US2051099A - Heating apparatus - Google Patents
Heating apparatus Download PDFInfo
- Publication number
- US2051099A US2051099A US56622A US5662235A US2051099A US 2051099 A US2051099 A US 2051099A US 56622 A US56622 A US 56622A US 5662235 A US5662235 A US 5662235A US 2051099 A US2051099 A US 2051099A
- Authority
- US
- United States
- Prior art keywords
- tube
- fuel
- section
- radiator
- oblong
- 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
Links
- 238000010438 heat treatment Methods 0.000 title description 6
- 239000000446 fuel Substances 0.000 description 32
- 238000002485 combustion reaction Methods 0.000 description 20
- 239000007789 gas Substances 0.000 description 9
- 230000008093 supporting effect Effects 0.000 description 7
- 238000007599 discharging Methods 0.000 description 5
- 239000012530 fluid Substances 0.000 description 5
- 230000001939 inductive effect Effects 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000001105 regulatory effect Effects 0.000 description 3
- 238000003756 stirring Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000010763 heavy fuel oil Substances 0.000 description 1
- 230000001976 improved effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
- F23C3/002—Combustion apparatus characterised by the shape of the combustion chamber the chamber having an elongated tubular form, e.g. for a radiant tube
Definitions
- the invention relates to fuel fired radiator tubes and has for its object to provide a radiator tube of such'form that it may be uniformly heated to such high temperatures that it shall have special utility as a heat radiating element in furnace chambers and the like where high temperature heating elements are required.
- Fig. 1 shows the improved heating apparatus partly in elevation and partly in section and as extending through the wall of a furnace chamber which is to be heated;
- Fig. 2 is a cross sectional view on line 22 of Fig. 1;
- Figs. 3 and 4 are section views of parts shown in elevation in Fig. 1.
- the heat radiator tube is generally indicated at It and is shown as of hair-pin type with its intake and exhaust ends extending through a wall ll of a furnace chamber which is to be heated. Fuel is delivered to the intake end of the tube It by means generally indicated atl2, and air for supporting combustion of the fuel is induced to enter said end by a draft producing means generally indicated at l3 at the exhaust end of the tube.
- the means l2 for delivering fuel to the radiator tube includes a fuel delivery tube It to which fuel gas is supplied by a pressure gas supply pipe l5 having a regulating valve IS.
- the fuel tube It is shown as extending a substantial distance into the inlet end of the radiator tube l0 primarily to compensate for the thickness of the furnace wall II.
- the fuel tube I4 is of relatively large cross sectional area without any constriction at its discharge end such as would tend to prevent the fuel stream from maintaining its integrity for a substantial distance after discharge from the tube.
- said means preferably takes the form of jet entraining apparatus consisting of a jet orifice nozzle is positioned to discharge into an eductor tube [9 which forms in eifect an extension of the radiator tube.
- the fluid pressure supply pipe for the nozzle is indicated at 20 and is provided with a regulating valve 2
- the fuel tube l4 extends beyond the tube 22 and the space between the two tubes at the discharge side of the ring 25 constitutes an annular combustion chamber 26 for the combustible mixture flowing through said ring.
- the present invention provides a radiator tube of special form as will now be described.
- the tube passes through the furnace wall II and for a substantial distance into the furnace chamber, it is circular as indicated at 28.
- This ci'rcular part 28 is followed by part 29 whose cross sectional area is somewhat greater than the preceding section and which is oblong in cross section and of greater length than the preceding part.
- This difference in contour between the two parts 28 and 29 materially speeds up interunixing of the air and fuel 'in the composite stream as it flows from the part 28 to the part 29 with the result that combustion is correspondingly accelerated but not to such degree as to cause objectionable spot heating.
- the increased liberation of heat is compensated for by the greater heat absorbing surface of the part 29 and consequently the tube does not become overheated.
- the present invention provides for repeated acceleration of combustion by following the expanded part 29 with parts 30-35 of which parts 30, 32 and 34 are preferably circular and of the same cross section area as the first part 28 whereas the parts 33 and 35 are preferably of the same cross sectional contour andarea as the part 29.
