US2746404A - Sectional flame suppressor tube - Google Patents

Sectional flame suppressor tube Download PDF

Info

Publication number
US2746404A
US2746404A US242638A US24263851A US2746404A US 2746404 A US2746404 A US 2746404A US 242638 A US242638 A US 242638A US 24263851 A US24263851 A US 24263851A US 2746404 A US2746404 A US 2746404A
Authority
US
United States
Prior art keywords
tube
duct
plates
flame
tubes
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 - Lifetime
Application number
US242638A
Inventor
Maurice H Rottersmann
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US242638A priority Critical patent/US2746404A/en
Application granted granted Critical
Publication of US2746404A publication Critical patent/US2746404A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00Subject-matter not provided for in other groups of this subclass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23MCASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/06Combustion apparatus using pulverized fuel
    • F23C2700/063Arrangements for igniting, flame-guiding, air supply in

Definitions

  • This invention relates to improvements in combustion andV space-heating systems, and more particularly to an improvedilame suppressortube;
  • Fig. l is a diagrammatic end. view-of Van assembly of ducts as same would be used in the heating system of an oven for bakery goods;y o o d l Fig. 2 is horizontal,. part-sectional View taken in a horizontal plane, as indicated" by line 2-2 of Fig. 1;
  • Fig. 3 is a fragmentary sectional view in a vertical plane through the lower portion of an oven, and particularly showing the sectional shape of certain of the cross tubes or ducts; o j
  • Fig. 4 is a side elevational View of assembled, perforate plates forming sections utilized ⁇ in forming a profusely.
  • Fig, 6 is a diagrammatic view, being an elevation in perspective showing the radiating ducts, flue ducts and flue gas recirculating arrangement in connection with a typical oven, the latter ybeing here shown only in Outline, and, d j d .d
  • Fig. 7 is a fragmentary'vertical sectional View of parts inthe llame-entering end region of the combustion chamber.
  • the. oven structure which, as such, isor may be of conventional character, includes a bottom or iloor portion 10, a top closure or roof 11, and a front wall element 12 which is provided with an access opening normally closed Vby door 13.
  • the rear wall 14 together with end walls 1,5 and 16 serve to complete the enclosure .of the chamber to be heated.
  • lt is of course a preferencethat the enclosing wall portions of the oven be thermallyvinsulatedfor obvious reasons of ⁇ economy. No novelty is herein claimedfor the oven per-se, hence onlyagen'eral description thereof 4is included for better Ashowing .Of .rela- ,tion of the heating elementsl thereto.
  • ducts or tubes 20-21 are preferably of sheet metal suitably formed and jointed so as to present a secr. tion of rectangular aspect as shown by Fig. 5. In actual installations, the tube 21 may be and is usually of somewhat smaller sectional area than the tube 20.
  • the longitudinal ducts 20 and 21 are cross-connected by a plurality of spaced tubes 22, the nature, arrangement i and sectional shape of which will best appear from Fig. ⁇ 3.
  • Each of the cross tubes 22 is open'at its ends into.
  • the opposite longitudinal tubes 20 and 21 each of the latter being provided with ports or openings (not. shown) and which correspond in shape and area to the section of the tubes 22.
  • the cross tubes 22 are preferably, but without restriction, of some polygonal section, and as an ultimate pref, ⁇ erence are of diamond shape, the adjacent tubesbeing mutually spaced, and all of the cross tubes located slight,- ly above the bottom 10 ot' the oven, so as to permit a free circulation of the heated air fully about eachof the cross tubes. It is a further preference for better control, direc.- tion and ⁇ balliing of convection air currents rising from the cross tubes as well as the longitudinal ducts l20 and 21, to arrange the cross tubes in groups, and to incline the tubes of each such group so that the major axes thereof are sloped toward the adjacent group of tubes. As will appear from" Fig. 3, two such groups are shown, with the major axis of each diamond tube inclined toward a vertical median plane across the oven chamber.
  • the primary combustion of fuel occurs within Vthe ⁇ duct or tube 20, whence the products of ⁇ combustion pass via the cross tubes 22 into duct 21.
  • a ue gas connection into a vertical duct which latter are indicated respectively at 23 and 24, and which merge or converge into a chambered structure 25 connected through ⁇ a duct 26 to the inlet eye of a centrifugal blower 27.
  • blower 27 which latter positively displaces the flue gasesplis branched, one branch'30 of which is directed to the stack for discharge, and anotherbranch 31 ⁇ of which is utilized forrecirculation of aportion of the hot gases into the burner end of duct 20, for recirculation and further heat recovery.
  • Suitablel dainpers may be provided for varying the proportion of flue gases delivered respectively to the branches 30 and 31. ⁇ f
  • the tube 20 is somewhat longer than the perforate combustion chamber therein (later described) so as to provide an antechamber 2S into which the llame nozzle FN of the burner GTB extends, and also into which the recirculating duct 31 is connected.
  • a flame tube generally indicated at 4t
  • the latter there is located coaxially Awith and within the tube or duct 20, a flame tube generally indicated at 4t) which is spaced inwardly of the walls of duct 20, the latter, now obviously, serving asA an enclosure ,for the flame tube, ⁇ d Q i
  • any type of readilydspersible fuel may be utilized such as oil, gas, powdered coal or the lilithy the burner unit being shown and lpreferred as of gun type and f indicated as GTB.
  • the latter is provided with tliehllame wheel BW or like positive propulsion agency for propelling the air, and usually therewith the combustible sub-f stance throughthe nozzle FN.
