U.S. patent number 3,866,674 [Application Number 05/402,261] was granted by the patent office on 1975-02-18 for gas turbine regenerator.
This patent grant is currently assigned to General Electric Company. Invention is credited to Howard M. Adriance, Robert W. Barta, James G. Miller, Salvatore S. Tramuta.
United States Patent |
3,866,674 |
Tramuta , et al. |
February 18, 1975 |
**Please see images for:
( Certificate of Correction ) ** |
Gas turbine regenerator
Abstract
A gas turbine regenerator for passing high pressure compressor
discharge air in a heat exchange relation with hot turbine exhaust
gases. An air inlet plenum and an air outlet plenum are disposed in
a cross-flow relation with respect to the exhaust gas flow, within
the exhaust gas flow, whereas a plurality of heat exchange unit
pressure tubes fluidly interconnect said air plenums and are
disposed in a generally parallel flow relation with respect to said
exhaust gas, within the exhaust gas flow. Opposite ends of each
unit pressure tube are received into either the air inlet plenum or
the air outlet plenum whereby fluid communication between plenums
is established and separation at each unit pressure tube opposite
end is prevented. Thermal expansion of the heat exchange unit is
substantially uniform since both the heat exchange pressure unit
tubes and the air plenums are disposed within the hot gas flow.
Inventors: |
Tramuta; Salvatore S.
(Schenectady, NY), Miller; James G. (Schenectady, NY),
Adriance; Howard M. (Schenectady, NY), Barta; Robert W.
(Schenectady, NY) |
Assignee: |
General Electric Company
(Schenectady, NY)
|
Family
ID: |
23591190 |
Appl.
No.: |
05/402,261 |
Filed: |
October 1, 1973 |
Current U.S.
Class: |
165/166;
165/DIG.384; 165/145 |
Current CPC
Class: |
F28F
9/0243 (20130101); F28F 9/06 (20130101); F28F
3/027 (20130101); F28D 9/0031 (20130101); F28G
13/00 (20130101); F28F 2250/104 (20130101); Y10S
165/384 (20130101) |
Current International
Class: |
F28F
9/04 (20060101); F28D 9/00 (20060101); F28F
9/02 (20060101); F28F 9/06 (20060101); F28G
13/00 (20060101); F28f 003/12 () |
Field of
Search: |
;165/165N,166F,4,145,165TD |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Myhre; Charles J.
Assistant Examiner: Streule, Jr.; Theophil W.
Attorney, Agent or Firm: Berrier, Jr.; Erwin F.
Claims
1. A heat exchange section for passing a high pressure air flow in
a heat exchange relation with a high temperature gas flow
comprising:
a tubular inlet and outlet plenum disposed in said housing, said
tubular plenums having at least one open end for receiving and
discharging said high pressure air flow, a plurality of axially
spaced, circumferentially elongated slots formed in said inlet and
outlet plenums, said plenums disposed in spaced, generally parallel
relationship with the slots of one plenum generally facing and
axially aligned with the slots of the other plenum;
a plurality of discrete high pressure air passage means for
directing high pressure air flow from said inlet plenum to said
outlet plenum and for transferring heat thereto from said high
temperature gas flow passing through said housing, said means
extending between and interconnecting said inlet and outlet plenums
and arranged in generally spaced parallel relationship and in
generally parallel flow relationship to said gas flow with each
said means comprising a pair of closely spaced generally parallel
plates joined together at their peripheral edges so as to define an
air passageway therebetween and formed with an open slot at
opposite ends for flow into and out of said air passageway, each
said passage means having one open end inserted into a slot of one
plenum and joined thereto and the other open end inserted into the
corresponding axial slot of the other plenum and joined thereto so
as to form a gas passageway between each pair of high pressure
passage means, whereby said passage means are connected to each
other through and supported exclusively by said tubular plenums so
as to permit removal and replacement of an individual one of said
passage means and to reduce thermal stressing of said passage
means.
2. The heat exchange section recited in claim 1 wherein the air
inlet plenum is downstream from the air outlet plenum with respect
to said gas
3. The heat exchange section recited in claim 1 wherein strip-fin
means are disposed between each pair of parallel plates having
alternating surfaces in metal joined abutment to the interior
surfaces of said unit pressure tube.
