CA1053105A - Heater for large flows at low pressure losses - Google Patents

Heater for large flows at low pressure losses

Info

Publication number
CA1053105A
CA1053105A CA255,376A CA255376A CA1053105A CA 1053105 A CA1053105 A CA 1053105A CA 255376 A CA255376 A CA 255376A CA 1053105 A CA1053105 A CA 1053105A
Authority
CA
Canada
Prior art keywords
sleeve
shell
convection
heater
hot gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA255,376A
Other languages
French (fr)
Inventor
Peter Von Wiesenthal
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Heat Research Corp
Original Assignee
Heat Research Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Heat Research Corp filed Critical Heat Research Corp
Priority to CA255,376A priority Critical patent/CA1053105A/en
Application granted granted Critical
Publication of CA1053105A publication Critical patent/CA1053105A/en
Expired legal-status Critical Current

Links

Abstract

HEATER FOR LARGE FLOWS AT LOW PRESSURE LOSSES
Peter von Wiesenthal ABSTRACT
This disclosure teaches a heater which is especially well suited to handling large flows of a process stream at low pressure losses. A cylindrical sleeve, having a first end and a second end, is mounted by means of a bellows in a cylindrical shell having a first end and a second end each corresponding with that of the sleeve. The first end converge to form a convection input passage therebetween, the second ends diverge to form a radiant zone therebetween. Hot gas passes between the shell and the sleeve through the radiant zone and then the convection input zone, the process stream passes through the inner flow space. A baffle is mounted within the sleeve in its first end to channel the process stream into a convection output passage boardered inwardly by the baffle and outwardly by the sleeve.
Extended surface projects from the sleeve into the convection input zone and additional extended surface projects from the sleeve into the convection output passage.

Description

~l~S;~ 5 There are numerous situa-tions wherein i-t is necessary to hea~ large flows of a process stream and wherein low pressure losses are mandated. Cases in point are air pre-heaters, particularly those employed in incineration sys-tems. Such heating of large flows a-t low pressure losses has been difficult to achieve by prior art installations in terms of capital costs~ thermal efficiency and the like.
BRIEF STATEMENT OF INVENTION
The present disclosure solves problems of prior art in-stallations in a parti~ularly use~ul, novel, unobvious and facile way, A heater is fabricated having a cylindrical s ;~
sleeve, with a first end and a second end, mounted in a cylidrical shell. The shell has a first end and a second ::
end each corresponding with that of the sleeve. The first ends converge to form a convection input passage therebetween, -the second ends diverge to form a radiant zone therebetween.
Hot gas passes between the shell and the sleeve through the radiant zone and then the convection input zone, while -the process stream passes through an inner flow space disposed inward of the sleeve. A baffle is mounted within the sleeve ~
in its first end to channel the process stream into a convec `
:- , tion output passage boardéred inwardly by the baffle and out-wardly by the sleeve. Extended surface projects from the sleeve into the convection input zone and additionallextended surface projects from the sleeve into the convec-tion output passage.
Accordingly, one object of this invention is to heat large flows at low pressure drops.
Another object of this invention ig to improve thermal efficiency.
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Still ~nother object o~ this invention is to ~abricate a heater of the type here contemplated and employing inexpensive ~aterials.
Still another object of this invention is to fabricate a heater of the type here contemplated which accommodates either con-ventional burners or an external source as a means to provide the hot gas.
S~ill another object of the invention i5 to fabricate a heater of the type here contemplated which can operate either co-currently or countercurrently.
` Still another object of this invention is to fabricate a heater of the type here conkemplated wherein allowance can be made conveniently for differential thermal expansion of parts of the heater.
Still another object of this invention is to fabricate a heater of the type here contemplated whlch is particularly well adapted to incineration systems wherein the process stream is com-bustion air and the hot gas is derived from the material being in-cinerated. Fuel requirements needed to achieve incinerakion tem-peratures are reduced drastically thereby.
Still another object o~ this invention is to provide a heater o~ the type here contemplated wherein the hot gas space is operable at a superatmospheric pressure so that structural re~uire-ments of the sleeve can be reduced.
Still another object of this invention is to fabricate a heater of the type here contemplated which is simple to de,ign, build .. . ~ , . . .................. , :
, ,. , . . , . ~:- , , . , , . ~ . , ~ 1.1353~
and maintain.
Still another object of this inventi.on is to fabricate a hea~er of the ty~e here contemplated which is suited well otherwise to its intended Eunctions. ' .

