US1782829A - Heat-transfer system - Google Patents
Heat-transfer system Download PDFInfo
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- US1782829A US1782829A US158549A US15854927A US1782829A US 1782829 A US1782829 A US 1782829A US 158549 A US158549 A US 158549A US 15854927 A US15854927 A US 15854927A US 1782829 A US1782829 A US 1782829A
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- combustion
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- tube
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- 238000002485 combustion reaction Methods 0.000 description 66
- 238000010521 absorption reaction Methods 0.000 description 16
- 230000005855 radiation Effects 0.000 description 13
- 238000010438 heat treatment Methods 0.000 description 12
- 239000012530 fluid Substances 0.000 description 10
- 239000007789 gas Substances 0.000 description 10
- 239000000463 material Substances 0.000 description 8
- 239000003208 petroleum Substances 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000003467 diminishing effect Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 229910001120 nichrome Inorganic materials 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
- C10G—CRACKING HYDROCARBON OILS; PRODUCTION OF LIQUID HYDROCARBON MIXTURES, e.g. BY DESTRUCTIVE HYDROGENATION, OLIGOMERISATION, POLYMERISATION; RECOVERY OF HYDROCARBON OILS FROM OIL-SHALE, OIL-SAND, OR GASES; REFINING MIXTURES MAINLY CONSISTING OF HYDROCARBONS; REFORMING OF NAPHTHA; MINERAL WAXES
- C10G9/00—Thermal non-catalytic cracking, in the absence of hydrogen, of hydrocarbon oils
- C10G9/14—Thermal non-catalytic cracking, in the absence of hydrogen, of hydrocarbon oils in pipes or coils with or without auxiliary means, e.g. digesters, soaking drums, expansion means
- C10G9/18—Apparatus
- C10G9/20—Tube furnaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F19/00—Preventing the formation of deposits or corrosion, e.g. by using filters or scrapers
- F28F19/002—Preventing the formation of deposits or corrosion, e.g. by using filters or scrapers by using inserts or attachments
Definitions
- 0111' invention relates to the art of controlling the application of heat to a heat ab sorption structure and has particular referenoe to a method of and apparatus for diminishing the quantity of convection heat applied thereto without to a substantial extent interfering with the radiant heat ap lication.
- suitable heat absorption structure traversed by fluid is disposed in the path of a hot medium, as hot gaseous decreasin from the ot medium to said structure there is utilized a member or baflle spaced, in part at least, therefrom and itself serving as a source of radiant heat.
- a vertical chamber whose lower wall structure is maintained at incandescence under the influence of hot gaseous products of combustion has disposed transversely thereofroups of tubes traversed by a' fluid, as petroeum or a compound or product thereof and,
- bafile structure itself heated to' radiance and constituting a secondary source of radiation and which shields from said gaseous products the tubes last mentioned.
- Fig. l is a perspective view of tubular heat absorption structure having a tubular bafie associated therewith.
- Fig. 2 is a transverse vertical sectional view of the structure shown in Fig. 1.
- Fig. 3 is a vertical sectional view showing another form'ofbafle.
- Fig. 4 is a vertical sectional view of a heating chamber'containing tubular heat absorpproducts of combustion, and for the heat applied by convection tion structures some having bafiles associated therewith.
- Fig. 5 is a side elevational view, partly in vertical section, showing a heat absorption structure with another form of bafile associated therewith.
- Fig. 6 is a transversevertical sectional view of the structure shown in Fig. 5.
- Fig.7 is a transverse vertical sectional view corresponding generally with Fig. 6
- Fig. 8 is an elevational View, partly invertical section, I showing another manner in which a bafile may be supported.
- a chamber 0 forme by the refractory walls W, W.
- a suitable heat absorption structure for
- a bank of tubes T of iron, steel or other suitable material for example, a bank of tubes T of iron, steel or other suitable material.