  • the element 40 serve as a flame suppressor, in the-sense that, although it must necessarily be provided with plenary outlet area for the products of combustion and any small proportion of the combustible which continues in process of burning, nevertheless the member 40 is so designed and constructed that the flame will be substantially confined to the space therein, as a z'on'e' of primary combustionbeyond the nozzle of the Vburner GTB, In operation the angle and rate of projection of the air-combustible mixture are such that actual burning occurs substantially over the full length of the member 40, the outer end, being that end opposite the burner, being closed as'by a suitable end plate designated at 41.
  • the llame tube is preferably of metal, and may conings 43 which are about evenly distributed over each plate. Solely by way of instruction but without limitation, these openings, in the case of a flame tube the maximum cross dimension of which is of the order of 8 to 10 inches, will usually be, if circular, of the order of /lg-g inch'in diameter, but possibly in larger units of a range up to 1A inch size, it being noted as a distinct preference that the aggregate area of the openings through the several sections of the flame tube, should at least equal i the aggregate area of the outlets from the enclosing tube 20, which in the present instance may be identified with the several ⁇ openings indicated by the numerals 44 establishing'communicatin between the duct 20 and the several cross tubes 22.
  • the flame tube or combustion chamber 40 may be built up entirely of the perforate plates such as 42, it is a preference that the lower portion of this member be imperforate, so that the hot gases will emanate only from the central and upper portions of this member.
  • the two lowerrnost sectional plates forming the faces indicated at 45 are imperforate as far as the openings 43 are concerned, but are otherwise similar to the sectional plates 42.
  • Assembly of the several plates to form the perimeterV of a'unit length or tubular section of the duct40 is effected by means of angulate bracket'members 46, each of a length proportioned to the plates about as shown by Fig. 4, the sections being provided with openings in their end regions to accommodate assembly bolts 47.
  • the angle bracket members 46 are each provided through each face, with a pair of spaced bolt openings as will appear from Fig.
  • the burner end of the flame suppressor tube 40 may be left entirely open, while the corresponding end of tube 20 may be provided with a partial closure plate 28A having a central aperture of a size more than sufficient to accommodate the burner nozzle and thus provide a port 28B for admission of secondary air.
  • the opposite end of tube 20 is closed, andas above briefly mentionedthe opposite end of tube 40- is closed with a hexagonal plugv insert indicated by numeral 41, which may be bolted into position through the use of bracket members such as 46, on the endmost section of the tube.
  • the plates 42 and 45 be of substantial gauge or thickness, and formed of a cast ferrous metal such ⁇ as cast iron or steel, wth preference to certain alloys known to be highly resistant to hightem- 4 n perature etects over long periods of time, without warping or other deformation. It is a preference, in order to insure against sagging' of the member 40 when of substantial length, and in order to maintain the coaxial position of the combustion chamber 40 within the enclosing duct 20, to provide the perforate tubular structure with a series of furcate feet 51, attachment to which may be made by the same bolts or like elements 47 as are utilized for assembly of the lower plates 45 in the region of the feet.
  • the gases normally within the duct or tube 20 consist primarily of hot products of combustion. Due to the displacement effect resulting from the projection of the air and flame by the burner, and due further to the aspirating effect of the fan 27, the hot burned gases will be moved rapidly outwardly through the side openings in duct 20, thence through the cross tubes 22 which are rapidly heated once the system is put into operation.
  • the cross tubes in turn discharge into the longitudinal duct 21 parallel to the duct or tube 20.
  • a flame suppressor tube comprised of tubular sections arranged in en-to-end relation, each tubular section including a plurality of substantially rectangular plates angularly arranged in edge-to-edge relation to form a tube of polygonal cross-section, a plurality of said plates being provided with numerous openings, a plurality of Vbracket members each having portions overlapping a p pair of adjacent corner portions of the plates of one section and the axially adjoining pair of adjacent corner portions of the next section, fastening elements connecting each corner portion to its overlapping bracket member portion to provide for end-t'o-end assembly of the plates of axially adjacent sections, and a plurality of axially spaced supports attached along one side of the tube.
  • a flame suppressor tube comprised of tubular sections arranged n end-to'end relation, each tubular section including a plurality of substantially rectangular plates angularly arranged in edge-to-edge relation to form a tube of polygonal cross section, a plurality of bracket members each having portions overlapping a pair of ⁇ adjacent corner portions of the plates of one section ⁇ and the axially adjoining pair of adjacent corner portions of 6 the next section, fastening elements connecting each corner portion to its overlapping bracket member portion to provide for end-to-end assembly of the plates of axially adjacent sections, and a plurality of axially spaced supports attached along one side of the tube, a plurality of said plates being characterized by numerous openings, each support being furcated to overlap adjacent pairs of corner portions of a pair of plates in one section and ⁇ in its axially adjacent section, and connectors for fastening the supports to said plates.

