US1415780A - Method of producing heat - Google Patents

Method of producing heat Download PDF

Info

Publication number
US1415780A
US1415780A US404248A US40424820A US1415780A US 1415780 A US1415780 A US 1415780A US 404248 A US404248 A US 404248A US 40424820 A US40424820 A US 40424820A US 1415780 A US1415780 A US 1415780A
Authority
US
United States
Prior art keywords
air
fuel
mixture
combustion
producing heat
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
US404248A
Inventor
Bowen William Spencer
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 US404248A priority Critical patent/US1415780A/en
Application granted granted Critical
Publication of US1415780A publication Critical patent/US1415780A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/12Devices or methods for making a gas mixture for a combustion engine

Definitions

  • My invention relates to the production of heat by the continuous burning of gaseous mixtures and subsequently cooling said gases to the desired temperature for efficient utilization in doing useful work.
  • the incoming fuel and air mixture is preheated in the heater by the hot gases of combustionprevious to ignition.
  • the velocity of flow need be only sufiicient to carry enough fuel and air to maintain combustion. This point is considered very important as the loss of efficiency involved due to the high velocitles required in surface combustion is considerable.
  • the air used for cooling purposes is introduced after combustion has taken place and this air is previously heated by passing the same through a jacket surrounding the heater thus producing a heat insulating jacket and the air moving through this jacket returns heat to the heater which would otherwise be lost.
  • the heater of my invention also effectivel employs radiant heat by providing coneshaped shells which are enveloped by the burning fuel and air mixture and the heat from these shells is reflectedand r e-reflected in the interior thereof until absorbed by the air or other gas while passing through them.
  • Fig. 1 shows a vertical section of an embodiment of my invention.
  • Fig.2 is a side elevation of the outer conical tube.
  • Fig. 3 is a sid elevation of the intermediate conical tube.
  • Two cone-shaped bodies 6 preferably of thin metallic material, so as to proximate shells, are placed base to base within the air jacket or casing 16, and securedtogether by any suitable means such as bolts (not shown) passing through the contacting base flanges of the same. While it is preferable that the conical bodies should be made of sheet metal such as iron, an infusible material may also be used if deemed advisable.
  • a conical tube surrounds a portion of each of the cones 6, in spaced relation thereto in order to form an annular passageway which is adapted to contain the burning gaseous mixture as will hereinafter appear.
  • the cones 5 are connected directly to the fuel pipes 2 which may conduct either gaseous or vaporized oil fuel for use in the heater.
  • Air or other combustion supporting gas is admitted through the pipe 3 which prefer" ably surrounds the fuel pipe 2 and connects to a cone-shaped outer tube 4 which surrounds the tube 5 in spaced relation so as to provide an annular passage whereby compressed air may be fed into the annular space between the conical tubes 4 and5.
  • the surfaces of the cones 5 are provided with a multiplicity of perforations see Fig. 3) and the bases of the cones 4: are closed so that all air admitted to the annular spaces between cones 4i and 5 must pass through these perforations. In this way a complete fuel and air mixture is obtained within the heater just before the ignition point is reached.
  • the conical expansion of the flame has a good effect on its burning. since it slows down the initial fuel velocity gradually so that proper mixture and burning can take place more easily and evenly.
  • Air is supplied to the jacket 16 by connection 17 which leads to an air pump or compressed air reservoir- (not shown). After circulating through the air jacket and becoming heated the air is conducted by pipes 1 to the nozzles 7 and into the interior of the conical shells 6. It should be noted that this air has no direct contact with the flame but receives its heat almost solely by radiation from the shells 6.
  • the compressed air passes through the cones 6 and passes in a diverging stream corresponding to the apex angle of the conical shells and passes out through ports 14 near the bases of the cones into the general receiving chamber within the casing 16 which beyond the point of ignition and burning of the fuel and air mixture.
  • This air is preheated by its passage through the jacket, and the fuel mixture is preheated by the hot gases surrounding the conical tubes 4 and 5.
  • a spark plug 18 is provided in each of the cones 5 beyond the closed end of the outer conical tube 4; in order to ignite the fuel mixture formed with the air in the annular pasprovided which may be bolted to the plate 10 or fastened thereto in any suitable manner.
  • water instead of air may be passed throughconnection 17, jacket 16 and pipes 1 to suitable nozzles 7 and sprayed into the interior of the conical bodies 6, thus being co'nverted'into steam by radiant heat.
  • the steam will then pass through ports lt and minglewith the combustionproducts in the :manner; described above for the compressed am.
  • the method of producing heat which consists in conducting fuel and a combustion supporting gas in proportions to form an explosive mixture in co-axial gradual tapering streams, mixing the fuel and gas near the point of ignition, preheating the mixture by the hot gases of combustion and introducing air for cooling the products of combustion.
  • the method of producing heat which consists in enveloping a diverging moving column of air in a burning fuel and air mixture and subsequently introducing air from said column into the products of combustion.

