of first and second plates pressed against each other, between which flows a first fluid, and at least one second assembly of third and fourth plates pressed against each other, between which flows a second fluid, the first and second assemblies being arranged so that they transfer heat between the first and second fluids. This configuration limits the risk of leaks and mixing of the two fluids.

First claim

The invention claimed is:

1. A plate heat exchanger transferring heat between first and second fluids, comprising:
a sealed housing, and
a body positioned inside the housing, said body including a stack of at least a first assembly of first and second plates pressed against each other, between which the first fluid flows, and at least a second assembly of third and fourth plates pressed against each other, between which the second fluid flows, the first and second assemblies being arranged so that they transfer heat between the first and second fluids,
wherein the first fluid is hydrogen and the housing comprises at least one sensor configured to detect a presence of hydrogen in the housing,
wherein the housing defines a cavity in which the body is positioned, the housing comprises an atmosphere, and the atmosphere is an inert atmosphere or a vacuum,
wherein the second fluid is a heat transfer fluid, and
wherein the housing has a first pair of orifices through which the first fluid flows to and from the first assembly, a second pair of orifices through which the second fluid flows to and from the second assembly, and a tapping point through which at least one of oxygen is extracted from the cavity or an inert gas is introduced into the cavity.

2. The heat exchanger as claimed in claim 1 ,
wherein each first assembly comprises at least one first peripheral rim around the first and second plates, and at least one first channel configured to channel the first fluid, positioned between the first and second plates and having a first end emerging on the first peripheral rim and a second end emerging on the first peripheral rim, and
wherein each second assembly comprises at least one second peripheral rim around the third and fourth plates, and at least one second channel configured to channel the second fluid, positioned between the third and fourth plates and having a first end emerging on the second peripheral rim and a second end emerging on the second peripheral rim.

3. The heat exchanger as claimed in claim 2 , wherein the body comprises a stack of a plurality of first assemblies and a plurality of second assemblies, the first and second assemblies being alternated, said stack including first and second faces on which the first and second ends of the first and second channels are distributed.

4. The heat exchanger as claimed in claim 3 , wherein the first ends of the first channels of the first assemblies are positioned on a first half of the first face and the second ends of the second channels of the second assemblies are positioned on a second half of the first face, and the second ends of the first channels of the first assemblies are positioned on a first half of the second face and the first ends of the second channels of the second assemblies are positioned on a second half of the second face.

5. The heat exchanger as claimed in claim 4 , wherein the body comprises:
a first leader having a first pipe and configured to connect said first pipe to the first ends of the first channels of the first assemblies,
a first manifold having a second pipe and configured to connect said second pipe to the second ends of the first channels of the first assemblies,
a second leader having a third pipe and configured to connect said third pipe to the first ends of the second channels of the second assemblies,
a second manifold having a fourth pipe and configured to connect said fourth pipe to the second ends of the second channels of the second assemblies.

6. The heat exchanger as claimed in claim 5 , wherein the heat exchanger comprises at least one double-skinned pipe including inner and outer pipes, and a connection system connecting the inner pipe of the double-skinned pipe and one of the first pipe of the first leader and the second pipe of the first manifold, the outer pipe of the double-skinned pipe being positioned outside the housing and having a collar pressed against the housing and sealably connected thereto around an orifice of the housing through which the inner pipe of the double-skinned pipe or the one of the first pipe of the first leader and the second pipe of the first manifold passes.

7. The heat exchanger as claimed in claim 5 , wherein at least one of the third pipe of the second leader and the fourth pipe of the second manifold has a collar positioned inside the housing, pressed against and sealably connected thereto around an orifice passing through the housing.

8. The heat exchanger as claimed in claim 1 , wherein the heat exchanger comprises a matrix made from an impermeable material in which the body is embedded.

9. The heat exchanger as claimed in claim 1 , wherein the first and second assemblies are pressed directly against each other.

10. The heat exchanger as claimed in claim 1 , wherein at least two first and second assemblies are spaced apart from each other and the body comprises at least one layer of thermally conductive material, interposed between the spaced apart first and second assemblies, transferring heat between them.

11. The heat exchanger as claimed in claim 1 , wherein the housing comprises at least one sensor configured to detect a presence of oxygen in the housing.

12. An aircraft comprising at least one heat exchanger as claimed in claim 1 .

Assignees

• Airbus Sas
• Airbus Operations Sas

Inventors

• Czapla Lionel
• Carretero Benignos Jorge A

Classifications

• F28F3/005

  Arrangements for preventing direct contact between different heat-exchange media (F28F3/10 takes precedence) · CPC title

• F28F9/005

  Other auxiliary members within casings, e.g. internal filling means or sealing means · CPC title

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• B64D37/32

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title

• B64D37/34

  Conditioning fuel, e.g. heating (during filling B64D37/18) · CPC title