US2491000A - Apparatus for cooling the exhaust end of combustion tubes - Google Patents

Apparatus for cooling the exhaust end of combustion tubes Download PDF

Info

Publication number
US2491000A
US2491000A US749387A US74938747A US2491000A US 2491000 A US2491000 A US 2491000A US 749387 A US749387 A US 749387A US 74938747 A US74938747 A US 74938747A US 2491000 A US2491000 A US 2491000A
Authority
US
United States
Prior art keywords
tube
exhaust end
combustion
cooling
exhaust
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
US749387A
Inventor
Cone Carroll
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.)
Surface Combustion Corp
Original Assignee
Surface Combustion Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Surface Combustion Corp filed Critical Surface Combustion Corp
Priority to US749387A priority Critical patent/US2491000A/en
Application granted granted Critical
Publication of US2491000A publication Critical patent/US2491000A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L17/00—Inducing draught; Tops for chimneys or ventilating shafts; Terminals for flues
    • F23L17/16—Induction apparatus, e.g. steam jet, acting on combustion products beyond the fire

Definitions

  • the present invention relates to heating apparatus for use with heat treating furnaces for producing heat therein without contaminating the furnace chamber with products of combustion, the heating element comprising an internally fired tube whose ends are outside ofthe furnace chamber. Where the ends of the heatin tube extend out of the furnace chamber, infiltration of air intothe chamber is prevented by gastight joints. However, because of the relatively high temperature of the spent heating gases at the exhaust end of the tube, special precautions must be taken to prevent overheating of the connection between the furnace wall and the projecting exhaust end of the tube.
  • the object of the present invention is to provide improvements in means for maintaining the connection between the furnace wall and projecting exhaust end of the tube relatively cool and more particularly to provide a relatively simple and practical air coolin system for said connection.
  • FIG. 1 shows an internally fired heating tube of hair-pin type so that both the firing and exhaust ends of the tube extend out of the furnace chamber through one and the same wall portion thereof, the improvement at the exhaust end of the tube being in elevation and the firing end of the tube being in section.
  • Fig. 2 is an enlarged sectional view of the improvement at the exhaust end of the heating tube.
  • the heating tube is indicated at I0, the tube for illustrative purposes being shown as of hairpin type so that its ends extend through one and the same wall ll of a furnace chamber.
  • the wall H includes a metal plate l2 which constitutes part of the furnace casing.
  • the tube I is fired in a manner to avoid localized heating, and to this end a stream of fuel gas undiluted with air is introduced into the front end or mouth I4 of the tube by a burner tube l3 coaxial therewith, the burner tube projecting some distance into said mouth.
  • Air for combustion enters the tube l0 through the mouth l4 thereof, the latter being open to the atmosphere.
  • the main fuel supply pipe is indicated at I5.
  • the fuel issuing from the burner tube is ignited by flame issuing from a pilot l6 to which combustible mixture is supplied by a tube li around the burner tube [3, the supply line for Said. mixture being indicated at l8.
  • the burner 4. Claims. (01. 12s 91) 2 arrangement thus far described is well known in the 'art and, therefore, need not be further de-- scribed.
  • a relatively strong draft is maintained through the heating tube ID by a suction producing device IS which is coupled to the exhaust 'end of the tube in a manner resently described. so that the fuel fromthe burner tube l3 and combustion sup.- porting air from the mouth l4 may be said to be drawn into the tube-by said draft.
  • the device 19 will ordinarily be an aspirator consisting of an entraining tube 20- into which motive fluid such as compressed air is discharged by a jet orifice nozzle 2
  • the exhaust end of the heating tube in is anchored to the furnace casing l2 by means comprisin a flange 22 carried by the terminal end of the tube, the back side of this flange being adapted to seat gas-tight against a flange 23 at the outer end of a barrel 24 whose inner end is welded gas-tight to the furnace casing I2, the two flanges being held in abutting relation by bolts 25, the latter being shown as of a length to extend through a disc 21 spaced from the front side of the tube flange 22 by spacer elements 29.
  • the disc 21 constitutes a supporting means for a tube 28, which projects coaxially into the exhaust end of the heating tube a substantial distance inwardly from the terminal flange 22 on the latter but not far enough to extend into the heating portion of the tube or in other words not beyond the plane of the inner side of the furnace wall II.
  • the tube 28 is substantially smaller than the discharge end of the heating tube so as to provide an annular air passage 30 therebetween. Centering fingers on the inner end of the tube 28 are indicated at 3 I.
  • the outer end of the tube 28 is coupled to the suction producing device 49; hence, the suction produced by the latter will draw the waste combustion gas into the outer end of the tube 28 and will draw cooling air into the outer end of the combustion tube ID by way of the annular passage 30, hence overheating of the connection between the exhaust end of the combustion tube l0 and the furnace casing l 2 is prevented in a relatively simple and practical manner. It will, of course, be understood that only a relatively small portion of the partial vacuum produced by the suction producing means I9 is utilized to draw air into the tube in by way of the annular space or passage 30.
  • the degree of suction effective in the tube 28 may be regulated as circumstances require and by reducing the spacing between the disc 21 and the flange 22 on the terminal end of the tube In, the effective inlet area of the annular passage 30 may be decreased as conditions may require.
  • the combination which comprises a first tube forming an elongate combustion chamber, a furnace wall having an opening through which the exhaust end of the tube extends, means forming a gas-tight connection between the outer side of said wall and the projecting end of said tube, a second tube extending a relatively short distance into the projecting exhaust end of the first tube in spaced relation to form between the two tubes an annular passage, and a suction producing device coupled to the outer end of the second tube for drawing waste combustion gas into the second tube and cooling air into said annular passage.
  • the combination which comprises a first tube forming an elongate combustion chamber, a furnace wall having an opening through which the exhaust end of said tube extends, the exterior side of said wall comprising a metal casing beyond which the said end of the tube extends, means including said casing forming a gas-tight connection between said wall and the. projecting end of said tube, a second tube extending a relatively short distance into the exhaust end of the first tube in spaced relation to form between the two tubes an annular passage, and suction producing means coupled to the outer end of the second tube for drawing waste combustion gas into the second tube and cooling air into said annular passage.
  • the said gas-tight connection comprising a barrel extending from said casing coaxial with the exhaust end of the first tube, a flange at the outer end of said barrel, and a complemental flange at the exhaust end of the first tube for seating against the flange on the barrel.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chimneys And Flues (AREA)

