Heat exchanger

Patent metadata

Field	Value
Publication number	US-9702630-B2
Application number	US-201515125710-A
Country	US
Kind code	B2
Filing date	Mar 11, 2015
Priority date	Mar 13, 2014
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

A heat exchanger ( 2 ) comprising a duct ( 4 ) through which a first fluid (e.g. a coolant such as ram air) may flow, and one or more vanes ( 18 ) disposed within the duct ( 4 ) and configured to disrupt the flow of the first fluid through the duct ( 4 ). Each vane ( 18 ) comprises one or more flow channels ( 24 ) through which a second fluid (e.g. a fluid to be cooled, such as engine coolant) may flow so as to transfer heat between the first fluid flowing through the duct ( 4 ) and the second fluid flowing through the one or more flow channels ( 24 ). The flow channels ( 24 ) within the vanes ( 18 ) are separated from the duct ( 4 ) by a channel wall such that fluid cannot flow between the duct ( 4 ) and the flow channels ( 24 ).

First claim

What is claimed is:

1. A heat exchanger ( 2 ) comprising:
an outer cylindrical portion ( 4 ) comprising a duct through which a first fluid may flow; and
one or more anti-swirl vanes ( 18 ) disposed within the duct and configured to disrupt the flow of the first fluid through the duct; wherein
each vane ( 18 ) comprises:
one or more first flow channels ( 22 ), the one or more first flow channels ( 22 ) being in fluid communication with the duct such that the first fluid flowing through the duct may flow through the one or more first flow channels ( 22 ); and
one or more second flow channels ( 24 ) through which a second fluid may flow so as to transfer heat between the first fluid and the second fluid;

the one or more second flow channels ( 24 ) are separated from the duct and the one or more first flow channels ( 22 ) by at least one channel wall, respectively, such that fluid cannot flow between the duct and the one or more second flow channels or between the one or more first flow channels and the one or more second flow channels ( 24 ).

2. The heat exchanger ( 2 ) according to claim 1 , wherein the at least one channel wall forms a channel wall of each second flow channel ( 24 ) and each first flow channel ( 22 ).

3. The heat exchanger ( 2 ) according to claim 1 , the heat exchanger ( 2 ) further comprising means ( 16 ) configured to divert at least some of the first fluid flowing through the duct into each first flow channel ( 22 ) of each vane ( 18 ).

4. The heat exchanger ( 2 ) according to claim 1 , wherein
the duct comprises a duct wall positioned in the duct;
the duct wall comprises a first cavity in fluid communication with each first flow channel ( 22 ) of each vane ( 18 ).

5. The heat exchanger ( 2 ) according to claim 1 , wherein
the outer cylindrical portion ( 4 ) comprises a wall;
the wall comprises:
a second cavity;
an inlet ( 10 ) through which the second fluid may enter the second cavity; and
an outlet ( 12 ) through which the second fluid may exit the second cavity; and

the second cavity is in fluid communication with each second flow channel ( 24 ) of each vane ( 18 ).

6. The heat exchanger ( 2 ) according to claim 5 , wherein
the second cavity is partitioned into two separate chambers;
the inlet ( 10 ) is an inlet to a first of the two chambers;
the outlet ( 12 ) is an outlet from a second of the two chambers; and
the two separate chambers are connected via each second flow channel ( 24 ) of each vane ( 18 ) such that the second fluid flowing from the inlet ( 10 ) to the outlet ( 12 ) passes through each second flow channel ( 24 ) of each vane ( 18 ).

7. The heat exchanger ( 2 ) according to claim 1 , wherein
the heat exchanger ( 2 ) further comprises a tube ( 14 ) located within and coaxially with the duct, the tube ( 14 ) having a smaller diameter than the duct; and
the one or more vanes ( 18 ) are attached between an inner surface of the outer cylindrical portion ( 4 ) and an outer surface of the tube ( 14 ).

8. The heat exchanger ( 2 ) according to claim 7 , wherein an inlet ( 26 ) of each first flow channel ( 22 ) of each vane ( 18 ) is located on an inner surface of the tube ( 14 ).

9. An aircraft comprising a heat exchanger ( 2 ), the heat exchanger ( 2 ) being in accordance with claim 1 .

10. The aircraft according to claim 9 , wherein
the first fluid is air; and
the heat exchanger ( 2 ) is arranged on the aircraft such that forward motion of the aircraft causes air to be forced through the duct.

11. The aircraft according to claim 10 , wherein the heat exchanger ( 2 ) is located at a main intake duct of an engine of the aircraft, such that prior to entering the engine, air passes through the heat exchanger ( 2 ).

12. The aircraft according to claim 9 , wherein
the second fluid is aircraft systems coolant; and
the aircraft comprises:
means to move aircraft systems coolant, from an aircraft system remote from the heat exchanger ( 2 ), through the one or more second flow channels ( 24 ); and
means to return aircraft systems coolant that has been passed through the one or more second flow channels ( 24 ) to the aircraft system.

13. A method of transferring heat between a first fluid and a second fluid, the method comprising:
providing an outer cylindrical portion ( 4 ) comprising a duct;
disposing one or more anti-swirl vanes ( 18 ) within the duct, the one or more anti-swirl vanes ( 18 ) being configured to disrupt a fluid flow through the duct, each vane ( 18 ) comprising:
one or more first flow channels ( 22 ), the one or more first flow channels ( 22 ) being in fluid communication with the duct such that the first fluid flowing through the duct may flow through the one or more first flow channels ( 22 ); and
one or more second flow channels ( 24 ), the one or more second flow channels ( 24 ) being separated from the duct and the one or more first flow channels ( 22 ) by at least one channel wall, respectively, such that fluid cannot flow between the duct and the one or more second flow channels ( 24 ) or between the one or more first flow channels ( 22 ) and the one or more second flow channels ( 24 );

causing the first fluid to flow through the duct and through the one or more first flow channels ( 22 ); and,
simultaneously with the first fluid flowing through the duct and the one or more first flow channels ( 22 ), causing the second fluid to flow through the one or more second flow channels ( 24 ), thereby causing heat to be transferred between the first fluid and the second fluid.

14. The method according to claim 13 , wherein at least one channel wall forms a channel wall of each second flow channel ( 24 ) and each first flow channel ( 22 ).

15. An anti-swirl vane ( 18 ) for disrupting fluid flow in a duct in which the vane ( 18 ) is placed, the vane ( 18 ) comprising:
one or more first flow channels ( 22 ) through which a first fluid flows;
one or more second flow channels ( 24 ) through which a second fluid flows; wherein
each second flow channel ( 24 ) is different from the one or more first flow channels ( 22 ); and

at least one channel wall of each second flow channel ( 24 ) forms a channel wall of at least one of the one or more first flow channels ( 22 );
wherein the one or more second flow channels ( 24 ) are separated from the duct and the one or more first flow channels ( 22 ) by the at least one channel wall, respectively, such that fluid cannot flow between the duct and the one or more second flow channels or between the one or more first flow channels ( 22 ) and the one or more second flow channels ( 24 ).

Assignees

• Bae Systems Plc

Inventors

• Whaites Colin
• Smith Stephen John Richard
• Townsley Andrew Mark

Classifications

• F28D7/0058

  the conduits for only one medium being tubes having different orientations to each other or crossing the conduit for the other heat exchange medium (F28D7/0008 takes precedence) · CPC title

• F02C7/185

  Cooling means for reducing the temperature of the cooling air or gas · CPC title

• B64D13/00

  Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space · CPC title

• F28D7/0008 Primary

  the conduits for one medium being in heat conductive contact with the conduits for the other medium · CPC title

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title