- chamber C Opening into the bottom of chamber C is a combustion chamber C, which, in the example illustrated, conforms with the one shown in our U. S. Patent No. 1,591,431. It shall be understood, however, that chamber C may be otherwise constructed as found suitable or desirable, for example, as disclosed in our co-pending application, Serial No. 151,307 filed Nov. 29, 1926.
- Heat radiating from the hot wall structure of the combustion chamber C may be utilized for any desired purpose, for example, it may be transferred substantially exclusively as radiant heat to suitable heat absorption structure, not shown, in the. manner illustrated and described in our aforesaid U. S. Patent No. 1,591,431.
- the tubes T are disposed between opposite wallsof the chamber 0 and may be connected in series or other suitable relation by couplings or headers, preferably connected to the tubes externally to the chamber C.
- any suitable fluid material either gaseous or liquid, as steam to be superheated, or water for the generation of steam.
- any suitable fluid material either gaseous or liquid, as steam to be superheated, or water for the generation of steam.
- petroleum, or a component or a product thereof under suitable pressure, as superatmospheric pressure is subjected to elevation of temperature while passing through the tubes T.
- the hot gaseous products of combustion emerging from the combustion chamber C pass, at relatively high velocity, between and around the tubes T and, when they are bare or unprotected, contact directly therewith, with resultant high rate of transfer of convection heat thereto.
- the gaseous products of combustion are at such elevated temperature that the walls W of chamber C, particularly the lower portions thereof, become incandescent and radiate heat-to the tubes T, particularly the lower groups thereof.
- some of the tubes T and the materialpassing therethrough are subjected to excessive temperature rise by the combined action of radiant and convection heat, and
- the tubes T are each encompassed by a cylinder or bafile B of greater cross sectional area than a tube T, and preferably circular and of a length corresponding with that of the tube between op osite walls of the chamber C.
- the ba e may assume a form such as is shown in Fi 3, that is, one that is circumferentially discontinuous.
- the cylinders or bafile members are supported by the respective tubes. It is obvious, however, that the baflle members may be supported by opposite walls W of chamber C and in such relation that they do not contact with the tubes T,
- a substantially V-shaped baffle B is shown as supported in opposite walls W of the chamber C in suitable close relation beneath a tube T and so disposed with respect thereto that the hot gases as they travel upwardly are diverted or deflected to either side of the tube.
- a baffle utilizable as is the one illustrated in Figs. 5 and 6 may assume any one of a variety of forms, for example, as shown in Fig. 7, where the battle B is semi-circular in shape.
- Fig. 5 suchbaffle or one of generally similar or'equivalent shape may be supported by a tube T in the manner illustrated in Fig, 8, wherein the members or straps S encircle both the tube and the bafiie to hold the latter in suitable position deflecting the hot gases to either side of the overlying tube.
- the bafile deflects or diverts substantially all the hot gaseous products of combustion from said tube within the longitudinal extent of the secondary source of radiant heat with resultant decrease in the amount of convection heat transferred thereto. It follows, then, that those tubes T with which the baflle structure is associated, together with the material passing therethrough, are not subjected to undue temperature rise, since the amount of convection heat applied thereto is substantially diminished.
- the bafiles are preferably. of such shape and so disposed within the chamber C as not to seriously impedethe upward passage of the hot gaseous products of combustion.
- the passages for gases between the various tubes T should not, to any substantial extent, be occupied by the baffles or parts thereof.
- Baflle structure of the character described herein may be formed by any suitable material, but preferably such as is chemically inert with respect to the gaseous products of combustion, of great resistance to oxidation at high temperature, and. of high heat conductivity.
- suitable material but preferably such as is chemically inert with respect to the gaseous products of combustion, of great resistance to oxidation at high temperature, and. of high heat conductivity.
- there may be utiliz'ed material as silicon carbide or the like, or and preferably a metal or alloy, as iron, steel, copper, nichrome and the chrome iron and nickel alloys.
- bafile structure of the character described herein attains such high temperature as to become incandescent or luminous.- However, under some circumstances the baffle structure may not reach incandescence, while still radiating heat.
