U.S. patent number 3,782,457 [Application Number 05/191,998] was granted by the patent office on 1974-01-01 for recuperator and method of making.
This patent grant is currently assigned to Rohr Corporation. Invention is credited to Walter C. Troy.
United States Patent |
3,782,457 |
Troy |
January 1, 1974 |
RECUPERATOR AND METHOD OF MAKING
Abstract
Recuperator having unusually high heat transfer capability is
made up of casing with headers, and matrix having tubes extending
between headers and fins integral with tubes. In preferred form a
continuous web of metal foil, such as stainless steel, is
repeatedly folded on itself to form multiple spaced corrugations
extending from one side of web. Each corrugation is pinched
together at its open edge and seam welded to produce tube integral
with web. Web is then wrapped on itself in spiral arrangement to
produce matrix of multiplicity of very small parallel tubes. The
tubes of each wrap are in contact with the web of the adjacent wrap
but not secured thereto. All portions brace each other, and
integral fins provide maximum heat transfer. Tubes are rigidly
connected only to headers, and mid portion of matrix is free to
work in response to temperature gradients, greatly reducing
localized stresses.
Inventors: |
Troy; Walter C. (National City,
CA) |
Assignee: |
Rohr Corporation (Chula Vista,
CA)
|
Family
ID: |
22707809 |
Appl.
No.: |
05/191,998 |
Filed: |
October 26, 1971 |
Current U.S.
Class: |
165/165;
29/890.034; 165/158; 165/183; 165/DIG.399; 60/39.511; 165/160 |
Current CPC
Class: |
F02C
7/08 (20130101); F28D 9/04 (20130101); Y02T
50/671 (20130101); Y10T 29/49357 (20150115); Y10S
165/399 (20130101); Y02T 50/60 (20130101) |
Current International
Class: |
F28D
9/00 (20060101); F28D 9/04 (20060101); F02C
7/08 (20060101); F28d 009/00 () |
Field of
Search: |
;165/183,175,160,165,166,158,122,171,148 ;60/39.51R
;29/157.3R,157.3D,157.3C ;113/118R,118D,118C ;432/179 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
716,435 |
|
Oct 1954 |
|
GB |
|
371,608 |
|
Apr 1932 |
|
GB |
|
Primary Examiner: Davis, Jr.; Albert W.
Attorney, Agent or Firm: Pearson; George E.
Claims
Having thus described the invention, what is claimed as new and
useful and is desired to be protected by U.S. Letters Patent
is:
1. A recuperator comprising: a casing having side walls and a
header at each end, and a heat exchanger matrix located within the
casing; the matrix comprising a plurality of layers of heat
exchanging core material arranged in overlying relation with each
other; the core material consisting of metal foil web means
provided with a multiplicity of elongate tubes integrally formed
from the web means and arranged at one side of the web means in
closely spaced parallel relation with each other and parallel with
the web means; the tubes of one layer being in contact with the web
means of the adjacent layer while remaining free and unsecured
thereto whereby the tubes and web means are free to move relative
to each other when subjected to thermal stresses produced in the
respective members; the ends of the tubes extending through and
being secured to their associated headers; the tubes providing a
flow path through the headers and the length of the casing for the
flow of a first heat exchanging fluid; fluid inlet and outlet means
formed in the casing; and the spaces between the tubes, the web
means, and the casing walls providing a flow path through the
interior of the casing between the inlet and outlet means for the
flow of a second heat exchanging fluid.
2. A recuperator as claimed in claim 1; the layers of core material
being arranged generally circumferentially about the longitudinal
axis of the casing with the tubes being directed parallel to the
longitudinal axis and spaced peripherally and radially from each
other.
3. A recuperator as claimed in claim 2; the core material
comprising continuous web means wrapped upon itself in a spiral
arrangement.
4. A recuperator as claimed in claim 1; the core material being
divided into a plurality of web sections to define discrete layers.
