US1755846A - Gas feeder - Google Patents

Gas feeder Download PDF

Info

Publication number
US1755846A
US1755846A US123575A US12357526A US1755846A US 1755846 A US1755846 A US 1755846A US 123575 A US123575 A US 123575A US 12357526 A US12357526 A US 12357526A US 1755846 A US1755846 A US 1755846A
Authority
US
United States
Prior art keywords
casing
air
chamber
fuel
gas feeder
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
US123575A
Inventor
Noel A Steed
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 US123575A priority Critical patent/US1755846A/en
Application granted granted Critical
Publication of US1755846A publication Critical patent/US1755846A/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

  • This invention relates to fuel vaporization means for engines and has for an object the provision of means for use in connection with a combustion engine whereb thorough vaporization of liquid fuel will e obtained and mixed with a proper amount of air to provide a more readily combustible slow burning fuel mixture, with the expanded gases acting upon the engine piston substantially in the same manner as steam upon the piston of the steam en ine.
  • ' nother object of the invention is the provision of a fuel mixing and feeding means of the above character, which may be applied to re- 3 5 ciprocating and rotary engines, and turbines, and will provide continuous combustion, which adapts it for the last mentioned use.
  • the invention further includes the following novel features and details of construction, to
  • Figure 1 is a sectional view of a fuel feeding means constructed in accordance with the invention.
  • Figure 2 is a section taken substantially on the line 22 of Figure 1.
  • the invention is illustrated as applied to the head H of an engine and comprises an outer casing 10 and an inner 5 casing 11.
  • the walls of the inner casing are spaced from the walls of the outer casing so as to provide an annular chamber 12.
  • the inner casing 11 is in communication with the cylinder of the engine.
  • the outer casing 10 is provided with a head 13 and this head is provided with a liquid fuel inlet passage 14 which is adapted to be connected with a suitable source of liquid fuel supply, the inner end of the passage communicating with the interior of theinner casing 11 through a chamber 15.
  • the outer casing 10 is further provided w th an air inlet ort 16 which communicates with the air cham er 17 communication being controlled by a valve 18 of any suitable character and operated by any suitable means.
  • the outer casing 10 is further provided with a water inlet passage 21 which communicates with a port 22.
  • This casing 11 is provided with circumferentially spaced inclined ports or passages 22, while the annular chamber 12 has locate'd therein an electric heating element 23 which may receive current from a suitable source.
  • the walls of the casing 11 are formed of lava or similar material so that they may be readily heated to incandescence.
  • Conductor wires 24 may extend to the heat ing element 23 through a suitable insulating sleeve 25.
  • Air which supports combustion, may be drawn from a suitable source of air under pressure maintained by a suitable entrance or air chamber under control of the valve '18 and if desired, the air may be suitably heated for this purpose.
  • Air from the chamber 17 passes into the annular space 12,. which forms a superheating chamber, this air coming in direct contact with the walls of the inner casing 11 which become incandescent.
  • This super- 7 heated air passes upward and into the inner casing 11 through the openings 22, the said air passing through these openings at high speed owing to the strong draft within the inner casing.
  • Liquid fuel passes inward 30 through the passage 14 and mixes with an auxiliary air feed through the passage 26 and the tube 20.
  • the tube 20 provides a cooling tube and the air passing through this tube mixes with the liquid fuel and the latter is 55 thoroughly atomized as it enters the upper end of the inner casing 11.
  • the space between the fuel entrance end of this casing and the openings 22 provides a vaporizing chamber V.
  • This fuel vapor is then thoroughly mixed with the air jets passing inward through the open ings 22.
  • Liquid fuel passin through the passage 14 is preferably fed y a time fuel pump (not shown) working synchronously with the valve 18 and when mixed with air from the tube 20 which leaves said tube at high speed, is thoroughly broken up and formed into a very fine spra which enters the vaporizing chamber V.
  • the invention furnishes highly expanded products of combustion under high pressure the air for which is regulated by the valve 18, the latter furnishing complete control over the volume of pressure and heat admitted. In this manner the exact heat, degree and duration of pressure upon the piston head of the engine is completely controlled and gives the same complete control over the engine as is possible with the present type of steam engme.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Description