Description

l. j o 2,746,404 s SECTIONAL FLAME SUPPRESSOR TUBE Maurice H. Rottersmann, Webster Groves, Mo. o `Application August 20, 1951, Serial No. 242,638.'
2 claims. (c1. 11o- 1) i This invention relates to improvements in combustion andV space-heating systems, and more particularly to an improvedilame suppressortube;
' A primary objective realizedin the presently improved combustion system, consists in a virtually evenly heated "detailed description of a presently preferred embodiment of theimprOVementS, particularly when considered in connection with the accompanying drawing, in which:
Fig. l is a diagrammatic end. view-of Van assembly of ducts as same would be used in the heating system of an oven for bakery goods;y o o d l Fig. 2 is horizontal,. part-sectional View taken in a horizontal plane, as indicated" by line 2-2 of Fig. 1;
Fig. 3 is a fragmentary sectional view in a vertical plane through the lower portion of an oven, and particularly showing the sectional shape of certain of the cross tubes or ducts; o j
Fig. 4 is a side elevational View of assembled, perforate plates forming sections utilized` in forming a profusely.
perforate flame-suppressor tube constituting a combustion chamber; d o t Fig. 5 is a transverse sectionall view through an inter.-
r'nediate portion ofthe ame suppressor tube and an en closing sheet metal duct;
"Fig, 6 is a diagrammatic view, being an elevation in perspective showing the radiating ducts, flue ducts and flue gas recirculating arrangement in connection with a typical oven, the latter ybeing here shown only in Outline, and, d j d .d
` Fig. 7 is a fragmentary'vertical sectional View of parts inthe llame-entering end region of the combustion chamber.
` Y* Referring new by characters of reference to the drawing,"the. oven structure which, as such, isor may be of conventional character, includes a bottom or iloor portion 10, a top closure or roof 11, and a front wall element 12 which is provided with an access opening normally closed Vby door 13. The rear wall 14 together with end walls 1,5 and 16 serve to complete the enclosure .of the chamber to be heated. lt is of course a preferencethat the enclosing wall portions of the oven be thermallyvinsulatedfor obvious reasons of` economy. No novelty is herein claimedfor the oven per-se, hence onlyagen'eral description thereof 4is included for better Ashowing .Of .rela- ,tion of the heating elementsl thereto.
z ,i In theheating of-a space ofrectangular plan, asin the 2,746,404 Patented May 22,. 1956 .longitudinal circulating tubes or ducts arranged along the inside lower portion of the front and back walls `12 and 1,4 respectively, of the oven, such tubesbeing indicated at l2l) along wall 14, and at 21 along the lower portion of wall 12. `The ducts or tubes 20-21 are preferably of sheet metal suitably formed and jointed so as to present a secr. tion of rectangular aspect as shown by Fig. 5. In actual installations, the tube 21 may be and is usually of somewhat smaller sectional area than the tube 20.
The longitudinal ducts 20 and 21 are cross-connected by a plurality of spaced tubes 22, the nature, arrangement i and sectional shape of which will best appear from Fig. `3. Each of the cross tubes 22 is open'at its ends into. the opposite longitudinal tubes 20 and 21 each of the latter being provided with ports or openings (not. shown) and which correspond in shape and area to the section of the tubes 22. o
The cross tubes 22 are preferably, but without restriction, of some polygonal section, and as an ultimate pref, `erence are of diamond shape, the adjacent tubesbeing mutually spaced, and all of the cross tubes located slight,- ly above the bottom 10 ot' the oven, so as to permit a free circulation of the heated air fully about eachof the cross tubes. It is a further preference for better control, direc.- tion and `balliing of convection air currents rising from the cross tubes as well as the longitudinal ducts l20 and 21, to arrange the cross tubes in groups, and to incline the tubes of each such group so that the major axes thereof are sloped toward the adjacent group of tubes. As will appear from" Fig. 3, two such groups are shown, with the major axis of each diamond tube inclined toward a vertical median plane across the oven chamber.