- tubular heat absorption structure disposed in said chamber in the path of said hot products of combustion, and means for limiting the heat transfer to a tube comprising a secondary source of radiant heat disposed adjacent to but spaced from the tube and consisting of a baflie heated by radiation from said walls and by said products of combustion and substantially completely shielding said tube from said hot products of cornbustion.
- comblnatlon w1th a heating chamber traversed by hot gaseous products of combustion andwhose walls radiate heat derived from said products of combustion, of tubular heat absorption structure disposed in said chamber in the path of said hot products of combustion, and means for limiting the heat transfer to a tube comprising a secondary source of radiant heat disposed adjacent to but spaced from the tube and consisting of a metallic baflie heated by radiation from said walls and by said products of combustion and substantially completely shielding said tube from said hot products of combustion.
- Petroleum treating apparatus comprising a heating chamber traversed by hot gas- -eous products of combustion and whose walls radiate heat derived from said products of combustion, of tubular heat absorption struc;
- Petroleum treating apparatus comprising a heating chamber traversed by hot gas eous products of combustion and whose walls radiate heat derived from said products of combustion, a bank of petroleum conducting tubes in said chainber and between which said products of'combustion pass, and a secondary source of radiant heat for each of a plurality of said tubes disposed adjacent thereto but spaced therefrom and consisting of a bafile heated by radiation from said walls and said products of combustion shielding the tube from saidhot products of combustion, said baflles spaced from each other to permit passage of said hot products of combustion to other tubes convectively heated by them.
- the method of diminishingthe rate of application of heat to said fluid which comprises heating a tube directly and substantially solely by radiation from an adjaecent secondary source heated by convection by the hot gaseous products of combustion and by heat radiated from said primary source, and by said secondary source substantially completely shielding the tube from absorption of heat directly from the hot gaseous products of combustion throughout substantially the entire longitudinal extent of the tube heated by said secondary source.
- the method of diminishing the P rate of application of heat to said fluid which comprises heating each of some of said tubes directly and substantially solely by radiation from an adjacent secondary sourceheated by convection by the hot gaseous products of combustion and by heat radiated from said primary source, by 'said secondary source substantially completely shielding each of said last named tubes from absorption of heat directly from the hot gaseous products of combustion throughout substantially the entire longitudinal extent of each of said last named tubes heated by said secondary source, and heating others of the tubes by convection by passing the hot gaseous products of combustion between and beyond said secondary sources.
- the method of preventing overheating of a tube and the petroleum which comprises heatinga tube directly and substantially solely by radiation from an adjacent secondary source heated by convection by the hot gaseous products of combustion and by heat radiated from said primary source, and by said secondary source substantially completely shielding the tube from absorption of heat directly from the hot gaseous products of cumbustion throughout substantially the entire longitudinal extent of the tube heated by said secondary source.
- spaced walls for directing the flow of hot products of combustion between the same, heat-absorption units spaced with respect to each other and arranged to constitute jointly a group of such units extending across the ath of flow of said products of combustion, the total area represented by the spaces between adjacent units being a relatively large portion of the entire area occupied by said group to permit free flow of said products of combustion through the spaces between the units of the group and in a direction transversely thereof, and means associated with said group operating'to direct the flow of said products of combustion through said group by way of the spaces between said units'out of intimate contact with the latter and operating to impart heat to said units by radiation.
- heat-absorption units spaced with respect to each other and arranged to constitute jointly a group of such units extending across the path of fiow of said products of combustion, the total area represented by the spaces between adjacent units being a relatively large portion of the entire area occupied by said group to permit free fiow of said products of combustion through the spaces between the units of the group and in a direction transversely thereof, means associated with said group operating to direct the flow of said products of combustion through said group by way of the spaces between said units out of intimate contact with the latter and operating to impart heat to said units by radiation, and a second group of heat-absorption units arranged to constitute jointly a second group similar to the first group, the second group arranged to require that the products of combustion pass between and into intimate contact with the units thereof subsequent to passages of such products through and beyond the first group.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
Description
N0v. 25, 1930. NASH ET AL 1,782,829
HEAT TRANSFER SYSTEM I Filed Jan. 3, 1927 3 1? 3 1m DATTORNEY.