N. A. STEED GAS FEEDER April 22, 1930.
Filed July 19, 1926 ALfI Sieed Patented Apr. 22, 1930 NOEL A. BTEED, OF PORTLAND, INDIANA GAS FEEDER Application field 'July 19, 1826. Serial No. 128,575.
This invention relates to fuel vaporization means for engines and has for an object the provision of means for use in connection with a combustion engine whereb thorough vaporization of liquid fuel will e obtained and mixed with a proper amount of air to provide a more readily combustible slow burning fuel mixture, with the expanded gases acting upon the engine piston substantially in the same manner as steam upon the piston of the steam en ine.
' nother object of the invention is the provision of a fuel mixing and feeding means of the above character, which may be applied to re- 3 5 ciprocating and rotary engines, and turbines, and will provide continuous combustion, which adapts it for the last mentioned use.
, With the above and other objects in view, the invention further includes the following novel features and details of construction, to
be hereinafter more fully described, illustrated in the accompanying drawings and pointed out in the appended claim.
In the drawings Figure 1 is a sectional view of a fuel feeding means constructed in accordance with the invention.
Figure 2 is a section taken substantially on the line 22 of Figure 1.
Referring particularly to the drawings wherein like characters of reference denote corresponding parts, the invention is illustrated as applied to the head H of an engine and comprises an outer casing 10 and an inner 5 casing 11. The walls of the inner casing are spaced from the walls of the outer casing so as to provide an annular chamber 12. The inner casing 11 is in communication with the cylinder of the engine.
The outer casing 10 is provided with a head 13 and this head is provided with a liquid fuel inlet passage 14 which is adapted to be connected with a suitable source of liquid fuel supply, the inner end of the passage communicating with the interior of theinner casing 11 through a chamber 15.
The outer casing 10 is further provided w th an air inlet ort 16 which communicates with the air cham er 17 communication being controlled by a valve 18 of any suitable character and operated by any suitable means.
The outer casing 10 is further provided with a water inlet passage 21 which communicates with a port 22. This casing 11 is provided with circumferentially spaced inclined ports or passages 22, while the annular chamber 12 has locate'd therein an electric heating element 23 which may receive current from a suitable source. The walls of the casing 11 are formed of lava or similar material so that they may be readily heated to incandescence. Conductor wires 24 may extend to the heat ing element 23 through a suitable insulating sleeve 25.
Air, which supports combustion, may be drawn from a suitable source of air under pressure maintained by a suitable entrance or air chamber under control of the valve '18 and if desired, the air may be suitably heated for this purpose. Air from the chamber 17 passes into the annular space 12,. which forms a superheating chamber, this air coming in direct contact with the walls of the inner casing 11 which become incandescent. This super- 7 heated air passes upward and into the inner casing 11 through the openings 22, the said air passing through these openings at high speed owing to the strong draft within the inner casing. Liquid fuel passes inward 30 through the passage 14 and mixes with an auxiliary air feed through the passage 26 and the tube 20. The tube 20 provides a cooling tube and the air passing through this tube mixes with the liquid fuel and the latter is 55 thoroughly atomized as it enters the upper end of the inner casing 11. The space between the fuel entrance end of this casing and the openings 22 provides a vaporizing chamber V. This fuel vapor is then thoroughly mixed with the air jets passing inward through the open ings 22. Liquid fuel passin through the passage 14 is preferably fed y a time fuel pump (not shown) working synchronously with the valve 18 and when mixed with air from the tube 20 which leaves said tube at high speed, is thoroughly broken up and formed into a very fine spra which enters the vaporizing chamber V. his vapor fuel then moves very slowly and is subjected to extremely high temperature, due to the incandescence of the casing ll,- so that the fuel is thoroughly vaporized and forms a very dry highly superheated mixture which due to its richness, will not burn within the vaporizing chamber. superheated air from the chamber 12 enters the casing 11 through the openings 22 at high speed and strikes the slow moving superheated vapor mixture from the chamber V and is-ignited between the openings 22 and the lower end of the casing 11 so that the interior of this portion of the casing forms a combustion chamber C. A very high temperature clean burning blue flame is thus provid ed which flame maintains the incandescence of the casing 11. A portion of the heat of the casing 11 also serves to superheat the air within the chamber 12. This air and the casing 11 are initially heated by the heating element 23 and after the casing 11 attains proper incandescence, the heating element 23 may be dispensed with.
The invention furnishes highly expanded products of combustion under high pressure the air for which is regulated by the valve 18, the latter furnishing complete control over the volume of pressure and heat admitted. In this manner the exact heat, degree and duration of pressure upon the piston head of the engine is completely controlled and gives the same complete control over the engine as is possible with the present type of steam engme.
The continuous feed is designed for turbine nozzles or feed chests, and the manifolds of engines requiring a continuous feed, while the intermittent or timed feed is designed for I single cylinder engines. The inventlon is susceptible of various changes 1n its form, proportions and minor details of construction and the right is herein reserved to make such changes as properly fall within the scope of the appended claim. Having described the invention what is claimed 1s A burner of the character described comprising an outer casing, an inner casing
US123575A 1926-07-19 1926-07-19 Gas feeder Expired - Lifetime US1755846A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US123575A US1755846A (en) 1926-07-19 1926-07-19 Gas feeder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US123575A US1755846A (en) 1926-07-19 1926-07-19 Gas feeder