Description

C. CONE APPARATUS FOR COOLING THE EXHAUST Filed May 20, 1947 END OF COMBUSTION TUBES lllllllllllll I l 1 O INVENTOR. fiarrd/Co/re BY $14 4&4 A rio/e/vfy Dec. 13, 1949 Patented Dec. 13, 1949 z-- APPARATUS FOR COOLING THE EXHAUST END OF COMBUSTION TUBES CarrolLCone, near Toledo, Ohio, assi-gnor to Surface Combustion Corporation,
corporation of Ohio Toledo, Ohio, a
Application May 20, 1947, Serial No. 749,387-" The present invention'relates to heating apparatus for use with heat treating furnaces for producing heat therein without contaminating the furnace chamber with products of combustion, the heating element comprising an internally fired tube whose ends are outside ofthe furnace chamber. Where the ends of the heatin tube extend out of the furnace chamber, infiltration of air intothe chamber is prevented by gastight joints. However, because of the relatively high temperature of the spent heating gases at the exhaust end of the tube, special precautions must be taken to prevent overheating of the connection between the furnace wall and the projecting exhaust end of the tube. The object of the present invention is to provide improvements in means for maintaining the connection between the furnace wall and projecting exhaust end of the tube relatively cool and more particularly to provide a relatively simple and practical air coolin system for said connection.
For a consideration of what I consider to be novel and my invention, attention is directed to the following specification and the claims appended thereto.
In the accompanying drawing- Fig. 1 shows an internally fired heating tube of hair-pin type so that both the firing and exhaust ends of the tube extend out of the furnace chamber through one and the same wall portion thereof, the improvement at the exhaust end of the tube being in elevation and the firing end of the tube being in section.
Fig. 2 is an enlarged sectional view of the improvement at the exhaust end of the heating tube.
The heating tube is indicated at I0, the tube for illustrative purposes being shown as of hairpin type so that its ends extend through one and the same wall ll of a furnace chamber. At its outer side the wall H includes a metal plate l2 which constitutes part of the furnace casing.
The tube I is fired in a manner to avoid localized heating, and to this end a stream of fuel gas undiluted with air is introduced into the front end or mouth I4 of the tube by a burner tube l3 coaxial therewith, the burner tube projecting some distance into said mouth. Air for combustion enters the tube l0 through the mouth l4 thereof, the latter being open to the atmosphere. The main fuel supply pipe is indicated at I5. The fuel issuing from the burner tube is ignited by flame issuing from a pilot l6 to which combustible mixture is supplied by a tube li around the burner tube [3, the supply line for Said. mixture being indicated at l8. The burner 4. Claims. (01. 12s 91) 2 arrangement thus far described is well known in the 'art and, therefore, need not be further de-- scribed.
A relatively strong draft is maintained through the heating tube ID by a suction producing device IS which is coupled to the exhaust 'end of the tube in a manner resently described. so that the fuel fromthe burner tube l3 and combustion sup.- porting air from the mouth l4 may be said to be drawn into the tube-by said draft. The device 19 will ordinarily be an aspirator consisting of an entraining tube 20- into which motive fluid such as compressed air is discharged by a jet orifice nozzle 2|.
The exhaust end of the heating tube in is anchored to the furnace casing l2 by means comprisin a flange 22 carried by the terminal end of the tube, the back side of this flange being adapted to seat gas-tight against a flange 23 at the outer end of a barrel 24 whose inner end is welded gas-tight to the furnace casing I2, the two flanges being held in abutting relation by bolts 25, the latter being shown as of a length to extend through a disc 21 spaced from the front side of the tube flange 22 by spacer elements 29.