Description
BACKGROUND OF THE INVENTION
This invention lies in the field of recuperators, or heat
exchangers, of the general type used in connection with gas
turbines to recover waste heat from the exhaust gas and transfer it
to the incoming air, although it is not limited to this type of
equipment. It is directed particularly to a recuperator which is
light and durable while achieving very high heat transfer
efficiency in terms of unit volume or unit weight.
The exhaust gas from the turbines of aircraft jet engines must
necessarily be expelled directly to atmosphere since it is the
source of thrust. However, many gas turbines in small size ranges
deliver their power through mechanical shaft means to operate land
vehicles, electric power generators, and other devices, and it is
common to recover energy from their exhaust gases by passing them
through heat exchangers, commonly referred to as recuperators, in
which incoming air for the turbines is passed in heat exchange
relation with the exhaust gases.
The recuperators commonly used for this purpose comprise casings
through which a plurality of tubes pass to serve as flow paths for
the exhaust gas. Incoming air is passed through such casing and
around the tubes to extract heat from the exhaust gas. Heat
transfer is increased by one or more schemes such as providing
multiple fins brazed on the tubes, or fin-like framework within the
casing holding the tubes in place and increasing the heat transfer
area, or providing tortuous air flow paths back and forth over the
tubes. All of these schemes are helpful but the efficiency is still
low in terms of weight and volume. The tubes are usually relatively
large so that a great deal of gas is transmitted without giving up
much heat, and the tubes are widely spaced with respect to their
diameters so that the volume of the casing is not efficiently used.
Also, if the tubes are supported by framework, the heat flow paths
to the remote parts of the framework are long and relatively
ineffective. If the tubes, fins, and framework are brazed together,
corrosion problems arise and high temperature stresses result from
uneven heat transfer.
Attempts have been made from time to time to produce a more unitary
heat exchanger by uniting two sheets of metal with weld lines which
define tube outlines between them, and then applying internal
pressure between the weld lines to expand the areas into tube-like
formations. This is a very difficult and expensive operation and
does not produce very uniform results. In addition, the structure
must then be curved or wrapped into some sort of annular
configuration, and this is very difficult and unsatifactory because
of the great stiffness of the welded structure. Moreover, the
double walls use up space, add weight, and reduce the rate of heat
transfer.
SUMMARY OF THE INVENTION
The present invention overcomes the difficulties mentioned above
and provides a recuperator which is very compact and light and
operates at an efficiency far higher than previous such devices.
Moreover it is easy to manufacture and very durable in service.
Generally stated, and in presently preferred forms, the heart of
the device is the core material for the recuperator matrix. This
core material comprises an elongate web of metal foil, such as
stainless steel, only a few thousandths of an inch thick which is
repeatedly folded back and forth on itself to form a multiplicity
of corrugations protruding from only one side of the general plane
of the web. The corrugations are parallel to each other and to the
web and are rather closely spaced, and they extend from edge to
edge of the web laterally of its principal axis. The open edges of
the corrugations are then pinched together and welded along lines
parallel to the web to make them into a multiplicity of tubes, all
of which are integral with the web. The entire web is readily
bendable about its lateral axes because of the flexibility of the
thin foil material.
The web is then wrapped tightly on itself in a spiral arrangement
about a small core or a large hollow core depending on its intended
use until a cylindrical matrix is produced in which the wraps or
layers are radially overlaid and the tubes of one layer are in
contact with the web of an adjacent layer although not bonded
thereto. Headers are then applied to each end of the matrix by any
suitable means, such as electrical discharge machining, powder
metallurgy, or ceramic molding. Casing walls are connected to the
header to complete the unit.
Air inlets and outlets are formed in the casing walls near the ends
and radial flow paths are formed by providing apertures in some or
all of the web portions between the tubes and adjacent to the ends
of the matrix. A longitudinal air flow path through the matrix is
defined by the longitudinal spaces between the tubes and the
web.
While the spiral wrap configuration is the most preferred form at
present, it is perfectly feasible to divide the elongate web into
short lengths determined by the shape of the casing to be used, and
to stack the web sections or layers in tube to web relation and
achieve the same goal of compact and light weight construction.
