Composite plate pin or ribbon heat exchanger

• US 5,845,399 A
• Filed: 09/09/1996
• Issued: 12/08/1998
• Est. Priority Date: 06/05/1995
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Alliedsignal Inc.
• Inventors: Duncan, Christopher K., Anderson, Alexander F., Dewar, Douglas M.
• Primary Examiner(s): Flanigan, Allen J.
• Application Number:
  US08/712,003
• Time in Patent Office: 820 Days
• Field of Search: 165/166, 165/185, 165/905, 165/DIG. 356, 29/890.03
• US Class Current: 29/890.03
• CPC Class Codes: F28D 9/0062 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 Class Codes: F28F 21/00 Constructions of heat-exchange apparatus characterised by the selection of particular materials coatings for modifying heat-transfer F28F13/18; coatings for preventing the formation of deposits or corrosion F28F19/02
• CPC Class Codes: F28F 2255/06 composite, e.g. polymers with fillers or fibres
• CPC Class Codes: F28F 3/022 the means being wires or pins
• CPC Class Codes: Y10S 165/356 Plural plates forming a stack providing flow passages therein
• CPC Class Codes: Y10S 165/905 Materials of manufacture
• CPC Class Codes: Y10T 29/4935 Heat exchanger or boiler making

Abstract

A composite parallel plate heat exchanger is provided constructed of a plurality of composite plates disposed in a substantial parallel stacked relationship and spaced from each other by composite ribs inserted through and bonded between adjacent plates. The composite plates and ribs are specially constructed to maximize heat transfer between adjacent passageways formed by the plates and the fluids flowing in these passageways.

Claims

1. A method of fabricating a composite heat exchanger comprising the steps of:

providing a plurality of substantially planar high-strength fiber-matrix composite plates;

providing a plurality of high-strength fiber-matrix composite ribs;

inserting the ribs in a transverse direction through the composite plates;

wherein the composite ribs and/or the composite plates comprise thermally conductive fibers oriented so as to impart an anisotropic thermal conductivity to the composite ribs and/or the composite plates;

separating the plates along the ribs to position the plates in spaced relation and thereby define first and second flow passageways therebetween; and

bonding the plates and ribs to fixedly position the ribs relative to the plates whereby a free-standing composite heat exchanger structure is achieved.

2. The method of fabricating a composite heat exchanger of claim 1 wherein the composite material of the plates and ribs is selected from a class of materials comprising of a carbon fiber and polymeric resin matrix which provides improved performance and significantly reduced weight when compared to a conventional metal heat exchanger materials.

3. The method of fabricating a composite heat exchanger of claim 1 wherein the ribs exhibit a cross sectional configuration selected from the class consisting of circular, linear, square, rectangular, triangular and diamond.

4. The method of fabricating a composite heat exchanger of claim 1 wherein the selected composite material provides a low coefficient of expansion and significantly reduces stress in the heat exchanger.

5. The method of fabricating a composite heat exchanger of claim 1 wherein the individual thermal conductance'"'"'s and coefficients of the components are matched to either increase performance or reduce heat exchanger stress.

6. The method of fabricating a composite heat exchanger of claim 1 wherein the composite materials exhibit high corrosion resistance and extend heat exchanger service life.

7. The method of fabricating a composite heat exchanger of claim 1 wherein the flow directions of the first and second passageways are transverse to each other.

8. The method of fabricating a composite heat exchanger of claim 1 where the flow directions of the first and second passageways are parallel to each other.

9. The method of fabricating a composite heat exchanger of claim 1 where the first and second passageways have a different plate spacings.

10. The method of fabricating a composite heat exchanger of claim 1 wherein the ribs having a primary axis of thermal conductivity, as provided by an anisotropic material, which is substantially transverse to the plane of the plates.