As'will later appear and be fully described, the primary combustion of fuel occurs within Vthe `duct or tube 20, whence the products of` combustion pass via the cross tubes 22 into duct 21. At one or each end of duct 21 there is provided a ue gas connection into a vertical duct, which latter are indicated respectively at 23 and 24, and which merge or converge into a chambered structure 25 connected through `a duct 26 to the inlet eye of a centrifugal blower 27. The outlet or discharge from blower 27, which latter positively displaces the flue gasesplis branched, one branch'30 of which is directed to the stack for discharge, and anotherbranch 31 `of which is utilized forrecirculation of aportion of the hot gases into the burner end of duct 20, for recirculation and further heat recovery. Suitablel dainpers (not shown) may be provided for varying the proportion of flue gases delivered respectively to the branches 30 and 31.` f
f As will appear from Fig. 7,`the tube 20 is somewhat longer than the perforate combustion chamber therein (later described) so as to provide an antechamber 2S into which the llame nozzle FN of the burner GTB extends, and also into which the recirculating duct 31 is connected. v
Referring now somewhat more in detail to the cont-r bustion system as such, there is located coaxially Awith and within the tube or duct 20, a flame tube generally indicated at 4t) which is spaced inwardly of the walls of duct 20, the latter, now obviously, serving asA an enclosure ,for the flame tube,` d Q i As asource of the combustibles together with air for burning same, any type of readilydspersible fuel may be utilized such as oil, gas, powdered coal or the lilithy the burner unit being shown and lpreferred as of gun type and f indicated as GTB. The latter is provided with tliehllame wheel BW or like positive propulsion agency for propelling the air, and usually therewith the combustible sub-f stance throughthe nozzle FN.
It is a preference that the element 40 serve as a flame suppressor, in the-sense that, although it must necessarily be provided with plenary outlet area for the products of combustion and any small proportion of the combustible which continues in process of burning, nevertheless the member 40 is so designed and constructed that the flame will be substantially confined to the space therein, as a z'on'e' of primary combustionbeyond the nozzle of the Vburner GTB, In operation the angle and rate of projection of the air-combustible mixture are such that actual burning occurs substantially over the full length of the member 40, the outer end, being that end opposite the burner, being closed as'by a suitable end plate designated at 41.
The llame tube is preferably of metal, and may conings 43 which are about evenly distributed over each plate. Solely by way of instruction but without limitation, these openings, in the case of a flame tube the maximum cross dimension of which is of the order of 8 to 10 inches, will usually be, if circular, of the order of /lg-g inch'in diameter, but possibly in larger units of a range up to 1A inch size, it being noted as a distinct preference that the aggregate area of the openings through the several sections of the flame tube, should at least equal i the aggregate area of the outlets from the enclosing tube 20, which in the present instance may be identified with the several `openings indicated by the numerals 44 establishing'communicatin between the duct 20 and the several cross tubes 22.
Although the flame tube or combustion chamber 40 may be built up entirely of the perforate plates such as 42, it is a preference that the lower portion of this member be imperforate, so that the hot gases will emanate only from the central and upper portions of this member. I