DESCRIPTION OF DRAWINGS
The foregoing and other objects, features and advantages - will appear more fully from detailed descriptions of preferred embodi-ments of the in~ention which follow along with claims which also follow, all viewed in conjunction with accompanying drawings wherein:
Fig~ 1 is a vertical view in section of a heater according to this invention with longitudinal fins mounted on the sleeve to serve as the extended surface.
Fig. 2 is a vertical view in section of another embodiment of the heater according to the present invention with fins wound splrally on the sleeve to serve as theextended surface.
; Fig~ ~ l S a broken sectional view of a portion of the sleeve with studs serving as the extended surface.
Fig. 4 is an enlarged detail view partly in section showing fins of Fig. 2.

DESCRIPTION OF PREFERRE~ EMBODIMENTS
As seen in Fig. 1 a heater generally designated 11 includes a vertical cylindrical shell 12 supported by a suitable structural , ~ system. A sleeve 13 is mounted in the shell 12 to separate a cylindri~
.~ , cal innsr flow space 14 from an annular outer flow space 15. The sleeve 13 has a flrst end 16 and a second end 17 each of which -- , ( ' ; .

;3~S

corresponds with a flrst end 18 and a second end 19 respectively of the shell 12. The first ends 16, 18cvnverge to form a convection input passage 21 therebetween, while the second ends 17, 1.~ di.verge to form a radiant zone 22 therebetween. To effect the foregoing, ~i the sleeve 1~ includes a duct 23 which penetrates into the shell 12 and is connected in sealed engagement with a hood 24, which in turn : is connected in sealed engagement with a cylindrical portion 25, which in turn is connected in sealed engagement with a disk like .
partition section 26, which in turn is connected in sealed engage-) ment with another duct portion 27 which also penetrates the shell 12. The sleeve 1~ can be supported at its top, in which case di-: ferential thermal expansion between the sleeve 1~ and the shell 12 can be taken care of by providing a bellows 28 between the duct 27 ; and the bottom 29 of the shell 12. Altexnately the sleeve 13 can be i supported anywhere along its length with expansion being accommo~
dated phrtially in each direction, in which case another bellows ~L could be provided between a top 32 of the shell 12 and the duct 2~
~ccording to this invention the process stream 33 is passed ;. thxough the inner flow space 14. Flow of the process stream 33 is :
) shown here to be downward in countercurrent heat exchange relationship with upward ~low of the hot gas 34, but it is ~ometimes desirable to flow the process stream 3~ cocurrently with the hot gas 34 and this cocurrent flow also can be accomplished by means of the heater 11 of this invention as will be understood by those skilled in heater design.
~ The process stream is shown to enter via the duct 23, and the hood 2~ ::
and to be diverted by a baffle ~5 disposed in the first end 16 o~ the : . 5 ~.,; i , .. . . .

sleeve 13 to conduct the prccess stream 33 into an annular convection output passa~e ~6 which is boarAered inwardly by the baffle 35 and outwardly by the sleeve 13. From the convection output passage 36 the process stream ~ passes through the duct 27 to exit the sleeve 1 5 .
The hot gas 34 may be provided by burning a ~uel in thP
radiant zone 22 of the outer flow space 15 using one or more burners 37 (which penetrate the bottom 29 o the shell 1~) or some other source of the hot gas ~4 may be employed. Usually the hot gas 34 will give up some of its heat by means of radiant transfer in the radiant zone 22. The size of the radiant zone 22 is a function of the temperature and constitution of the hot gas 34 and/or the com-bustion space required. At very low radiant temperatures or low heat input rates, the xadiant zone 22 required could be practically nil, in which case the heater 11 would operate on substantially convec-., .
tion principles.
From the radiant zone 22 the hot gas 34 passes throughthe convection input passage 21 boardered inwardly by the first end 16 of the sleeve 13 and outwardly by the first end 18 o~ the shell 12. From ths convection input passage 21 the hot gas 34 is collected in a plenum 38 boardered by the hood 24 and the top 32 o the shell 12 whence the hot gas 34 exits via a line ~9.
The shell 12 is lined with an insulating refractory 41 to reduce heat losses to the surroundings. This re~ractory 41 can be ~pplied internally (as shown~ ore~ternally of the shell 12, depending upon circumstances. If the refractory ~1 is applied externally of .