Patented Nov. 2 5, 1930 UNITED STATES PATENT OFFICE.
ARTHUR E. NASH, 0F PHILADELPHIA, AND JAMES S. ALCORN, SYLVANIA, ASSIGNORS TO ALCORN COMBUSTION COMPANY, PENNSYLVANIA,-A CORPORATION OF DELAWABE OI CYNWYD, PENN- OF PHILADELPHIA,
nna'r-rnansrna svs'rnu Application filed. January 3, 1927. Serial No. 158,549.
0111' invention relates to the art of controlling the application of heat to a heat ab sorption structure and has particular referenoe to a method of and apparatus for diminishing the quantity of convection heat applied thereto without to a substantial extent interfering with the radiant heat ap lication.
- n accordance with our invention, suitable heat absorption structure traversed by fluid is disposed in the path of a hot medium, as hot gaseous decreasin from the ot medium to said structure there is utilized a member or baflle spaced, in part at least, therefrom and itself serving as a source of radiant heat.
Further in accordance with our invention, a vertical chamber whose lower wall structure is maintained at incandescence under the influence of hot gaseous products of combustion has disposed transversely thereofroups of tubes traversed by a' fluid, as petroeum or a compound or product thereof and,
for preventing undue temperature rise in those tubes and the therein-contained fluid subjected to radiant heat from thechamber wall structure and to convection heat from the hot gaseous products of combustion, there is utilized bafile structure itself heated to' radiance and constituting a secondary source of radiation and which shields from said gaseous products the tubes last mentioned.
Our invention resides in the method and apparatus of the character hereinafter described and claimed.
For .an understanding of our method and for an illustration of some of the forms our apparatus may take, reference is to be had to the accompanying drawing, in which:
,Fig. l is a perspective view of tubular heat absorption structure having a tubular bafie associated therewith.
' Fig. 2 is a transverse vertical sectional view of the structure shown in Fig. 1.
Fig. 3 is a vertical sectional view showing another form'ofbafle.
Fig. 4 is a vertical sectional view of a heating chamber'containing tubular heat absorpproducts of combustion, and for the heat applied by convection tion structures some having bafiles associated therewith.
Fig. 5 is a side elevational view, partly in vertical section, showing a heat absorption structure with another form of bafile associated therewith.
Fig. 6 is a transversevertical sectional view of the structure shown in Fig. 5. Fig.7 is a transverse vertical sectional view corresponding generally with Fig. 6
showing another form of baflie.
Fig. 8 is an elevational View, partly invertical section, I showing another manner in which a bafile may be supported.
Referring to Fi 4, there is lllustrated a chamber 0 forme by the refractory walls W, W. Within the chamber C there is disposed a suitable heat absorption structure, for
example, a bank of tubes T of iron, steel or other suitable material.
Opening into the bottom of chamber C is a combustion chamber C, which, in the example illustrated, conforms with the one shown in our U. S. Patent No. 1,591,431. It shall be understood, however, that chamber C may be otherwise constructed as found suitable or desirable, for example, as disclosed in our co-pending application, Serial No. 151,307 filed Nov. 29, 1926.
Within the chamber 0 is effected combustion of suitable fuel, ordinarily gas or oil,
which, upon admission thereinto, passes, together with the air and gases, from left toward the right, Fig. 4, the hot gases or products of combustion passing into the bottom of the chamber C, then upwardly and around the tubes T and thence onwardly to any-suitable destination, as, for example, a stack, not shown. 1
Heat radiating from the hot wall structure of the combustion chamber C may be utilized for any desired purpose, for example, it may be transferred substantially exclusively as radiant heat to suitable heat absorption structure, not shown, in the. manner illustrated and described in our aforesaid U. S. Patent No. 1,591,431.