- This periodic expansion and contraction of the gases promotes intermixing of the gases in the stream as will now be readily understood with the result that combustion of residual fuel will be accelerated and combustion completed before the gases reach the exhaust end of the tube.
- the last portion 36 of the tube where it passes through the furnace wall II is preferably circular in cross section and of the same diameter as the first portion 28. It will be readily appreciated that in a hair-pin tube the bend 3
- the first expanded part or section 29 is of relatively greater importance than the other expanded sections 33 and 35, it being noted in this connection that the last named sections are severally shorter than the first section 29.
- the short width or minor axis of the several expanded sections is preferably the same as the diameter of the preceding round section as is clearly shown in Fig. 2 whereby the gases in flowing from the round into the, oblong section of the tube expand only in two opposite directions, it having been found that the turbulence or stirring produced in the gases by this arrangement gives the best results.
- the amount of fuel that can be burned in the tube is greatly in excess of what could be burned if the tube were of uniform cross sectional area through its length, and consequently, the utility of the tube is correspondingly increased due to the high temperature to which it can be heated.
- a radiator tube and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube having an oblong section preceded and followed by a circular section whose diameter is substantially the same as the minor axis of the oblong section.
- a radiator tube and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube being of hair-pin type and having between its bend and its intake end an oblong section preceded and followed by a circular section whose diameter is substantially the same as the minor axis of the oblong section.
- a radiator tube, and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube being of hair-pin type and having in each of its legs an oblong section preceded and followed by a circular section whose diameter is substantially the same as the 20 minor axis of the oblong section.
- a radiator tube, and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube being of hair-pin type and having in each of its legs an oblong section preceded and followed by a circular section whose diameter is substantially the same as the minor axis of the oblong section, the oblong portion between the intake end of the tube and its bend being longer than the other oblong por- 35 tion.
- a radiator tube and means for burning fuel therein comprising power-operated suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging unignited fuel therelnto, and said tube comprising an alternate succession of restricted and expanded sections.
- a combustion chamber consisting of a radiator tube having a substantial portion of its length between its ends of greater cross sectional area than the next preceding and following portions and the distance between the intake end of the tube and the point where said portion begins being many times less than the distance between the point where said portion ends and the exhaust end of the tube, said enlarged portion being oblong in cross section and the next adjacent portion being circular and the diameter of the circular portion being substantially the same as the short axis of the oblong portion.
- a combustion chamber consisting of a radiator tube having a substantial portion of its length between its ends of greater cross sectional area than the next preceding and following portions and the distance between the intake end of the tube and the point where said portion begins being many times less than the distance between the point where said portion ends and the exhaust end ot the tube, and said the ends of the last mentioned dist are x u: least one additional enlarged portion of shorter length then the first mentioned portion.
- a combustion ber consisting of a, radiator tube be en sueoewon of circular and oblong sections, means for flowing ,unignitecl fuel into the intake end of the tube, means for producing a strong draft vthroturh the tube whereby to cause air to stream into the intake end of the tube and how towards the exhaust end thereof to support combustion of the fuel as it flows through the tube, and means at the intake end of the tube for insuring that ignition of combustible mixture resulting from tntermixlng of the flowing air and fuel shell on 10 our es and when said mixture is initially formed.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Of Fluid Fuel (AREA)
Description
Ailg. 1 8, 1936. T. w. MUNFORD HEATING APPARATUS Filed Dec. 30 1955 INVENTOI? Z'W/Wuhforc/ A TTORNE Y Patented Aug. 18, 1936 Iss tries Surface Combustion Corporation,
Toledo,
Ohio, a corporation of New York Application December 30, 1935, Serial No. 56,622
10 Claims.
The invention relates to fuel fired radiator tubes and has for its object to provide a radiator tube of such'form that it may be uniformly heated to such high temperatures that it shall have special utility as a heat radiating element in furnace chambers and the like where high temperature heating elements are required. Other objects will more fully appear hereinafter.