The disc 21 constitutes a supporting means for a tube 28, which projects coaxially into the exhaust end of the heating tube a substantial distance inwardly from the terminal flange 22 on the latter but not far enough to extend into the heating portion of the tube or in other words not beyond the plane of the inner side of the furnace wall II. The tube 28 is substantially smaller than the discharge end of the heating tube so as to provide an annular air passage 30 therebetween. Centering fingers on the inner end of the tube 28 are indicated at 3 I. The outer end of the tube 28 is coupled to the suction producing device 49; hence, the suction produced by the latter will draw the waste combustion gas into the outer end of the tube 28 and will draw cooling air into the outer end of the combustion tube ID by way of the annular passage 30, hence overheating of the connection between the exhaust end of the combustion tube l0 and the furnace casing l 2 is prevented in a relatively simple and practical manner. It will, of course, be understood that only a relatively small portion of the partial vacuum produced by the suction producing means I9 is utilized to draw air into the tube in by way of the annular space or passage 30.
By adjusting a throttling valve in the supply line 32 leading to the nozzle 2| the degree of suction effective in the tube 28 may be regulated as circumstances require and by reducing the spacing between the disc 21 and the flange 22 on the terminal end of the tube In, the effective inlet area of the annular passage 30 may be decreased as conditions may require.
It will, of course, be understood that the air drawn into the passage 30 will be drawn into the inner end of the suction tube 28 along with the oncoming waste heating gases and thus partially cool the latter before they reach the aspirator l9.
What I claim is:
1. In apparatus of the class described, the combination which comprises a first tube forming an elongate combustion chamber, a furnace wall having an opening through which the exhaust end of the tube extends, means forming a gas-tight connection between the outer side of said wall and the projecting end of said tube, a second tube extending a relatively short distance into the projecting exhaust end of the first tube in spaced relation to form between the two tubes an annular passage, and a suction producing device coupled to the outer end of the second tube for drawing waste combustion gas into the second tube and cooling air into said annular passage.
2. The combination set forth in claim 1, which includes a disc on the outer portion of the second tube, and means for varying the spacing between said disc and the front end of the annular passage.
3. In apparatus of the class described, the combination which comprises a first tube forming an elongate combustion chamber, a furnace wall having an opening through which the exhaust end of said tube extends, the exterior side of said wall comprising a metal casing beyond which the said end of the tube extends, means including said casing forming a gas-tight connection between said wall and the. projecting end of said tube, a second tube extending a relatively short distance into the exhaust end of the first tube in spaced relation to form between the two tubes an annular passage, and suction producing means coupled to the outer end of the second tube for drawing waste combustion gas into the second tube and cooling air into said annular passage.
4. In the combination set forth in claim 3, the said gas-tight connection comprising a barrel extending from said casing coaxial with the exhaust end of the first tube, a flange at the outer end of said barrel, and a complemental flange at the exhaust end of the first tube for seating against the flange on the barrel.
CARROLL CONE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,189,623 Reid July 4, 1916 2,077,043 Gehnrich Apr. 13, 1937
US749387A 1947-05-20 1947-05-20 Apparatus for cooling the exhaust end of combustion tubes Expired - Lifetime US2491000A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US749387A US2491000A (en) 1947-05-20 1947-05-20 Apparatus for cooling the exhaust end of combustion tubes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US749387A US2491000A (en) 1947-05-20 1947-05-20 Apparatus for cooling the exhaust end of combustion tubes