The tubes T are disposed between opposite wallsof the chamber 0 and may be connected in series or other suitable relation by couplings or headers, preferably connected to the tubes externally to the chamber C.
Passing through the tubes T and subjected to temperature rise therein is any suitable fluid material, either gaseous or liquid, as steam to be superheated, or water for the generation of steam. Ordinarily, however, petroleum, or a component or a product thereof under suitable pressure, as superatmospheric pressure, is subjected to elevation of temperature while passing through the tubes T.
The hot gaseous products of combustion emerging from the combustion chamber C pass, at relatively high velocity, between and around the tubes T and, when they are bare or unprotected, contact directly therewith, with resultant high rate of transfer of convection heat thereto. Usually, the gaseous products of combustion are at such elevated temperature that the walls W of chamber C, particularly the lower portions thereof, become incandescent and radiate heat-to the tubes T, particularly the lower groups thereof. As a result, some of the tubes T and the materialpassing therethrough are subjected to excessive temperature rise by the combined action of radiant and convection heat, and
this may result in deterioration of the tubes and damage to the material.
It is well understood that in order to transfer any substantial amount of heat by convection from hot gases to a heat absorption structure, the gases must be brought into contact therewith. Therefore, by deflecting or diverting substantially all of the gaseous products of combustion from those tubes T subjected to radiant heat, the heating effect upon the tube within the longitudinal extent of the secondary source of radiation and due to convection may be substantially entirely eliminated with the result that said tubes and the material passing therethrough are not unduly elevated in temperature. In so doing,
however, the application of radiant heat to said tubes should not be substantially im- .eded.
, 1? To this end, there may be utilized structure which may assume any one of a variety of forms. Forexample, in Figs. 1, 2 and 4, the tubes T are each encompassed by a cylinder or bafile B of greater cross sectional area than a tube T, and preferably circular and of a length corresponding with that of the tube between op osite walls of the chamber C.
Or, the ba emay assume a form such as is shown in Fi 3, that is, one that is circumferentially discontinuous.
With constructions of the character illustrated in Figs-L4, the cylinders or bafile members are supported by the respective tubes. It is obvious, however, that the baflle members may be supported by opposite walls W of chamber C and in such relation that they do not contact with the tubes T,
In Figs. 5 and 6, a substantially V-shaped baffle B is shown as supported in opposite walls W of the chamber C in suitable close relation beneath a tube T and so disposed with respect thereto that the hot gases as they travel upwardly are diverted or deflected to either side of the tube. A baffle utilizable as is the one illustrated in Figs. 5 and 6 may assume any one of a variety of forms, for example, as shown in Fig. 7, where the battle B is semi-circular in shape.
Instead of utilizing the walls 'W as a sup port for the bafile B, Fig. 5, suchbaffle or one of generally similar or'equivalent shape may be supported by a tube T in the manner illustrated in Fig, 8, wherein the members or straps S encircle both the tube and the bafiie to hold the latter in suitable position deflecting the hot gases to either side of the overlying tube.
A battle of the character hereinbefore de scribed under the influence of the heat from the gases and radiated by the incandescent walls W of chamber C in turn becomes incandescent and is a secondary source which radiates heat through the intervening space to the tube T with which said bafile is associated, the amount of radiant heat absorbed by the tube being chan ed sli htl if at all, due to the presence 0 said is. e. At the same time, the bafile deflects or diverts substantially all the hot gaseous products of combustion from said tube within the longitudinal extent of the secondary source of radiant heat with resultant decrease in the amount of convection heat transferred thereto. It follows, then, that those tubes T with which the baflle structure is associated, together with the material passing therethrough, are not subjected to undue temperature rise, since the amount of convection heat applied thereto is substantially diminished.