Description
BACKGROUND OF THE INVENTION
This invention was made under contract with the United States
Government under Contract 0-35510 with the United States Maritime
Administration of the Department of Commerce. The U.S. Government
is licensed in accordance with the terms of the aforesaid contract
and has reserved the rights set forth in Sections 1 f and 1 g of
the Oct. 10, 1963 Presidential Statement of Government Patent
Policy.
The invention relates, in general, to heat exchangers; and, in
particular, this invention relates to gas turbine regenerators
(recuperators). A regenerator (recuperator) is used in a gas
turbine power plant to heat compressor discharge air prior to its
entry into the combustion chambers thereby reducing the amount of
fuel necessary to bring the combustion gases to the required
operating temperatures. Heat is transferred to the compressor
discharge air from hot turbine exhaust gases which pass through the
regenerator in heat transfer relation with the compressor discharge
air. The regenerator includes alternating air and gas channels to
effect the heat transfer.
Prior art gas turbine regenerators have included box-like
structures having plate-fin tube banks with the entire regenerator
banded together by tie straps interconnecting massive structural
end frames. Compressor discharge air, at relatively high pressure
(about 130 psia) tends to push apart the tube banks as well as
tending to warp or bow the end frame structure. In the prior art,
bowing of the end frame structure was prevented by using a
plurality of relatively thick structural ribs incorporated into the
massive end frame. The aforesaid construction is disadvantageous in
that a thermal mass mismatch is created between the end frames and
tube banks in that the tube banks expand more quickly than the end
frames creating undesirable stressing in the regenerator.
An attempt to solve this problem is set forth in U.S. Pat.
Application Ser. No. 383,705, for Tramuta et al. filed July 30,
1973, and assigned to the assignee of the present invention. The
application entitled "Pressurized Strongback Regenerator" minimizes
thermal mismatch by replacing the heavy structural ribs by a
pressurized air chamber at the ends of each tube bank.
It is therefore one object of the present invention to reduce the
overall weight of a gas turbine regenerator.
It is another object of the present invention to minimize thermal
mismatch between the tube bundle and its support structure.
It is another object of the present invention to obviate massive
structural end frames and tie-straps in regenerator
construction.
Other objects and advantages will become apparent from the
following description of one embodiment of the present invention,
and the novel features will be particularly pointed out hereinafter
in the claims.
BRIEF DESCRIPTION OF THE INVENTION
According to the present invention, a regenerator may include one
or several heat exchange modules, or sections each section
comprising an air inlet plenum and an air outlet plenum mounted in
a cross-flow relation with respect to said exhaust gas flow. A heat
exchange tube bank is positioned between the air inlet and outlet
plenums in a generally parallel flow relation to said exhaust gas
flow, the tube bank including a number of unit pressure tubes. Each
unit tube includes an air passageway defined by a pair of spaced
apart parallel plates attached together at their peripheral edges.
There is a slotted opening at each opposite end of each pressure
tube. Each air plenum is formed with circumferential slots, along
its axial length which receive therein respective opposite end unit
pressure tube slotted openings whereby the air inlet and air outlet
plenums are in fluid communication and opposite ends of each unit
pressure tube are held together by the slotted air plenums. Gas
passageways are defined between each pair of air passageways. The
air inlet and outlet plenums are in the hot gas flow and thus tend
to expand uniformly with the heat exchange tube bank.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a partially cut-away perspective view of a gas turbine
regenerator according to the present invention.
FIG. 2 is an exploded perspective view of a regenerator section
including a heat exchange tube bank and air inlet and outlet
plenums.
FIG. 3 is a partially cut-away perspective view of a unit tube
structure.
FIG. 4 is a partial end view of a unit tube structure.
DETAILED DESCRIPTION OF THE INVENTION
A regenerative cycle for a gas turbine is well known and is, in
particular, shown in FIG. 1 of U.S. Pat. application Ser. No.
