Dual-density header fin for unit-cell plate-fin heat exchanger

Abstract
A heat exchange cell for a recuperator includes top and bottom plates sandwiching a matrix finned member and a pair of header finned members. The top and bottom plates each include a pair of manifold openings, and the header finned members each include a curved free edge following the curvature of an associated manifold opening. The header finned member includes a high fin density portion along the free edge and a low fin density portion communicating with the high fin density portion. The dual fin density header finned member thus provides increased structural strength along the free edge and provides a low pressure drop through the low fin density portion.
Description




FIELD OF THE INVENTION




The invention relates to recuperators primarily for use in gas turbine engines, and more particularly to a fin construction for the header portions of such recuperators.




BACKGROUND




Plate-fin heat exchangers or recuperators have been used to pre-heat combustion-inlet air in a microturbine. A typical configuration for a heat exchanger includes a stacked array of cells of plate-fins, each cell including top and bottom plates, an internal finned member or matrix fin disposed between the plates, two external finned members on the outside surfaces of the cell, an inlet header finned member, and an outlet header finned member. The header finned members and matrix finned members are typically brazed or otherwise metallurgically bonded to the top and bottom plates. The inlet and outlet header finned members are also commonly referred to as crossflow headers because they are positioned at the inlet and outlet ends of the cell and because the flow of fluid through them is at an angle with respect to the flow of fluid through the matrix finned member.




In some applications, the pressure in the headers can reach high levels, which forces the top and bottom plates away from each other and creates tension in the header finned members. The header finned members thus perform a structural function as they tie the top and bottom plates together and resist deformation of the header portion of the cell that may be caused by the pressure in the cell. Accordingly, the header finned members must be sufficiently strong to resist such tensile deformation.




While the header finned members must perform the above-described structural function, the header finned members must also be constructed to not unduly restrict flow of air. The density of the fins must be selected to minimize the pressure drop through the headers. A balance must be found between maximizing header fin density to provide structural strength to the header, and minimizing header fin density to lower the pressure drop across the header.




One known method for balancing the structural and performance requirements of a header is to make the header wide enough to provide sufficient fin density to meet structural requirements while allowing enough flow area to meet pressure loss or performance requirements. To minimize the cost of tooling, standard header sizes have been implemented to cover a range of applications. Problems arise with these standard head sizes when volumetric constraints, non-typical operating conditions, or unusual performance specifications are required for a particular application.




SUMMARY




The present invention seeks to balance structural and performance requirements in crossflow headers by presenting a graded approach to fin density. In this way, the present invention provides a higher density of fins in regions with the greatest structural demand while minimizing fin density where structural demands are lighter to minimize pressure loss.




More specifically, the present invention provides a recuperator or heat exchanger cell including top and bottom plates each including a manifold opening. The top and bottom plates are positioned relative to one another to align the respective manifold openings. The cell also includes a matrix finned member disposed between the top and bottom plates. The matrix finned member and the top and bottom plates together define matrix channels for the flow of fluid between the top and bottom plates in a first direction.




Also disposed between the top and bottom plates is at least one header finned member. The header finned member, together with the top and bottom plates, defines header channels for the flow of fluid between the top and bottom plates in a second direction at an angle to the first direction, and the header channels communicate between the matrix channels and the manifold openings. The header finned member includes a low fin density portion and a high fin density portion positioned between the low fin density portion and the manifold openings.




Other features and advantages of the invention will become apparent to those skilled in the art upon review of the following detailed description, claims, and drawings.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a perspective view of the core of a recuperator.





FIG. 2

is an exploded view of one cell of the core illustrated in FIG.


1


.





FIG. 3

is a partially exploded view of the cell illustrated in FIG.


2


.





FIG. 4

is a cross-section view of a header of one cell of the core illustrated in FIG.


1


.





FIG. 5

is a top plan view of the dual density header finned member.











Before one embodiment of the invention is explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of other embodiments and of being practiced or being carried out in various ways. Also, it is understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including” and “comprising” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. The use of “consisting of” and variations thereof herein is meant to encompass only the items listed thereafter. The use of letters to identify elements of a method or process is simply for identification and is not meant to indicate that the elements should be performed in a particular order.