Only where the bafllle structure is directly in contact with the tubes, as in Figs. 1-4, is heat transmitted thereto by conduction, and, due to the restricted areas of contact surface between the respective tubes and baffles, this type of heat transmission is insubstantial and inconsequential.
The bafiles are preferably. of such shape and so disposed within the chamber C as not to seriously impedethe upward passage of the hot gaseous products of combustion. In other words, the passages for gases between the various tubes T should not, to any substantial extent, be occupied by the baffles or parts thereof.
Baflle structure of the character described herein may be formed by any suitable material, but preferably such as is chemically inert with respect to the gaseous products of combustion, of great resistance to oxidation at high temperature, and. of high heat conductivity. For example, there may be utiliz'ed material as silicon carbide or the like, or and preferably a metal or alloy, as iron, steel, copper, nichrome and the chrome iron and nickel alloys.
It usually obtains that bafile structure of the character described herein attains such high temperature as to become incandescent or luminous.- However, under some circumstances the baffle structure may not reach incandescence, while still radiating heat.
Those tubes T receiving small or inconsequential amounts of radiant heat, as those above the lowermost layers or tiers, Fig. 4, should not be equipped with baflle structure, for, otherwise said tubes and the therein contained material would not be heated to a sufiicient'degree, since the baflie structure would eliminate or reduce the application of convection heat without at the same time continuing the application of radiant heat.
What we claim is:
1. The combination with a heating chamber traversed by hot gaseous products of combustion and whose walls radiate heat derived from said products of combustion,
. of tubular heat absorption structure disposed in said chamber in the path of said hot products of combustion, and means for limiting the heat transfer to a tube comprising a secondary source of radiant heat disposed adjacent to but spaced from the tube and consisting of a baflie heated by radiation from said walls and by said products of combustion and substantially completely shielding said tube from said hot products of cornbustion.
2. The comblnatlon w1th a heating chamber traversed by hot gaseous products of combustion andwhose walls radiate heat derived from said products of combustion, of tubular heat absorption structure disposed in said chamber in the path of said hot products of combustion, and means for limiting the heat transfer to a tube comprising a secondary source of radiant heat disposed adjacent to but spaced from the tube and consisting of a metallic baflie heated by radiation from said walls and by said products of combustion and substantially completely shielding said tube from said hot products of combustion.
3; The combination with a heating chamber traversed by hot gaseous products of combustion and whose walls radiate heat derived from said products of combustion, of a bank of fluid-containing tubes in said chamber and between which said products of combustion pass, and means for limiting the heat transfer to tubes comprising a secondary source of radiant heat for each of a plurality of said tubes disposed adjacent thereto but spaced therefrom and consisting of a batfie heated by radiation from said walls and by said products of combustion and substantially cdmpletely shielding the tube from of fluid-containing tubes in said chamber and 1 between which said products of combustion pass, and means for limiting the heat transfer to tubes comprising a secondary source of radiant heat for each of a plurality of said tubes disposed adjacent thereto but spaced therefrom and consisting of.a metallic baflie heated by said products of combustion and by radiation from said walls and substantially completely shielding the tube from said hot' products of combustion, said bafiies s aced from each other to permit passage 0 said hot products of combustion to other tubes convectively heated by them.
5. Petroleum treating apparatus comprising a heating chamber traversed by hot gas- -eous products of combustion and whose walls radiate heat derived from said products of combustion, of tubular heat absorption struc;
ture through which the petroleum is passed disposed in said chamber in the path of said hot products of combustion, and means for heating a tube and preventing excessive temperature rise thereof and of the contained petroleum comprising a secondary source of radiant heat disposed adjacent to but spaced from the tube and consisting of a baflie heated by radiation from said walls and by said products of combustion and substantially completely shielding said tube from said hot products of combustion.