The various features of novelty and invention will be fully described in connection with the accompanying drawing forming part of this specification and wherein',-
Fig. 1 shows the improved heating apparatus partly in elevation and partly in section and as extending through the wall of a furnace chamber which is to be heated;
Fig. 2 is a cross sectional view on line 22 of Fig. 1; and
Figs. 3 and 4 are section views of parts shown in elevation in Fig. 1.
The heat radiator tube is generally indicated at It and is shown as of hair-pin type with its intake and exhaust ends extending through a wall ll of a furnace chamber which is to be heated. Fuel is delivered to the intake end of the tube It by means generally indicated atl2, and air for supporting combustion of the fuel is induced to enter said end by a draft producing means generally indicated at l3 at the exhaust end of the tube.
The means l2 for delivering fuel to the radiator tube includes a fuel delivery tube It to which fuel gas is supplied by a pressure gas supply pipe l5 having a regulating valve IS. The fuel tube It is shown as extending a substantial distance into the inlet end of the radiator tube l0 primarily to compensate for the thickness of the furnace wall II. The fuel tube I4 is of relatively large cross sectional area without any constriction at its discharge end such as would tend to prevent the fuel stream from maintaining its integrity for a substantial distance after discharge from the tube.
It is essential to the successful firing of the radiator tube that the combustion supporting air be induced to enter the intake end of the tube by draft producing means at the exhaust end of the tube, and said means preferably takes the form of jet entraining apparatus consisting of a jet orifice nozzle is positioned to discharge into an eductor tube [9 which forms in eifect an extension of the radiator tube. The fluid pressure supply pipe for the nozzle is indicated at 20 and is provided with a regulating valve 2| to permit the entraining eifectto be adjusted as desired.
Inasmuch as the strong draft through the radiator tube tends to pull the flame away from the fuel tube and thus causes it to go out, means are provided for constantly insuring ignition of the air and fuel where they initially intermix in combustible proportions and the means herein disclosed for that purpose will now be described. Surrounding the fuel tube It in spaced relation is a tube 22 to which preformed combustible mixture under pressure is supplied by a supply pipe 23 having regulating valve 24. In the tube 22 near its outlet end is a ring 25 through which the fuel .tube 14 passes and which is provided with a plurality of relatively small passages through which the mixture supplied to the outer tube 22 must flow to pass from the latter. The fuel tube l4 extends beyond the tube 22 and the space between the two tubes at the discharge side of the ring 25 constitutes an annular combustion chamber 26 for the combustible mixture flowing through said ring. The outer ends of the tubes Hi and 22, therefore, become highly heated and along with the high temperature gases issuing from said chamber constantly insure ignition of the fuel issuing from the inner tube M.
In order to permit the burning of a greater volume of fuel in the radiator tube I0 than could possibly be burned if the tube were of uniform cross sectional area through its length, the
present invention provides a radiator tube of special form as will now be described. Where the tube passes through the furnace wall II and for a substantial distance into the furnace chamber, it is circular as indicated at 28. This ci'rcular part 28 is followed by part 29 whose cross sectional area is somewhat greater than the preceding section and which is oblong in cross section and of greater length than the preceding part. This difference in contour between the two parts 28 and 29 materially speeds up interunixing of the air and fuel 'in the composite stream as it flows from the part 28 to the part 29 with the result that combustion is correspondingly accelerated but not to such degree as to cause objectionable spot heating. The increased liberation of heat is compensated for by the greater heat absorbing surface of the part 29 and consequently the tube does not become overheated. Since combustion tends to decelerate due to the air and fuel becoming diluted with products of combustion, the present invention provides for repeated acceleration of combustion by following the expanded part 29 with parts 30-35 of which parts 30, 32 and 34 are preferably circular and of the same cross section area as the first part 28 whereas the parts 33 and 35 are preferably of the same cross sectional contour andarea as the part 29. This periodic expansion and contraction of the gases promotes intermixing of the gases in the stream as will now be readily understood with the result that combustion of residual fuel will be accelerated and combustion completed before the gases reach the exhaust end of the tube. The last portion 36 of the tube where it passes through the furnace wall II is preferably circular in cross section and of the same diameter as the first portion 28. It will be readily appreciated that in a hair-pin tube the bend 3| is also an important factor in materially stirring up the gases as they flow therethrough.