383,705, filed July 30, 1973, for Tramuta, Miller and Knox and
assigned to the assignee of the present invention. Generally
described, the regenerative cycle consists in passing compressor
discharge air in a heat exchange relation with hot turbine exhaust
gases through a regenerator (recuperator) to raise the temperature
of the air prior to the combustion cycle. However, the present
invention is applicable to any heat exchange device and the present
preferred embodiment is illustrative of one particular use.
Referring to the drawings of the present invention, FIG. 1 shows a
regenerator 11 including an outer frame 13 of minimal construction
and end flanges 15 for attaching the regenerator into an exhaust
gas duct (not shown). The regenerator may be comprised of one or
more heat exchange sections 17 each comprising a heat exchange tube
bank 19 and an air inlet plenum 21 and an air outlet plenum 23.
Flow arrows indicate the exhaust gas flow direction and the
compressor discharge air flow direction. The air plenums are each
formed with end flanges 25 for connecting the air inlet plenum to
the compressor discharge and the air outlet plenum to the
combustion chamber inlet respectively (not shown).
Each heat exchange section includes a heat exchange tube bank 19
comprising a plurality of unit pressure tubes as shown in FIGS. 2,
3 and 4. Each unit tube includes a pair of parallel, spaced apart
plates 35a and 35b defining an air passageway 37 there between.
Each air passageway may further include a number of staggered
strip-fin means 39 interposed between the parallel plates providing
alternating brazing surfaces S. The peripheral edges of each pair
of parallel plates are joined to provide a closed seam 43 forming a
sealed perimeter about the unit tube air passageway.
The unit pressure tube may be formed with a substantially
rectangular section including gas strip-fin means 49 on each air
passageway outer surface. Moreover, the air passageways are
extended beyond each rectangular portion to form trapezoidal end
portions each terminating in an open semi-circular slot 45 which
permits air flow through the unit tube air passageway. The gas
strip-fin means may be attached to the outer surfaces of the
rectangular section by brazing. Obviously, this is only one of
several possible configurations since the rectangular section
including gas strip-fin means may be extended to obviate the
trapezoidal end sections.
The air inlet and outlet plenums are formed with semi-circular
slotted openings 55 which are disposed along the longitudinal axis
of each air plenum. The slotted openings in the air inlet plenum
are substantially aligned with and directed toward the slotted
openings in the air outlet plenum. Each unit pressure tube is
disposed between the air plenums so that the slot at one end is
received into an air inlet plenum slotted opening and the slot at
the opposite unit tube structure end is received into an air outlet
plenum slotted opening thereby fluidly communicating the air inlet
plenum with the air outlet plenum through the plurality of unit
pressure tubes. Moreover, separation of the joined parallel plates
is prevented at each end of the unit tube structure by the
restraint imposed by the slotted pipes comprising the air inlet
plenum and the air outlet plenum respectively.
The operation of the regenerator is as follows. Hot turbine exhaust
gas flows through the regenerator as indicated in FIG. 1. The air
inlet plenums and the air outlet plenums are disposed in a
generally cross-flow relation with respect to the hot exhaust path
as well as positioned in the hot exhaust flow path. The plenums are
interconnected by heat exchange tube banks disposed in a parallel
flow relation with respect to the exhaust gas flow and positioned
in the hot gas flow. Because the plenums and heat exchange tube
banks are both positioned in the exhaust gas flow heating of
component parts is more uniform. Moreover, the hotter air outlet
plenum is positioned at the hot exhaust gas inlet, where the gas
temperature is highest; whereas, the cooler air inlet plenum is
positioned downstream, where the gas temperature is cooler, further
contributing to more uniform heating and hence thermal
expansion.
The unique slotted plenum construction equalizes thermal mass by
obviating massive end structures. The unit pressure tube, high
pressure, air passageways are each held together by the slotted air
plenum pipes, internal and peripheral brazing thereby providing a
more uniform construction rather than relatively light heat
exchange tube banks and a massive end structure associated with the
prior art.
An additional advantage of the unit pressure tube construction is
realized in that individual tubes may be removed from the
regenerator for maintenance and replacement.
While there is shown what is considered to be, at present, the
preferred embodiment of the invention, it is, of course, understood
that various other modifications may be made therein; and, it is
intended to cover in the appended claims all such modifications as
fall within the true spirit and scope of the invention.
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