Landscapes

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

Description

W. S. BOWEN.
METHOD OF PRODUCING HEAT.
APPLICATION FILED AUG-17,1920.
1,415,786. Patented May 9,1922.
10 3 W00 Mon TES PATENT OFFICE.
WILLIAM SPENCER BOWEN, or New YORK, N. Y.
mn'rnon or PRODUCING HEAT.
Specification of Letters Patent.
Patented May 9,1922.
Application filed August 17, 1920. Serial No. 404,248.
To all whom it may concern."
Be it known that 1. WILLIAM SPENCER Bowrm, a citizen of the United States, residing at New York, in the county of New York and State of New York, have invented new and useful. Improvements in Methods of Producing Heat, of which the following is a specification.
My invention relates to the production of heat by the continuous burning of gaseous mixtures and subsequently cooling said gases to the desired temperature for efficient utilization in doing useful work.
According to my invention the incoming fuel and air mixture is preheated in the heater by the hot gases of combustionprevious to ignition. There is no flow of explosive mixture as in surface combustion and consequently the velocity of flow need be only sufiicient to carry enough fuel and air to maintain combustion. This point is considered very important as the loss of efficiency involved due to the high velocitles required in surface combustion is considerable. Furthermore, the air used for cooling purposes is introduced after combustion has taken place and this air is previously heated by passing the same through a jacket surrounding the heater thus producing a heat insulating jacket and the air moving through this jacket returns heat to the heater which would otherwise be lost.
The heater of my invention also effectivel employs radiant heat by providing coneshaped shells which are enveloped by the burning fuel and air mixture and the heat from these shells is reflectedand r e-reflected in the interior thereof until absorbed by the air or other gas while passing through them.
In the drawing accompanying this application:-
Fig. 1 shows a vertical section of an embodiment of my invention.
Fig.2 is a side elevation of the outer conical tube.
Fig. 3 is a sid elevation of the intermediate conical tube.
Two cone-shaped bodies 6 preferably of thin metallic material, so as to proximate shells, are placed base to base within the air jacket or casing 16, and securedtogether by any suitable means such as bolts (not shown) passing through the contacting base flanges of the same. While it is preferable that the conical bodies should be made of sheet metal such as iron, an infusible material may also be used if deemed advisable. A conical tube surrounds a portion of each of the cones 6, in spaced relation thereto in order to form an annular passageway which is adapted to contain the burning gaseous mixture as will hereinafter appear. The cones 5 are connected directly to the fuel pipes 2 which may conduct either gaseous or vaporized oil fuel for use in the heater.
Air or other combustion supporting gas is admitted through the pipe 3 which prefer" ably surrounds the fuel pipe 2 and connects to a cone-shaped outer tube 4 which surrounds the tube 5 in spaced relation so as to provide an annular passage whereby compressed air may be fed into the annular space between the conical tubes 4 and5. The surfaces of the cones 5 are provided with a multiplicity of perforations see Fig. 3) and the bases of the cones 4: are closed so that all air admitted to the annular spaces between cones 4i and 5 must pass through these perforations. In this way a complete fuel and air mixture is obtained within the heater just before the ignition point is reached. The conical expansion of the flame has a good effect on its burning. since it slows down the initial fuel velocity gradually so that proper mixture and burning can take place more easily and evenly.
Air is supplied to the jacket 16 by connection 17 which leads to an air pump or compressed air reservoir- (not shown). After circulating through the air jacket and becoming heated the air is conducted by pipes 1 to the nozzles 7 and into the interior of the conical shells 6. It should be noted that this air has no direct contact with the flame but receives its heat almost solely by radiation from the shells 6.
The compressed air passes through the cones 6 and passes in a diverging stream corresponding to the apex angle of the conical shells and passes out through ports 14 near the bases of the cones into the general receiving chamber within the casing 16 which beyond the point of ignition and burning of the fuel and air mixture. This air is preheated by its passage through the jacket, and the fuel mixture is preheated by the hot gases surrounding the conical tubes 4 and 5. A spark plug 18 is provided in each of the cones 5 beyond the closed end of the outer conical tube 4; in order to ignite the fuel mixture formed with the air in the annular pasprovided which may be bolted to the plate 10 or fastened thereto in any suitable manner.
It is contemplated also by my invention that water instead of air may be passed throughconnection 17, jacket 16 and pipes 1 to suitable nozzles 7 and sprayed into the interior of the conical bodies 6, thus being co'nverted'into steam by radiant heat. The steam will then pass through ports lt and minglewith the combustionproducts in the :manner; described above for the compressed am. I
Having thus described my invention, what Icclaim asnew and desire to secure by Letters Patent, is 1 1 1. The method of producing heat, which consists in vconducting fuel and a combustion supporting gas in proportions to form an explosive mixture in co-axial gradual tapering streams, mixing the fuel and gas near the point of ignition, enveloping a coneshaped moving column of air in the burning fuel and gas mixture and subsequently introducing air from said column into the products of combustion.
2. The method of producing heat, which consists in conducting fuel and a combustion supporting gas in proportions to form an explosive mixture in co-axial gradual tapering streams, mixing the fuel and gas near the point of ignition, preheating the mixture by the hot gases of combustion and introducing air for cooling the products of combustion.
3. The method of producing heat, which consists in enveloping a diverging moving column of air in a burning fuel and air mixture and subsequently introducing air from said column into the products of combustion.
In testimony whereof I have hereunto set my hand in presence of two subscribing witnesses.
WILLIAM SPENCER BOWEN.
WVitnesses:
CHAS. J. WILLIs, LESTER STORK.
US404248A 1920-08-17 1920-08-17 Method of producing heat Expired - Lifetime US1415780A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US404248A US1415780A (en) 1920-08-17 1920-08-17 Method of producing heat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US404248A US1415780A (en) 1920-08-17 1920-08-17 Method of producing heat