The first expanded part or section 29 is of relatively greater importance than the other expanded sections 33 and 35, it being noted in this connection that the last named sections are severally shorter than the first section 29. The short width or minor axis of the several expanded sections is preferably the same as the diameter of the preceding round section as is clearly shown in Fig. 2 whereby the gases in flowing from the round into the, oblong section of the tube expand only in two opposite directions, it having been found that the turbulence or stirring produced in the gases by this arrangement gives the best results.
The advantages of a radiator tube constructed in accordance with the present invention may be stated as follows:
(1) Owing to the greater internal volume than a circular tube of equal length, a longer time is expansion away from the outer core of the stream, and this outward movement induces a turbulent area at the core thus promoting thorough mixing of the air and fuel in the process of burning. Owing to the tubeform, ample space is provided for flow through the tube on either side of the turbulent area without excessive friction losses.
(3) In spite of the fact that turbulence is produced in successive parts of the tube, no localized heating is produced since the turbulent areas are separated from the tube walls by those portions of the total gas stream flowing along the walls in substantially stream line flow under the influence of the draft source at the exhaust end of the tube.
(4) By utilizing a radiator tube of the type herein disclosed, the amount of fuel that can be burned in the tube is greatly in excess of what could be burned if the tube were of uniform cross sectional area through its length, and consequently, the utility of the tube is correspondingly increased due to the high temperature to which it can be heated.
What I claim is:
1. In combination, a radiator tube, and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube having an oblong section preceded and followed by a circular section whose diameter is substantially the same as the minor axis of the oblong section. I
2. In combination, a radiator tube, and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube being of hair-pin type and having between its bend and its intake end an oblong section preceded and followed by a circular section whose diameter is substantially the same as the minor axis of the oblong section.
3. In combination, a radiator tube, and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube being of hair-pin type and having in each of its legs an oblong section preceded and followed by a circular section whose diameter is substantially the same as the 20 minor axis of the oblong section.
4. In combination, a radiator tube, and means for burning fuel therein comprising a suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging fluid fuel thereinto, and said tube being of hair-pin type and having in each of its legs an oblong section preceded and followed by a circular section whose diameter is substantially the same as the minor axis of the oblong section, the oblong portion between the intake end of the tube and its bend being longer than the other oblong por- 35 tion.
5. In combination, a radiator tube, and means tube for a portion of its length remote from the last named means being of greater cross sectional area than in the preceding portion of the tube.
6. In combination, a radiator tube, and means for burning fuel therein comprising power-operated suction producing means coupled to the exhaust end of the tube for inducing combustion supporting air to enter the intake end of the tube, means at the air intake end of the tube for discharging unignited fuel therelnto, and said tube comprising an alternate succession of restricted and expanded sections.
7. A combustion chamber consisting of a radiator tube having a substantial portion of its length between its ends of greater cross sectional area than the next preceding and following portions and the distance between the intake end of the tube and the point where said portion begins being many times less than the distance between the point where said portion ends and the exhaust end of the tube, said enlarged portion being oblong in cross section and the next adjacent portion being circular and the diameter of the circular portion being substantially the same as the short axis of the oblong portion.
8. A combustion chamber consisting of a radiator tube having a substantial portion of its length between its ends of greater cross sectional area than the next preceding and following portions and the distance between the intake end of the tube and the point where said portion begins being many times less than the distance between the point where said portion ends and the exhaust end ot the tube, and said the ends of the last mentioned dist are x u: least one additional enlarged portion of shorter length then the first mentioned portion.
9. A combustion chamber oonsistmg 0: e rm?- ator tube of hale-pm type ha between its bend and its intake end a portion which is oblong in cross section and which is preceded and. followed by e circular portion whose diameter is substantially the same as the minor axis of the oblong portion.