DETAILED DESCRIPTION




For the sake of brevity, not all aspects of plate fin heat exchanger and microturbine combustor technology are discussed herein. For additional information and discussion of the technology, reference is made to U.S. patent application Ser. No. 09/668,358 filed Sep. 25, 2000, Ser. No. 09/409,641 filed Oct. 1, 1999, Ser. No. 09/239,647 filed Jan. 29, 1999 (now U.S. Pat. No. 5,983,992), and Ser. No. 08/792,261 filed Jan. 13, 1997, and U.S. Provisional Patent Application No. 60/010,998 filed Feb. 1, 1996. The entire contents of the just-listed patent applications are incorporated herein by reference.





FIG. 1

illustrates a core


10


for a recuperator used in a microturbine. The core


10


includes a plurality of stacked plate-fin cells


14


defining an inlet manifold


18


and an outlet manifold


22


. As seen in

FIGS. 2 and 3

, each cell


14


includes top and bottom plates


24


,


28


, an internal or matrix finned member


32


, inlet and outlet header finned members


36


, and external finned members


40


. The top and bottom plates


24


,


28


include manifold openings


42


that align to define the manifolds


18


,


22


.




The matrix finned member


32


and header finned members


36


are sandwiched between and metallurgically bonded (e.g., by brazing) to the inwardly-facing surfaces of the top and bottom plates


24


,


28


. The external finned members


40


are metallurgically bonded to the outwardly-facing surfaces of the top and bottom plates


24


,


28


. The cells


14


are assembled and are bonded to each other as described in the above-referenced patents and patent applications. The header finned members


36


and the plates


24


,


28


define header channels, and the matrix finned member


32


and the plates


24


,


28


define matrix channels for the flow of compressed air through the cell


14


between the manifolds


18


,


22


.




Thus, a flow path


44


(

FIGS. 1 and 3

) between the cells


14


is provided for the flow of hot products of combustion, and a flow path


48


,


52


,


56


(

FIG. 3

) is provided within the cell


14


for compressed air being supplied to the combustor. The header portions of the cell


14


are also commonly referred to as “crossflow headers” because the flow of fluid


48


,


56


through the header channels is at an angle with respect to the flow of fluid


52


through the matrix channels of the cell


14


. The core


10


acts as a counterflow heat exchanger as hot products of combustion flow in one direction


44


and compressed air flows in the opposite direction


52


through the matrix channels. This has the effect of preheating the compressed air and increasing the efficiency of the microturbine. Most of the heat transfer occurs in the counterflow portion of the core


10


.





FIG. 4

illustrates a few fins of one of the header finned members


36


, along with portions of the top and bottom plates


24


,


28


. The compressed air flowing through the header portions of the cells


14


creates high pressure in the header portions, and tends to force the top and bottom plates


24


,


28


away from each other, as indicated by reference numerals


60


,


64


. This pressure creates tension in the vertical portions of the header finned members


36


, and the vertical portions resist the pressure forces in the header portions and resist separation of the top and bottom plates


24


,


28


.




Turning to

FIG. 5

, a free edge portion


68


of the header finned members


36


is positioned along the manifold openings of the cell


10


and is curved to mirror the shape of the manifold openings. The more pronounced the curvature of the header finned member's free edge


68


, the greater the spacing between the header fins along the edge


68


. The free edge


68


includes a sharply pointed or acutely angled portion


72


where the effective header fin density is lowest.




Elsewhere in the header portion, the theoretical nominal pressure capacity for the fins (i.e., the pressure at which the header finned member will theoretically fail) is proportionate to the fin density multiplied by the thickness of the fin material. However, the theoretical pressure capacity along the curved free edge


68


of the header finned member


36


equals the nominal pressure capacity multiplied by the sine of the angle φ of a line tangent to the free edge


68


. The sharply pointed portion


72


is therefore the portion of the header most likely to fail under high pressure conditions because the angle φ is smallest at the sharply pointed portion


72


.




To account for the change in effective fin density along the free edges


68


of the header finned members


36


, a high fin density portion


76


is provided to withstand the highest pressure conditions expected to be encountered. The high density portions


76


extend the entire width of the header finned members


36


to equalize the flow of fluid across the header finned members


36


. To minimize the pressure drop across the header portions, low fin density portions


80


are provided in areas of the header fined members


36


that are subject to less stress due to pressure. Alternatively, the thickness of the material used to fabricate the header finned members


36


may be increased in the high fin density portion


76


, while maintaining the nominal fin density constant throughout the header fined member


36


.