, S3~)5 the shell 12, the shell 12 will run hotter~ thus reducing temperature differentical between the shell 12 and the sleeve 13.
It is important to extrac-t heat Erom the hot gas 34 by means of convective heat transfer as well as by radiant heat transfer. Toward -this objective the disk like parti-tion 26 channels the hot gas 34 into the convection input passage 21 which is boardered between the sleeve 13 and the shell 12 and is in flow series with the plenum 38.
Extended surface used in this heater may be in the form of longitudinally organized fins 42 as shown in Fig. 1, hel~
ically organized fins ~3 ~ ~hown in Fig. 2, studs 44 as shown in Fig. 3 or any other commerically available system of like kind. As shown in Fig. 1 the longitudinal fins 42 ~ ;
extend from the sleeve 13 outwardly into the convection in- ;
put passage 21 ~o provide a large metal surface area in heat exchange relationship with the hot gas 34 so as to take heat therefrom. The longitudinally organized fins 42 al50 ex-tend inwardly from the sleeve 13 into the convection output passage 36 so ~s to conduct heat to the process stream 33 without need for passing the process stream 33i through tubes (at a consequent pressure loss penal~y). Heat transfer to the sleeve 13 via the disk like partition section 26 and the duct 27 at the second end 17 is substantially by means 0!~ radiant heat transf~r. The same priciples are involved inthe embodiments of Figs. 2 and 3 with the only differeces being that the extended surfaces used therein are the helically organized fins 42 and studs .~44 respectively.
If desired the outer flowspace 15 may be operated at ` ,' '~ .
' -7- ~

;- ::~ ., .. , , : :: .

~s;~
superatmospheric pressure to reduce pressure differential between the inner 1~ and the outer lS flow spaces, thereby reducing wall ~hi-kness requiremen.ts of the sleeve 1~.
It will be understood by those familiar with heater design that various deviations may be made from the described preferred em-bodiments, without departing from a main theme of invention set forth in a claim which follows.

:;, '' , . .

Claims

The embodiments of the invention in which an exclu-sive property or privilege is claimed are defined as follows:
1. A heater for a large flow of air to be heated at a low pressure loss, the heater characterized by the following:
a cylindrical shell having a first end and a second end, a cylindrical sleeve mounted coaxially in the shell and having a first end and a second end each corresponding with that of the shell, the sleeve connected expandably by means of bellows to the shell at one end of the shell and connected fixedly to the shell at the other end of the shell, the bellows positioned about the sleeve outwardly of the sleeve, the first ends of the shell and the sleeve converging to form a convection input passage therebetween, convection-input extended surface projecting from the sleeve into the convection input passage, the second ends of the shell and the sleeve diverging to form a radiant zone therebetween, hot gas means for passing a hot gas in turn through the radiant zone and the convection input passage, the hot gas means including at least one burner connected to supplies of fuel and oxygen as well as penetrating the shell to introduce the hot gas into the radiant zone, a cylindrical baffle mounted within the sleeve in its first end and defining a convection output passage boardered inwardly by the baffle and outwardly by the sleeve, air input means for introducing the air to be heated into the sleeve with the baffle organized to channel the air to be heated to the convection output passage, air output means for withdrawing the air to be heated from the convection output passage out of the heater, convection output extended surface projecting from the sleeve into the convection output passage.
CA255,376A 1976-06-22 1976-06-22 Heater for large flows at low pressure losses Expired CA1053105A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA255,376A CA1053105A (en) 1976-06-22 1976-06-22 Heater for large flows at low pressure losses

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA255,376A CA1053105A (en) 1976-06-22 1976-06-22 Heater for large flows at low pressure losses

Publications (1)

Publication Number Publication Date
CA1053105A true CA1053105A (en) 1979-04-24

Family

ID=4106255

Family Applications (1)

Application Number Title Priority Date Filing Date
CA255,376A Expired CA1053105A (en) 1976-06-22 1976-06-22 Heater for large flows at low pressure losses

Country Status (1)

Country Link
CA (1) CA1053105A (en)

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