Publications (1)

Publication Number Publication Date
US1415780A true US1415780A (en) 1922-05-09

Family

ID=23598806

Family Applications (1)

Application Number Title Priority Date Filing Date
US404248A Expired - Lifetime US1415780A (en) 1920-08-17 1920-08-17 Method of producing heat

Country Status (1)

Country Link
US (1) US1415780A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2627163A (en) * 1947-12-16 1953-02-03 Ingersoll Rand Co One-half wave length resonant explosion gas unit
US2647364A (en) * 1948-09-10 1953-08-04 Kellogg M W Co Pulse jet engine with spontaneously ignitable fuel and oxidizer
US2890569A (en) * 1954-05-03 1959-06-16 Phillips Petroleum Co Removal of carbon deposits in jet engines
US3772881A (en) * 1970-06-04 1973-11-20 Texaco Ag Apparatus for controllable in-situ combustion

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2627163A (en) * 1947-12-16 1953-02-03 Ingersoll Rand Co One-half wave length resonant explosion gas unit
US2647364A (en) * 1948-09-10 1953-08-04 Kellogg M W Co Pulse jet engine with spontaneously ignitable fuel and oxidizer
US2890569A (en) * 1954-05-03 1959-06-16 Phillips Petroleum Co Removal of carbon deposits in jet engines
US3772881A (en) * 1970-06-04 1973-11-20 Texaco Ag Apparatus for controllable in-situ combustion

Similar Documents

Publication Publication Date Title
US1879186A (en) Apparatus for igniting liquid fuel
US2095065A (en) Surface combustion process
US2725929A (en) Combustion chamber type burner
US2286909A (en) Combustion chamber
US2572338A (en) Autothermic cracking reactor
US1273466A (en) Fuel-burner.
US2561793A (en) Incandescent gas burner for furnace wall
US2645673A (en) Process of producing acetylene
US2561200A (en) Internal gas burner
US2552277A (en) Furnace
US1415780A (en) Method of producing heat
US1755846A (en) Gas feeder
US2904108A (en) Radiant cup type gas burner
US2102152A (en) Premixing device for fluid fuel burners
US1747522A (en) Heating apparatus employing powdered fuel
US1647675A (en) Burner for gaseous and powderous solid fuel
US1677811A (en) Gas burner
US1925131A (en) Carbon black producer
US2340120A (en) Pressure heating device
US2131977A (en) Burner
US1244864A (en) Method of heating.
US1469178A (en) Apparatus for supplying heat
US2086290A (en) Apparatus for heating the ends of rods, bars, tubes, or the like
US1425343A (en) Oil or gas burner
US1415781A (en) Method of producing heat