In such case, assuming a hexagonal tube 40, the two lowerrnost sectional plates forming the faces indicated at 45, are imperforate as far as the openings 43 are concerned, but are otherwise similar to the sectional plates 42. Assembly of the several plates to form the perimeterV of a'unit length or tubular section of the duct40, is effected by means of angulate bracket'members 46, each of a length proportioned to the plates about as shown by Fig. 4, the sections being provided with openings in their end regions to accommodate assembly bolts 47. In addition to providing for the perimetral assembly of the requisite number of the substantially planar plates 42 and 45, the angle bracket members 46 are each provided through each face, with a pair of spaced bolt openings as will appear from Fig. 4 and indicated at 50,l such that the bracket members also serve to permit endwise assembly of the tubular sections formed of the plates. The burner end of the flame suppressor tube 40 may be left entirely open, while the corresponding end of tube 20 may be provided with a partial closure plate 28A having a central aperture of a size more than sufficient to accommodate the burner nozzle and thus provide a port 28B for admission of secondary air. The opposite end of tube 20 is closed, andas above briefly mentionedthe opposite end of tube 40- is closed with a hexagonal plugv insert indicated by numeral 41, which may be bolted into position through the use of bracket members such as 46, on the endmost section of the tube.
It is preferred that the plates 42 and 45 be of substantial gauge or thickness, and formed of a cast ferrous metal such` as cast iron or steel, wth preference to certain alloys known to be highly resistant to hightem- 4 n perature etects over long periods of time, without warping or other deformation. It is a preference, in order to insure against sagging' of the member 40 when of substantial length, and in order to maintain the coaxial position of the combustion chamber 40 within the enclosing duct 20, to provide the perforate tubular structure with a series of furcate feet 51, attachment to which may be made by the same bolts or like elements 47 as are utilized for assembly of the lower plates 45 in the region of the feet.
It is Ythought that the function of the combustion chamber and immediate pertinent parts, and of the duct system therewith, will have become apparent from the foregoing detailed description of elements, but it may be noted for completeness that, as the burning fuel is projected into the flame suppressor tube 40, substantially complete combustion will take place therein, the speed of blower wheel BW in the burner being so regulated as to result in a flame length which is substantially equal to the length of the combustionchamber identified with the space in tube 40. Based on actual usage, best results are obtained with a regulation of fuel feed to the burner GTB so proportioned to the air discharged by the blower wheel BW, that the tubular member 40 will be kept at a temperature of 900-1000 degrees F., although such statement of range should not be taken as limiting. Under such conditions, very little flame will be apparent upon observation, exteriorly of the combustion chamber 40, although at times small nonprojected llames willgappear close to and in wiping contact with the outside surfaces of the perforate plates, it being highly desirable that there be avoided any protracted. flame contact with the sheet metal tube 20. Regulationofame characteristics may be effected in some degree by control of area of opening 28B, as by any simple form of damper orl shutter (not shown), to vary the secondary air aspirated through this area.
As the combustion ismore or less complete within the member 40, the gases normally within the duct or tube 20 consist primarily of hot products of combustion. Due to the displacement effect resulting from the projection of the air and flame by the burner, and due further to the aspirating effect of the fan 27, the hot burned gases will be moved rapidly outwardly through the side openings in duct 20, thence through the cross tubes 22 which are rapidly heated once the system is put into operation. The cross tubes in turn discharge into the longitudinal duct 21 parallel to the duct or tube 20. The gas being somewhat reduced in temperature by thermal exchange in the oven, the ue gases moving upwardly through ducts 23 and 24 vare somewhat cooled, and are mixed in the fan intake enclosure 25, thence proceed into and through the fan 27, part of the combustion gases at this point being impelled to the stack through connection 30, and the remainder passed downward through duct 31. This latter as earlier mentioned, is a recirculation duct for the flue gases and delivers a `certainproportion thereof back into the duct 2t) specifically as disclosed, into antechamber 28 so as to provide for further utilization of the heat remaining therein.