In a preferred embodiment of the invention, the angle φ at the sharply pointed portion


72


is between about 20-35°. Thus, assuming the high and low density portions


76


,


80


are constructed of the same material having the same thickness, the low density portion


80


may theoretically have a fin density of about 34-58% that of the high density portion


76


. However, due to certain bending stresses present at the plate-fin interface, it is preferred to make the density of the low density portion


80


about 50-70% of the density of the high density portion


76


.




Alternatively, the fin density may be maintained substantially the same in the high and low density portions


76


,


80


, and the material thickness in the low density portion


80


can be reduced to 34-58%, or preferably 50-70%, of the material thickness of the high density portion


76


. As another alternative, the width of the header finned members


36


can be reduced and the material thickened in the high density portion


76


to create a potential reduction in the cost of manufacturing the header finned members


36


.




An example of one dual-density header construction includes the high and low density portions both being constructed of 0.005 inch thick high temperature material (e.g., stainless steel or Iconel 625 nickel alloy). The minimum value of φ is about 20°. The high density portion may have a fin density of 15 fins-per-inch and the low density portion may have a fin density of 5 fins-per-inch.



Claims
  • 1. A heat exchanger cell comprising:top and bottom plates each including a manifold opening at least partially surrounded by an arcuate edge, said top and bottom plates being positioned relative to one another to align their respective manifold openings in stacked relation with each other; a matrix finned member disposed between said top and bottom plates and at least partially defining matrix channels for the flow of fluid between said top and bottom plates in a first direction; and a header fined member disposed between said top and bottom plates and at least partially defining header channels for the flow of fluid between said top and bottom plates in a second direction at an angle to said first direction, said header channels communicating between said matrix channels and said manifold openings, said header finned member including a low fin density portion having a plurality of fins, and a high fin density portion having a plurality of fins along said arcuate edges of said top and bottom plates; wherein the fins of the low fin density portion are substantially parallel to the fins of the high fin density portion, and wherein the low fin density portion and the high fin density portion are in contact with and metallurgically bonded to the top and bottom plates, said low fin density portion and high fin density portion having equal height.
  • 2. The cell of claim 1, wherein said low fin density portion has a fin density of about 50-70% the fin density of said high fin density portion.
  • 3. The cell of claim 1, wherein said high fin density portion has a fin density that is at least twice the fin density of said low fin density portion.
  • 4. The cell of claim 1, wherein said high fin density portion includes an arcuate free edge and an acutely angled portion.
  • 5. The cell of claim 4, wherein said arcuate free edge follows the curvature of one of said manifold openings.
Parent Case Info

This application is a continuation-in-part of U.S. patent application Ser. No. 09/668,358 filed Sep. 25, 2000, abandoned which is a continuation-in-part of U.S. application Ser. No. 09/409,641 filed Oct. 1, 1999, U.S. Pat. No. 6,305,079, which is a continuation of U.S. application Ser. No. 09/239,647 filed Jan. 29, 1999 now U.S. Pat. No. 5,983,992, which is a continuation of U.S. application Ser. No. 08/792,261 filed Jan. 13, 1997, abandoned, which claims the benefit of U.S. Provisional Application No. 60/010,998 filed Feb. 1, 1996.

US Referenced Citations (10)
Number Name Date Kind
3166122 Hryniszak Jan 1965 A
3322189 Topouzian May 1967 A
3380517 Butt Apr 1968 A
3669186 Schauls Jun 1972 A
3860065 Schauls Jan 1975 A
4073340 Parker Feb 1978 A
4291754 Morse et al. Sep 1981 A
4352393 Vidal-Meza Oct 1982 A
5983992 Child et al. Nov 1999 A
6032730 Akita et al. Mar 2000 A
Provisional Applications (1)
Number Date Country
60/010998 Feb 1996 US
Continuations (2)
Number Date Country
Parent 09/239647 Jan 1999 US
Child 09/409641 US
Parent 08/792261 Jan 1997 US
Child 09/239647 US
Continuation in Parts (2)
Number Date Country
Parent 09/668358 Sep 2000 US
Child 09/790464 US
Parent 09/409641 Oct 1999 US
Child 09/668358 US