BRIEF DESCRIPTION OF THE DRAWINGS
Various other advantages and features of novelty will become
apparent as the description proceeds in conjunction with the
accompanying drawings, in which:
FIG. 1 is a schematic perspective view of an elongate web of foil
material, part of which has been corrugated;
FIG. 2 is a view similar to FIG. 1 after a second forming step;
FIG. 3 is a view similar to FIG. 1 after a third forming step;
FIG. 4 is a view similar to FIG. 1 after a fourth forming step;
FIG. 5 is a view similar to FIG. 4 showing a modification;
FIG. 6 is a schematic end view of a matrix spirally wrapped on a
minimum core;
FIG. 7 is a view similar to FIG. 6 but with a large hollow core to
receive a component;
FIG. 8 is a schematic perspective view of a recuperator with the
matrix of FIG. 7 with portions of the sidewalls removed;
FIG. 9 is a schematic plan view of a portion of the web used to
make up the matrix of FIGS. 7 and 8;
FIG. 10 is a schematic sectional view of the matrix and headers of
FIG. 8;
FIG. 11 is a view similar to FIG. 10 with the matrix wrapped on a
minimum core; and
FIG. 12 is a schematic cross sectional view of a modified form of
recuperator.
DESCRIPTION OF PREFERRED EMBODIMENTS
The manner of producing core material for use in making up the
matrix is illustrated schematically in FIGS. 1 to 5. The relative
sizes of components in these and the other figures are modified for
ease of illustration and description. It will be seen in FIG. 1
that the starting material for the matrix is a very long continuous
flat length or web 10 of metal foil, such as stainless steel, which
is only a few thousandths of an inch thick. The first step is to
process the web in any suitable machine to form a multiplicity of
reversely bent portions or corrugations 12 which are generally
U-shaped and project only from one face of the web. The
corrugations extend in spaced parallel relation laterally of the
principal axis of the web.
In the next phase, the open edges 14 of the corrugations are
pinched together and welded from end to end along lines parallel to
the plane of the web to produce individual sealed tubes 16 or tear
drop configuration as seen in FIG. 2. A series of slots or
apertures 18 are then pierced in some or all of the web portions 20
between the tubes and inward of the side edges 22 of the web, as
seen in FIG. 3. Typically, the slots may be about 1/4 to 3/8 inch
in length with lands of about 1/16 inch between them to maintain
the web strength. For maximum flow capacity a sizing tool is then
passed through each tube to give it the cylindrical formation shown
in FIG. 4. The core material is now completed and ready to be
wrapped around a mandrel or core in a spiral arrangement.
The full width of the web, as in FIG. 4, is retained for applying
headers to the spirally wrapped matrix by means of electrical
discharge machining in the well known manner. However, when other
systems are used for forming the headers in situ, as by powder
metallurgy or ceramic molding, the side edges 22 together with the
neck members 24 which connect the tubes to the web are cut back as
shown in FIG. 5 to form new side edges 26, with the tube ends
protruding a predetermined distance.
In order to make up a matrix, the web may be readily bent about
lateral axes because of the flexibility of the very thin foil and
wrapped in spiral arrangement about a mandrel 28 provided with a
cam-like formation 30 to initiate the spiral form as indicated
schematically in FIG. 6. The wrapping is continued with the tubes
of one wrap or layer in contact with the web of the adjacent wrap
or layer until a matrix 32 of the desired capacity is attained.
Headers are then applied in any suitable manner so that the tube
ends pass through the headers and are permanently secured thereto,
and then the casing is applied to complete the closure. Since all
of the layers are in contact, they are mutually self supporting. At
the same time, only the tube ends are held rigidly and the
remainder of the matrix may work in response to high temperature
gradients because the layers are not rigidly secured to each other,
and the stresses of uneven heating are substantially
eliminated.