6. Petroleum treating apparatus comprising a heating chamber traversed by hot gas eous products of combustion and whose walls radiate heat derived from said products of combustion, a bank of petroleum conducting tubes in said chainber and between which said products of'combustion pass, and a secondary source of radiant heat for each of a plurality of said tubes disposed adjacent thereto but spaced therefrom and consisting of a bafile heated by radiation from said walls and said products of combustion shielding the tube from saidhot products of combustion, said baflles spaced from each other to permit passage of said hot products of combustion to other tubes convectively heated by them. i 7. In the art of transferring heat to fluid contained in tubes in a zone in which there are hot gaseous products of'combustion and in which there exists heat radiated from a primary source heated by said products of combustion, the method of diminishingthe rate of application of heat to said fluid which comprises heating a tube directly and substantially solely by radiation from an adjaecent secondary source heated by convection by the hot gaseous products of combustion and by heat radiated from said primary source, and by said secondary source substantially completely shielding the tube from absorption of heat directly from the hot gaseous products of combustion throughout substantially the entire longitudinal extent of the tube heated by said secondary source.
8. In the art of transferring heat to fluid contained in tubes in a zone in which there are hot gaseous products of combustion and in which there exists heat radiated from a primary source heated by said products of combustion, the method of diminishing the P rate of application of heat to said fluid which comprises heating each of some of said tubes directly and substantially solely by radiation from an adjacent secondary sourceheated by convection by the hot gaseous products of combustion and by heat radiated from said primary source, by 'said secondary source substantially completely shielding each of said last named tubes from absorption of heat directly from the hot gaseous products of combustion throughout substantially the entire longitudinal extent of each of said last named tubes heated by said secondary source, and heating others of the tubes by convection by passing the hot gaseous products of combustion between and beyond said secondary sources.
9. In the art of transferring heat to pctroleum contained in tubes in a zone in which there are hot gaseous products of combustion and in which there exists heat radiated from a primary source heated by said products of combustion, the method of preventing overheating of a tube and the petroleum which comprises heatinga tube directly and substantially solely by radiation from an adjacent secondary source heated by convection by the hot gaseous products of combustion and by heat radiated from said primary source, and by said secondary source substantially completely shielding the tube from absorption of heat directly from the hot gaseous products of cumbustion throughout substantially the entire longitudinal extent of the tube heated by said secondary source.
10. In the art of transferring heat to pctroleum contained in tubes in a zone in which there are hot gaseous products of combustion and in which there exists heat radiated from primary source, by said secondary source substantially completely shielding each of said last named tubes from absorption of heat di 1,7ea,sea
rectly from the hot gaseous products of combustion throughout substantially the entire longitudinal extent of each of said last named tubes heated by said secondary source, and heating others of the tubes by convection by passing the hot gaseous products of combustion between and beyond said secondary sources.
11. In a system of the character described, spaced walls for directing the flow of hot products of combustion between the same, heat-absorption units spaced with respect to each other and arranged to constitute jointly a group of such units extending across the ath of flow of said products of combustion, the total area represented by the spaces between adjacent units being a relatively large portion of the entire area occupied by said group to permit free flow of said products of combustion through the spaces between the units of the group and in a direction transversely thereof, and means associated with said group operating'to direct the flow of said products of combustion through said group by way of the spaces between said units'out of intimate contact with the latter and operating to impart heat to said units by radiation.
12. In a system of the character described, spaced walls for directing the flow of'hot products of combustion between the same,
. heat-absorption units spaced with respect to each other and arranged to constitute jointly a group of such units extending across the path of fiow of said products of combustion, the total area represented by the spaces between adjacent units being a relatively large portion of the entire area occupied by said group to permit free fiow of said products of combustion through the spaces between the units of the group and in a direction transversely thereof, means associated with said group operating to direct the flow of said products of combustion through said group by way of the spaces between said units out of intimate contact with the latter and operating to impart heat to said units by radiation, and a second group of heat-absorption units arranged to constitute jointly a second group similar to the first group, the second group arranged to require that the products of combustion pass between and into intimate contact with the units thereof subsequent to passages of such products through and beyond the first group.
