Cold corner flow baffle

Patent metadata

Field	Value
Publication number	US-10124452-B2
Application number	US-201614996459-A
Country	US
Kind code	B2
Filing date	Jan 15, 2016
Priority date	Aug 9, 2013
Publication date	Nov 13, 2018
Grant date	Nov 13, 2018

Abstract

A heat exchanger for an aircraft includes a hot fluid inlet, a hot fluid outlet, a cold fluid inlet, a cold fluid outlet, and a header connected to the hot fluid outlet. The header includes a housing defining a header volume and a baffle separating the header volume into a first volume and a second volume, wherein the first volume and the second volume are in fluid communication with each other.

First claim

What is claimed is:

1. A heat exchanger for an aircraft comprising:
a hot fluid inlet;
a hot fluid outlet;
a cold fluid inlet;
a cold fluid outlet; and
a header connected to the hot fluid outlet, the header comprising:
a housing defining a header volume; and
a baffle located within the housing and separating the header volume into a first volume and a second volume, wherein the first volume and the second volume are in fluid communication with each other,
wherein the housing has a first end wall and a second end wall and a housing length defined between the first end wall and the second end wall, wherein the baffle extends from the first end toward the second end with a length of the baffle being less than the housing length,
the header further comprising a bypass outlet in fluid communication with the first volume,
a heat exchanger outlet, the heat exchanger outlet located in the housing opposite the bypass outlet, and
a bypass valve configured to control fluid flow through the bypass outlet, such that:
when the bypass valve is closed, no air can flow through the bypass outlet, and all air in the header volume will flow through the heat exchanger outlet, and
when the bypass valve is open, air from the first volume can flow into and through the bypass outlet, and air within the second volume will flow through the heat exchanger outlet,
wherein the bypass valve and baffle are arranged such that when the bypass valve is open a volume of air comprising 0% to 60% of a total air within the header volume will flow through the bypass outlet.

2. The heat exchanger of claim 1 , wherein the baffle extends from the hot fluid outlet to a top of the housing.

3. The heat exchanger of claim 1 , wherein the baffle is positioned parallel with the first side wall.

4. The heat exchanger of claim 1 , wherein the baffle extends at an angle relative to the first side wall.

5. The heat exchanger of claim 1 , wherein the baffle is integrally formed with the housing.

6. A method of making a heat exchanger for an aircraft, the method comprising:
connecting a header to a heat exchanger having a hot fluid inlet, a hot fluid outlet, a cold fluid inlet, and a cold fluid outlet, the header connected to the hot fluid outlet, the header comprising:
a housing defining a header volume; and
a baffle located within the housing and separating the header volume into a first volume and a second volume, wherein the first volume and the second volume are in fluid communication with each other
wherein the housing has a first end wall and a second end wall and a housing length defined between the first end wall and the second end wall, wherein the baffle extends from the first end toward the second end with a length of the baffle being less than the housing length,
the header further comprising a bypass outlet in fluid communication with the first volume,
a heat exchanger outlet, the heat exchanger outlet located in the housing opposite the bypass outlet, and
a bypass valve configured to control fluid flow through the bypass outlet, such that:
when the bypass valve is closed, no air can flow through the bypass outlet, and all air in the header volume will flow through the heat exchanger outlet, and
when the bypass valve is open, air from the first volume can flow into and through the bypass outlet, and air within the second volume will flow through the heat exchanger outlet,
wherein the bypass valve and baffle are arranged such that when the bypass valve is open a volume of air comprising 0% to 60% of a total air within the header volume will flow through the bypass outlet.

7. The method of claim 6 , wherein the baffle extends from the hot fluid outlet to a top of the housing.

8. The method of claim 6 , wherein the baffle is positioned parallel with the first side wall.

9. The method of claim 6 , wherein the baffle extends at an angle relative to the first side wall.

10. The method of claim 6 , wherein the baffle is integrally formed with the housing.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Army Donald E
• Bruno Louis J
• Kline Erin G
• Delugan Anthony

Classifications

• F28F9/0214 Primary

  having only longitudinal partitions · CPC title

• B64D13/00

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

• B23P15/26 Primary

  heat exchangers {or the like (making heat exchangers by methods covered by other subclasses B21D53/02)} · CPC title

• F28F2265/00

  Safety or protection arrangements; Arrangements for preventing malfunction · CPC title

• F28D9/0068

  with means for changing flow direction of one heat exchange medium, e.g. using deflecting zones · CPC title