Compact heat exchange device incorporated into an aircraft pylon

Patent metadata

Field	Value
Publication number	US-10746100-B2
Application number	US-201816129499-A
Country	US
Kind code	B2
Filing date	Sep 12, 2018
Priority date	Sep 14, 2017
Publication date	Aug 18, 2020
Grant date	Aug 18, 2020

Abstract

A heat exchange device to be positioned in an aircraft pylon and including a heat exchanger and an obturator to adopt a closed state where it prevents flow of air from flowing through the heat exchanger, and more- or less-permissive states where it allows flow of air to flow with a higher or lower flow rate. The obturator includes slats each including a pivot axis, the pivot axes of the various slats being mutually parallel and intersecting the direction of the flow of air, the slats being simultaneously mobile in rotation about their pivot axis between a closed position in which the slats are contiguous, which corresponds to the closed state of the obturator, and an open position in which the slats are spread apart, which corresponds to the permissive state of the obturator.

First claim

The invention claimed is:

1. A heat exchange device configured to be positioned in an aircraft pylon and comprising:
a heat exchanger which comprises a first hot air circuit connecting a first inlet and a first outlet, and a second cold air circuit connecting a second inlet and a second outlet that is extended by an exhaust duct;
a regulating system configured to adjust a flow rate of a flow of air flowing in the second cold air circuit of the heat exchanger, and that comprises:
an obturator configured to adopt a closed state in which the obturator prevents the flow of air from flowing, and permissive states in which the obturator allows the flow of air to flow with a higher or lower flow rate; and
an actuator configured to control a state of the obturator,

wherein the obturator comprises a plurality of slats, each of the slats comprising a pivot axis, the pivot axes of the slats being mutually parallel and intersecting a direction of the flow of air, the slats being simultaneously mobile in rotation about their pivot axis between a closed position in which the slats are contiguous, which corresponds to the closed state of the obturator, and an open position in which the slats are spread apart, which corresponds to the permissive state of the obturator.

2. The heat exchange device according to claim 1 , wherein the obturator is positioned downstream of the heat exchanger.

3. The heat exchange device according to claim 2 , wherein the second outlet of the heat exchanger has a square or rectangular cross section,
wherein the obturator comprises a frame positioned between the second outlet and the exhaust duct, the frame having two longitudinal walls and two transverse walls while having a passage cross section essentially identical to that of the second outlet of the heat exchanger, and
wherein ends of the pivot axes of the slats are mounted so as to be able to pivot with respect to the longitudinal walls of the frame.

4. The heat exchange device according to claim 1 , wherein the obturator comprises, for each slat, an arm extending in a direction perpendicular to the pivot axis and having a first end rigidly connected to one of the ends of the pivot axis of the slat, all the arms of the various slats being connected to a single bar which is connected to the actuator.

5. The heat exchange device according to claim 1 , wherein the actuator is configured to displace the bar in a displacement direction which is approximately parallel to a portion of a supply duct connected to the first inlet, the bar and the actuator being arranged in a direction parallel to the displacement direction.

6. The heat exchange device according to claim 4 , wherein the actuator is configured to displace the bar in a displacement direction which is approximately parallel to a portion of a hot air outlet duct connected to the first outlet, the bar and the actuator being arranged in a direction parallel to the displacement direction.

7. An aircraft pylon comprising a heat exchange device configured to be positioned in an aircraft pylon, the heat exchange device comprising:
a heat exchanger which comprises a first hot air circuit connecting a first inlet and a first outlet, and a second cold air circuit connecting a second inlet and a second outlet that is extended by an exhaust duct;
a regulating system configured to adjust a flow rate of a flow of air flowing in the second cold air circuit of the heat exchanger, and that comprises:
an obturator configured to adopt a closed state in which the obturator prevents the flow of air from flowing, and permissive states in which the obturator allows the flow of air to flow with a higher or lower flow rate; and
an actuator configured to control a state of the obturator,

wherein the obturator comprises a plurality of slats, each of the slats comprising a pivot axis, the pivot axes of the slats being mutually parallel and intersecting a direction of the flow of air, the slats being simultaneously mobile in rotation about their pivot axis between a closed position in which the slats are contiguous, which corresponds to the closed state of the obturator, and an open position in which the slats are spread apart, which corresponds to the permissive state of the obturator.

8. An aircraft comprising an aircraft pylon according to claim 7 .

Assignees

• Airbus Operations Sas

Inventors

• Combes Stéphane
• Geliot Jean
• Deforet Thomas
• Soulie Adeline
• Orteu Benoit

Classifications

• B64D13/08 Primary

  the air being heated or cooled · CPC title

• B64D33/08 Primary

  of power plant cooling systems · CPC title

• B64D15/04

  Hot gas application · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2260/213

  by the provision of a heat exchanger within the cooling circuit · CPC title