ARTHUR E. NASH. JAMES S. ALCORN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US158549A US1782829A (en) | 1927-01-03 | 1927-01-03 | Heat-transfer system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US158549A US1782829A (en) | 1927-01-03 | 1927-01-03 | Heat-transfer system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1782829A true US1782829A (en) | 1930-11-25 |
Family
ID=22568638
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US158549A Expired - Lifetime US1782829A (en) | 1927-01-03 | 1927-01-03 | Heat-transfer system |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1782829A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3190352A (en) * | 1962-08-23 | 1965-06-22 | Modine Mfg Co | Radiator tube protector |
| US3217797A (en) * | 1961-11-30 | 1965-11-16 | United Aircraft Corp | Space radiator |
| US3999600A (en) * | 1973-10-24 | 1976-12-28 | Foster Wheeler Corporation | Heat transfer shields |
| US4142578A (en) * | 1977-09-12 | 1979-03-06 | Exxon Research & Engineering Co. | Heat exchanger impingement protection |
| US4253520A (en) * | 1978-10-26 | 1981-03-03 | The Garrett Corporation | Heat exchanger construction |
| DE2952142A1 (en) * | 1979-12-22 | 1981-06-25 | August Brötje GmbH & Co, 2902 Rastede | Heat-transfer medium direction component - comprises two hollow profiled sections one inside other and in contact |
| DE3047736A1 (en) * | 1980-12-18 | 1982-07-15 | Klein, Schanzlin & Becker Ag, 6710 Frankenthal | Spiral tube double walled heat exchanger - has fixed or loose joint between walls over entire length |
| US4811783A (en) * | 1984-11-15 | 1989-03-14 | Westinghouse Electric Corp. | Heat exchanger tube bundle protection apparatus |
| US4949781A (en) * | 1989-03-20 | 1990-08-21 | Smc O'donnell Inc. | Cooling apparatus |
| US5915468A (en) * | 1996-04-17 | 1999-06-29 | Ebara Corporation | High-temperature generator |
| US6612366B1 (en) * | 2002-02-26 | 2003-09-02 | Lung-Hsi Chuang | Protective wrapping device for a condenser tube |
-
1927
- 1927-01-03 US US158549A patent/US1782829A/en not_active Expired - Lifetime
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3217797A (en) * | 1961-11-30 | 1965-11-16 | United Aircraft Corp | Space radiator |
| US3190352A (en) * | 1962-08-23 | 1965-06-22 | Modine Mfg Co | Radiator tube protector |
| US3999600A (en) * | 1973-10-24 | 1976-12-28 | Foster Wheeler Corporation | Heat transfer shields |
| US4142578A (en) * | 1977-09-12 | 1979-03-06 | Exxon Research & Engineering Co. | Heat exchanger impingement protection |
| US4253520A (en) * | 1978-10-26 | 1981-03-03 | The Garrett Corporation | Heat exchanger construction |
| DE2952142A1 (en) * | 1979-12-22 | 1981-06-25 | August Brötje GmbH & Co, 2902 Rastede | Heat-transfer medium direction component - comprises two hollow profiled sections one inside other and in contact |
| DE3047736A1 (en) * | 1980-12-18 | 1982-07-15 | Klein, Schanzlin & Becker Ag, 6710 Frankenthal | Spiral tube double walled heat exchanger - has fixed or loose joint between walls over entire length |
| US4811783A (en) * | 1984-11-15 | 1989-03-14 | Westinghouse Electric Corp. | Heat exchanger tube bundle protection apparatus |
| US4949781A (en) * | 1989-03-20 | 1990-08-21 | Smc O'donnell Inc. | Cooling apparatus |
| US5915468A (en) * | 1996-04-17 | 1999-06-29 | Ebara Corporation | High-temperature generator |
| US6612366B1 (en) * | 2002-02-26 | 2003-09-02 | Lung-Hsi Chuang | Protective wrapping device for a condenser tube |
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