10. In combination, a. combustion ber consisting of a, radiator tube be en sueoewon of circular and oblong sections, means for flowing ,unignitecl fuel into the intake end of the tube, means for producing a strong draft vthroturh the tube whereby to cause air to stream into the intake end of the tube and how towards the exhaust end thereof to support combustion of the fuel as it flows through the tube, and means at the intake end of the tube for insuring that ignition of combustible mixture resulting from tntermixlng of the flowing air and fuel shell on 10 our es and when said mixture is initially formed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US56622A US2051099A (en) | 1935-12-30 | 1935-12-30 | Heating apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US56622A US2051099A (en) | 1935-12-30 | 1935-12-30 | Heating apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
US2051099A true US2051099A (en) | 1936-08-18 |
Family
ID=22005612
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US56622A Expired - Lifetime US2051099A (en) | 1935-12-30 | 1935-12-30 | Heating apparatus |
Country Status (1)
Country | Link |
---|---|
US (1) | US2051099A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423018A (en) * | 1942-10-14 | 1947-06-24 | Henry M Griffoul | Rotary drum furnace |
US2607191A (en) * | 1947-11-28 | 1952-08-19 | United Aircraft Corp | Vortex producing mechanism for mixing combustion chamber fluids |
US2635866A (en) * | 1950-04-05 | 1953-04-21 | Oscar R Olson | Radiant tube portable furnace |
US3221796A (en) * | 1963-11-29 | 1965-12-07 | Midland Ross Corp | Self-stabilizing combustion apparatus |
US3225757A (en) * | 1962-11-09 | 1965-12-28 | Hazen Engineering Company | Radiant tube heaters |
US4870947A (en) * | 1987-05-26 | 1989-10-03 | Nippon Furnace Kogyo Kaisha, Ltd. | Radiant tube burner |
-
1935
- 1935-12-30 US US56622A patent/US2051099A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423018A (en) * | 1942-10-14 | 1947-06-24 | Henry M Griffoul | Rotary drum furnace |
US2607191A (en) * | 1947-11-28 | 1952-08-19 | United Aircraft Corp | Vortex producing mechanism for mixing combustion chamber fluids |
US2635866A (en) * | 1950-04-05 | 1953-04-21 | Oscar R Olson | Radiant tube portable furnace |
US3225757A (en) * | 1962-11-09 | 1965-12-28 | Hazen Engineering Company | Radiant tube heaters |
US3221796A (en) * | 1963-11-29 | 1965-12-07 | Midland Ross Corp | Self-stabilizing combustion apparatus |
US4870947A (en) * | 1987-05-26 | 1989-10-03 | Nippon Furnace Kogyo Kaisha, Ltd. | Radiant tube burner |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3905751A (en) | Gas burner | |
US2458543A (en) | Low velocity gas burner | |
US2725929A (en) | Combustion chamber type burner | |
US4453913A (en) | Recuperative burner | |
US2059523A (en) | Heating apparatus | |
US4062343A (en) | Tube firing burner | |
US1273466A (en) | Fuel-burner. | |
US4125360A (en) | Steam atomizing burner | |
US2561200A (en) | Internal gas burner | |
US2745250A (en) | Reverse vortex combustion chamber | |
US4060380A (en) | Furnace having burners supplied with heated air | |
US2051099A (en) | Heating apparatus | |
US2539165A (en) | Dispersible fuel burner having a reverse gas flow flame stabilizer | |
US3187798A (en) | Radiant gas burner | |
US3320999A (en) | Internal combustion burner | |
US3187799A (en) | Self-stabilizing combustion apparatus and method | |
US3225757A (en) | Radiant tube heaters | |
US2904108A (en) | Radiant cup type gas burner | |
US3265113A (en) | Gas burner apparatus | |
US1805066A (en) | Gas burner or nozzle | |
US3189017A (en) | Fuel burning air heating apparatus | |
US3247884A (en) | Burner means for furnaces | |
GB537657A (en) | Improvements relating to heating elements or radiants for furnaces | |
US2250680A (en) | Combustion tube burner | |
US2876831A (en) | Internal-combustion burners |