Brief reference was heretofore made to the advantage of inclination of the major axes, and the grouping of the diamond tubes 22. By so arranging the cross tubes they serve ina sense as baffles, and the air warmed thereby, is caused to converge in a central region of the oven or other space, thence proceeding upwardly until approaching or reaching the inner surface of the top of the oven, whence the now divided stream will proceed downwardly along the end walls of the oven for reheating and further circulation. Such a control of theV convection currents within the oven has been found to conduce to uniformity of temperature in the various baking zones of the enclosure.
For brevity and simplicity of illustration and description, the structure disclosedislpartly diagrammatic. It
outer sheet metal enclosure coactng with wall 16, can
be used to house the burner, the blower 27, together With elements 25 and 26, and such control dampers or valves as desired, all in position for easy access for any purpose of control or service attention.
Although the invention has been described by particularzed reference to a single preferred embodiment, the detail of description is to be understood solely in an illustrative, rather than in any limiting sense, numerous variants being possible within the scope of the claims hereunto appended.
I claim as my invention:
1. A flame suppressor tube comprised of tubular sections arranged in en-to-end relation, each tubular section including a plurality of substantially rectangular plates angularly arranged in edge-to-edge relation to form a tube of polygonal cross-section, a plurality of said plates being provided with numerous openings, a plurality of Vbracket members each having portions overlapping a p pair of adjacent corner portions of the plates of one section and the axially adjoining pair of adjacent corner portions of the next section, fastening elements connecting each corner portion to its overlapping bracket member portion to provide for end-t'o-end assembly of the plates of axially adjacent sections, and a plurality of axially spaced supports attached along one side of the tube.
2. A flame suppressor tube comprised of tubular sections arranged n end-to'end relation, each tubular section including a plurality of substantially rectangular plates angularly arranged in edge-to-edge relation to form a tube of polygonal cross section, a plurality of bracket members each having portions overlapping a pair of` adjacent corner portions of the plates of one section `and the axially adjoining pair of adjacent corner portions of 6 the next section, fastening elements connecting each corner portion to its overlapping bracket member portion to provide for end-to-end assembly of the plates of axially adjacent sections, and a plurality of axially spaced supports attached along one side of the tube, a plurality of said plates being characterized by numerous openings, each support being furcated to overlap adjacent pairs of corner portions of a pair of plates in one section and `in its axially adjacent section, and connectors for fastening the supports to said plates.
References Cited in the le of this patent UNITED STATES PATENTS 1,502,200 Howlett et al. July 22, 1924 1,574,839 Morse Mar. 2, 1926 1,694,393 Nash et al. Dec. 11, 1928 1,735,945 Wollaston Nov. 19, 1929 1,857,447 Engles May 10, 1932 1,914,567 Hopkins June 20, 1933 1,943,053v Boisset v--- Jan. 9, 1934 2,041,930 Houlis May 26, 1936 2,247,849 Ritter July 1, 1941 2,299,154 Lair Oct. 20, 1942 `2,410,881 Hunter Nov'. 12, 1946 2,411,324 Gagnon Nov. 19, 1946 2,430,101 Campbell et al. Nov. 4, 1947 2,474,169 Shelton June 21, 1949 2,478,732 Wilson et al. Aug. 9, 1949 2,501,041 Gates Mar. 21, 1950 2,527,937 Klug Oct. 31, 1950 2,540,359 Torpy et a1. Feb. 6, 1951 2,556,984 Smith June 12, 1951 FOREIGN `PATENTS 272,784 Switzerland Apr. 2, 1951
US242638A 1951-08-20 1951-08-20 Sectional flame suppressor tube Expired - Lifetime US2746404A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US242638A US2746404A (en) 1951-08-20 1951-08-20 Sectional flame suppressor tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US242638A US2746404A (en) 1951-08-20 1951-08-20 Sectional flame suppressor tube