Publications (1)

Publication Number Publication Date
US2491000A true US2491000A (en) 1949-12-13

Family

ID=25013555

Family Applications (1)

Application Number Title Priority Date Filing Date
US749387A Expired - Lifetime US2491000A (en) 1947-05-20 1947-05-20 Apparatus for cooling the exhaust end of combustion tubes

Country Status (1)

Country Link
US (1) US2491000A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2870829A (en) * 1954-03-26 1959-01-27 Selas Corp Of America Radiant heat fuel burner
US3032326A (en) * 1954-07-15 1962-05-01 Midland Ross Corp Two-stage combustion direct fired and radiant tube furnace
US4858592A (en) * 1987-02-20 1989-08-22 Belshaw Bros., Inc. Burner system
US5642660A (en) * 1996-02-22 1997-07-01 Killgore; Robert R. Gas fired deep fat fryer
US20080283047A1 (en) * 2007-05-18 2008-11-20 John Vancak Radiant heater assembly

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1189623A (en) * 1915-10-28 1916-07-04 Grace L Peine Smoke-pipe air-check.
US2077043A (en) * 1936-02-01 1937-04-13 Charles L Gehnrich Industrial heater

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1189623A (en) * 1915-10-28 1916-07-04 Grace L Peine Smoke-pipe air-check.
US2077043A (en) * 1936-02-01 1937-04-13 Charles L Gehnrich Industrial heater

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2870829A (en) * 1954-03-26 1959-01-27 Selas Corp Of America Radiant heat fuel burner
US3032326A (en) * 1954-07-15 1962-05-01 Midland Ross Corp Two-stage combustion direct fired and radiant tube furnace
US4858592A (en) * 1987-02-20 1989-08-22 Belshaw Bros., Inc. Burner system
US5642660A (en) * 1996-02-22 1997-07-01 Killgore; Robert R. Gas fired deep fat fryer
US20080283047A1 (en) * 2007-05-18 2008-11-20 John Vancak Radiant heater assembly
US7654257B2 (en) * 2007-05-18 2010-02-02 John Vancak Radiant heater assembly

Similar Documents

Publication Publication Date Title
US2188133A (en) Heating apparatus
US2857961A (en) Oil burners
US4310303A (en) Plug-in recuperator and method
US3275057A (en) Tunnel burners
US2458542A (en) Low velocity oil and gas burner
US5059117A (en) Radiant tube furnace and method of burning a fuel
US1729763A (en) Apparatus and method of fuel burning
US2570554A (en) Radiant gas burner internally fired
US2973032A (en) Gas or oil burner
US2571336A (en) Gaseous fuel burner for furnace walls
US2491000A (en) Apparatus for cooling the exhaust end of combustion tubes
US2826249A (en) Multiple nozzle gas burner
US2620967A (en) Gas ejector apparatus for a catalyst regenerator
US2148466A (en) Heating apparatus
US1805066A (en) Gas burner or nozzle
US1791561A (en) Apparatus for heating air
US2480255A (en) Burner for soaking pit furnaces and the like
US1975033A (en) Oil burner
US2051099A (en) Heating apparatus
US1603462A (en) Purnace
US2048644A (en) Annealing apparatus
US2843107A (en) Combustion apparatus having pilot burner with booster
US2700380A (en) Radiant tube heater and combustion air preheater therefor
US2207010A (en) Recuperating burner block
GB990346A (en) Burner nozzle for use in burning gaseous media