Cross-flow heat exchanger having graduated fin density

Patent metadata

Field	Value
Publication number	US-9377250-B2
Application number	US-201213665396-A
Country	US
Kind code	B2
Filing date	Oct 31, 2012
Priority date	Oct 31, 2012
Publication date	Jun 28, 2016
Grant date	Jun 28, 2016

Abstract

The heat transfer capacity of a cross-flow heat exchanger can be increased by changing or graduating the density of the fins that form a row of hot passages in the direction normal to those fins. In accordance with some embodiments, the fin density in each row of hot passages is lower in a first region near the cold air inlets than it is in a second region located between the first region and the cold air outlets. This has the beneficial effect of increasing the rate of flow of hot air through hot passages adjacent or near to the cold air inlets of the heat exchanger, i.e., where the temperature of the cold air is coldest. As cold air flows along each cold passage, the cold air is heating up, becoming less capable of cooling the hot air in the adjacent hot passages as it gets closer to the cold air outlets. In addition or alternatively, the cold passages may have a non-uniform fin density that increases heat transfer capacity.

First claim

The invention claimed is:

1. A system comprising a source of relatively colder fluid, a source of relatively hotter fluid, and a cross-flow fluid-to-fluid heat exchanger connected to receive fluid from said source of relatively colder fluid and said source of relatively hotter fluid, wherein said heat exchanger comprises:
a first multiplicity of fins which partly define a first row of passages arranged side by side and aligned in a first direction, each passage of said first row having a fluid inlet connected to receive fluid from said source of relatively hotter fluid, a fluid outlet in fluid communication with said fluid inlet, and a constant height along its length;
a second multiplicity of fins which partly define a second row of passages arranged side by side and aligned in a second direction that is not parallel with said first direction, each passage of said second row having a fluid inlet connected to receive fluid from said source of relatively colder fluid, a fluid outlet in fluid communication with said fluid inlet, and a constant height along its length; and
a first planar plate disposed between said first and second rows of passages,
wherein said first and second rows of passages and said first planar plate form a stack in which respective portions of each passage of said first row are disposed above respective portions of respective passages of said second row in a cross-flow relationship that allows heat to be transferred from any one passage of said first row to all of the passages of said second row; and
wherein said first multiplicity of fins have a first fin density in a first region occupied by some passages of said first row of passages and a second fin density in a second region occupied by other passages of said first row of passages, said first fin density being less than said second fin density, said first region being between said second region and a first side of the heat exchanger where said fluid inlets of said second row of passages are located.

2. The system as recited in claim 1 , further comprising:
a third multiplicity of fins which partly define a third row of passages arranged side by side and aligned in said first direction, each passage of said third row having a fluid inlet connected to receive fluid from said source of relatively hotter fluid, a fluid outlet in fluid communication with said fluid inlet, and a constant height along its length; and
a second planar plate disposed between said second and third rows of passages,
wherein said first, second and third rows of passages and said first and second planar plates form a stack in which respective portions of each passage of said third row are disposed below respective portions of respective passages of said second row in a cross-flow relationship that allows heat to be transferred from any one passage of said third row to all of the passages of said second row; and
wherein said third multiplicity of fins have said first fin density in a first region occupied by some passages of said third row of passages and said second fin density in a second region occupied by other passages of said third row of passages, said first region being between said second region and said first side of the heat exchanger.

3. The system as recited in claim 1 , wherein said second multiplicity of fins have a third fin density in a first region occupied by some passages of said second row of passages and a fourth fin density in a second region occupied by other passages of said second row of passages, said third fin density being less than said fourth fin density, said first region being between said second region and a second side of the heat exchanger where said fluid inlets of said first row of passages are located.

4. The system as recited in claim 1 , wherein said fluid is air.

5. The system as recited in claim 1 , wherein said source of relatively colder fluid is a fan duct of a gas turbine engine.

6. The system as recited in claim 1 , wherein said source of relatively hotter fluid is a compressor of a gas turbine engine.

7. The system as recited in claim 1 , further comprising an environmental control system connected to receive fluid from said fluid outlets of said first row of passages.

8. A system comprising a source of relatively colder air, a source of relatively hotter air, and a cross-flow air-to-air heat exchanger connected to receive air from said source of relatively colder air and said source of relatively hotter air, wherein said heat exchanger comprises:
a first multiplicity of fins which partly define a first row of passages arranged side by side and aligned in a first direction, each passage of said first row having an air inlet connected to receive air from said source of relatively hotter air, an air outlet in fluid communication with said air inlet, and a constant height along its length;
a second multiplicity of fins which partly define a second row of passages arranged side by side and aligned in a second direction that is not parallel with said first direction, each passage of said second row having an air inlet connected to receive air from said source of relatively colder air, an air outlet in fluid communication with said air inlet, and a constant height along its length; and
a first planar plate disposed between said first and second rows of passages,
wherein said first and second rows of passages and said first planar plate form a stack in which respective portions of each passage of said first row are disposed above respective portions of respective passages of said second row in a cross-flow relationship that allows heat to be transferred from any one passage of said first row to all of the passages of said second row; and
wherein said first multiplicity of fins have a first fin density in a first region occupied by some passages of said first row of passages and a second fin density in a second region occupied by other passages of said first row of passages, said first fin density being less than said second fin density, said first region being between said second region and a first side of the heat exchanger where said air inlets of said second row of passages are located.

9. The system as recited in claim 8 , further comprising:
a third multiplicity of fins which partly define a third row of passages arranged side by side and aligned in said first direction, each passage of said third row having an air inlet connected to receive air from said source of relatively hotter air, an air outlet in fluid communication with said air inlet, and a constant height along its length; and
a second planar plate disposed between said second and third rows of passages,
wherein said first, second and third rows of passages and said first and second planar plates form a stack in which respective portions of each passage of said third row are disposed below respective portions of respective passages of said second row in a cross-flow relationship that allows heat to be transferred from any one passage of said third row to all of the passages of said second row; and
wherein said third multiplicity of fins have said first fin density in a first region occupied by some passages of said third row of passages and said second fin density in a second region occupied by other passages of said third row of passages, said first region being between said second region and said first side of the heat exchanger.

10. The system as recited in claim 8 , wherein said second multiplicity of fins have a third fin density in a first region occupied by some passages of said second row of passages and a fourth fin density in a second region occupied by other passages of said second row of passages, said third fin density being less than said fourth

Assignees

• Boeing Co

Inventors

• Landre Eric G

Classifications

• F28D9/0062

  the conduits for one heat-exchange medium being formed by spaced plates with inserted elements (F28D9/0012, F28D9/0025, F28D9/0081, F28D9/04 take precedence) · CPC title

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title

• F28F3/025 Primary

  the means being corrugated, plate-like elements · CPC title

• F28F2215/04

  Assemblies of fins having different features, e.g. with different fin densities · CPC title