Publications (1)

Publication Number Publication Date
US2746404A true US2746404A (en) 1956-05-22

Family

ID=22915597

Family Applications (1)

Application Number Title Priority Date Filing Date
US242638A Expired - Lifetime US2746404A (en) 1951-08-20 1951-08-20 Sectional flame suppressor tube

Country Status (1)

Country Link
US (1) US2746404A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3373732A (en) * 1966-10-10 1968-03-19 Tarnas Wincenty Gaseous-fuel jet-fired heater

Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1502200A (en) * 1922-01-14 1924-07-22 William T Howlett Gas stove
US1574839A (en) * 1923-03-03 1926-03-02 Albert W Morse Oil-burning unit
US1694393A (en) * 1924-01-04 1928-12-11 Alcorn Comb Co Radiating combustion chamber
US1735945A (en) * 1927-08-05 1929-11-19 Wollaston Thomas Roland Boiler and the like
US1857447A (en) * 1930-09-11 1932-05-10 Baker Perkins Co Inc Heating system for bake ovens
US1914567A (en) * 1928-05-26 1933-06-20 Hudson Motor Car Co Oil or gas burner
US1943053A (en) * 1931-02-28 1934-01-09 Charles L Bolsset Internal combustion apparatus
US2041930A (en) * 1936-05-26 Baking oven
US2247849A (en) * 1938-04-01 1941-07-01 Emil W Ritter Heater
US2299154A (en) * 1939-12-12 1942-10-20 Lair Paul Henry Refractory assembly for heating plants
US2410881A (en) * 1942-07-29 1946-11-12 Robert H Hunter Heating apparatus
US2411324A (en) * 1944-10-02 1946-11-19 Charles L Gagnon Burner device for furnaces
US2430101A (en) * 1947-11-04 Combustion chamber
US2474169A (en) * 1948-07-22 1949-06-21 Samuel Stamping And Enameling Metal radiant for gas heaters
US2478732A (en) * 1948-04-01 1949-08-09 Wilson Combustion tube heating apparatus
US2501041A (en) * 1947-01-16 1950-03-21 Harold J Gates Furnace construction for fluid fuel fired air-heating furnaces
US2527937A (en) * 1948-08-10 1950-10-31 Ferdinand H Klug Hot-air furnace
CH272784A (en) * 1950-05-15 1951-01-15 Oelfeuerungen Ag Flame chamber in oil-heated devices.
US2540359A (en) * 1949-05-13 1951-02-06 Thomas J Torpy Furnace
US2556984A (en) * 1946-02-14 1951-06-12 Du Pont Immersion heater