When it is desired to form the matrix as a muff to surround some
other component such as the combustor of a jet engine, the same
process is used starting with a hollow mandrel 34 large enough to
encompass the desired component and provided with a spiral
initiating formation 36. Again the wrapping is continued until a
matrix 38 of the desired size is attained, and headers and casing
are applied in any suitable way.
A complete recuperator incorporating the muff-type matrix of FIG. 7
is schematically illustrated in FIG. 8, where it will be seen that
headers 40 and 42 are permanently secured to the tube ends and a
casing wall 4 surrounds the matrix between the headers. The end
portions of the casing wall have been omitted for clarity of
illustration. Air enters the casing at the end adjacent to header
42 and flows radially inward through the slots or apertures 18 to
all portions of the cross section.
It then flows longitudinally through all of the passageways defined
between the tubes and the web, and at the end adjacent to header 40
it flows radially inward through slots or apertures 18 to the
interior of the core where it may be used as the combustion air for
the turbine. The exhaust gas from the turbine flows through tubes
16 from header 40 to header 42. Thus this arrangement produces a
combination of lateral flow and counter flow to achieve maximum
heat transfer. The effectiveness is, of course, greatly enhanced by
the unusually large number of tubes and the large area of integral
fins made possible by the present construction. A typical example
is a recuperator configured approximately like FIG. 8 having an
inside diameter of about 10 inches and an outside diameter of about
20 inches and a length of about 13 inches, and containing upward of
22,000 tubes each having an outside diameter of about 0.078
inch.
It is desirable in most recuperator constructions in which air
enters and leaves the casing radially to provide the greatest area
of flow path adjacent to the inlet and outlet and to gradually
decrease the area to a minimum at the wall remote from the entrance
and exit in order to improve distribution through the various
portions of the matrix. In the present construction, this may be
accomplished in the manner indicated in FIG. 9, in which a web 10
with its integral tubes not shown is provided with apertures 18
extending laterally inward from adjacent the margins or side edges
22. At one end of the web, their extent is a predetermined minimum
and at the other end their extent is a predetermined maximum, which
the extent gradually increasing along the length of the web. The
web shown in this figure is suitable for making up the matrix for
the recuperator of FIG. 8. If it is wrapped from either end of the
web the resulting matrix will have maximum extent slots at the
radially inner side of one end and at the radially outer side of
the opposite end as in FIG. 8. The result is more graphically shown
in FIG. 10 which represents the matrix formed by spirally wrapping
the web of FIG. 9.
The same scheme may be used to produce the matrix 32 having a
minimum core. In such case, both the inlet and the outlet are at
the radially outer side of the matrix, and therefore the slot
arrangement must be modified so that the minimum slot extent at
both margins is at one end of the web and the maximum slot extent
is at the other end. The minimum slot end of the web must be
located at the core so that the smallest flow path areas will be at
the center of the matrix. When this is done, the resulting matrix
will be as indicated in FIG. 11.
While the spiral wrap arrangement is the most preferred for general
use, there are various special installations where some
modifications is desirable. In the example shown in FIG. 12, the
total web is cut into individual web sections 46 of predetermined
length and the sections are then stacked in multiple layers to
produce a matrix which just fills casing 48. Headers are attached
in the same way as with the previous forms and the web portions are
appropriately slotted to accord with the inlet and outlet
locations. This type of construction may be used with cylindrical
casings but its greatest utility lies in its accommodation to
casings of any size and shape, whether regular or irregular, in
which a spiral type cannot properly be fitted.
It will be apparent that the constructions disclosed above provide
a recuperator which is superior in terms of efficiency, weight,
volume, and durability because it is extremely compact and heat
transfer is multiplied manyfold since it is practical to use an
unusually large number of tubes in a given space with adequate
finning and mutual reinforcement.
While the invention has been described in detail in its present
preferred embodiment, it will be obvious to those skilled in the
art, after understanding this invention, that various changes and
modifications may be made therein, specifically in the fabrication
of the core material, without departing from the spirit or scope
thereof.
* * * * *