Patent Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430101A (en) * 1947-11-04 Combustion chamber
US2041930A (en) * 1936-05-26 Baking oven
US1502200A (en) * 1922-01-14 1924-07-22 William T Howlett Gas stove
US1574839A (en) * 1923-03-03 1926-03-02 Albert W Morse Oil-burning unit
US1694393A (en) * 1924-01-04 1928-12-11 Alcorn Comb Co Radiating combustion chamber
US1735945A (en) * 1927-08-05 1929-11-19 Wollaston Thomas Roland Boiler and the like
US1914567A (en) * 1928-05-26 1933-06-20 Hudson Motor Car Co Oil or gas burner
US1857447A (en) * 1930-09-11 1932-05-10 Baker Perkins Co Inc Heating system for bake ovens
US1943053A (en) * 1931-02-28 1934-01-09 Charles L Bolsset Internal combustion apparatus
US2247849A (en) * 1938-04-01 1941-07-01 Emil W Ritter Heater
US2299154A (en) * 1939-12-12 1942-10-20 Lair Paul Henry Refractory assembly for heating plants
US2410881A (en) * 1942-07-29 1946-11-12 Robert H Hunter Heating apparatus
US2411324A (en) * 1944-10-02 1946-11-19 Charles L Gagnon Burner device for furnaces
US2556984A (en) * 1946-02-14 1951-06-12 Du Pont Immersion heater
US2501041A (en) * 1947-01-16 1950-03-21 Harold J Gates Furnace construction for fluid fuel fired air-heating furnaces
US2478732A (en) * 1948-04-01 1949-08-09 Wilson Combustion tube heating apparatus
US2474169A (en) * 1948-07-22 1949-06-21 Samuel Stamping And Enameling Metal radiant for gas heaters
US2527937A (en) * 1948-08-10 1950-10-31 Ferdinand H Klug Hot-air furnace
US2540359A (en) * 1949-05-13 1951-02-06 Thomas J Torpy Furnace
CH272784A (en) * 1950-05-15 1951-01-15 Oelfeuerungen Ag Flame chamber in oil-heated devices.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3373732A (en) * 1966-10-10 1968-03-19 Tarnas Wincenty Gaseous-fuel jet-fired heater

Similar Documents

Publication Publication Date Title
US3719180A (en) Device for heat treatment by way of forced gas convection, forming a bakery, pastry, pork-butchery oven or the like
US2506120A (en) Gas wall heater
US3670713A (en) Gas-fired heater means
US2157643A (en) Oil-fired furnace
US1927174A (en) Gas furnace
US1334741A (en) Air-heating structure
US2746404A (en) Sectional flame suppressor tube
US1747522A (en) Heating apparatus employing powdered fuel
US2752912A (en) Forced air flow air heating furnace
GB1181651A (en) Improvements in or relating to Air Heaters
US3693598A (en) Boiler
US2023136A (en) Air heating and conditioning device
US2771132A (en) Radiant gas burner apparatus
US3111978A (en) Dual blower and burner for furnaces
US2258682A (en) Air conditioning system
US2514011A (en) Combined combustion chamber and heat exchanger
US1421247A (en) Air heater for furnaces
US1991513A (en) Stove construction
US2192636A (en) Heating unit
US1977783A (en) Heating furnace
US1339784A (en) Rug-drying device
US2132563A (en) Fireplace heater
US1420264A (en) Heating apparatus
US2310406A (en) Ceramic heating element and gas heater embodying the same
US1506121A (en) Apparatus for the exchange of heat