Publications (1)

Publication Number Publication Date
US1755846A true US1755846A (en) 1930-04-22

Family

ID=22409491

Family Applications (1)

Application Number Title Priority Date Filing Date
US123575A Expired - Lifetime US1755846A (en) 1926-07-19 1926-07-19 Gas feeder

Country Status (1)

Country Link
US (1) US1755846A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2415748A (en) * 1943-03-08 1947-02-11 Galvin Mfg Corp Liquid fuel preparing apparatus
US2521179A (en) * 1947-04-11 1950-09-05 G W Abernathy Apparatus for spraying plastic material
US2967224A (en) * 1956-10-08 1961-01-03 Ford Motor Co Hot wire igniter
US3190071A (en) * 1961-10-11 1965-06-22 Snecma Igniter device intended in particular for jet engines
US3683215A (en) * 1970-03-16 1972-08-08 Dan Fire Energy Ved Mita Gudma Method and an apparatus for the production of heat and pressure energy
US4118925A (en) * 1977-02-24 1978-10-10 Carmel Energy, Inc. Combustion chamber and thermal vapor stream producing apparatus and method
US4212163A (en) * 1978-06-16 1980-07-15 Mikina Stanley J Heat engine
US5015173A (en) * 1988-06-09 1991-05-14 Vth Ag Verfahrenstechnik Fur Heizung Burner for the combustion of liquids in the gaseous state
US5154597A (en) * 1987-03-13 1992-10-13 Vth Ag Verfahrenstechnik Fur Heizung Burner for combustion of gasified liquid fuels
US5257926A (en) * 1991-12-17 1993-11-02 Gideon Drimer Fast, safe, pyrogenic external torch assembly
US20060154189A1 (en) * 2004-12-08 2006-07-13 Ramotowski Michael J Method and apparatus for conditioning liquid hydrocarbon fuels
US20070254966A1 (en) * 2006-05-01 2007-11-01 Lpp Combustion Llc Integrated system and method for production and vaporization of liquid hydrocarbon fuels for combustion
US20100300103A1 (en) * 2002-10-10 2010-12-02 LLP Combustion, LLC System for vaporization of liquid fuels for combustion and method of use

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2415748A (en) * 1943-03-08 1947-02-11 Galvin Mfg Corp Liquid fuel preparing apparatus
US2521179A (en) * 1947-04-11 1950-09-05 G W Abernathy Apparatus for spraying plastic material
US2967224A (en) * 1956-10-08 1961-01-03 Ford Motor Co Hot wire igniter
US3190071A (en) * 1961-10-11 1965-06-22 Snecma Igniter device intended in particular for jet engines
US3683215A (en) * 1970-03-16 1972-08-08 Dan Fire Energy Ved Mita Gudma Method and an apparatus for the production of heat and pressure energy
US4118925A (en) * 1977-02-24 1978-10-10 Carmel Energy, Inc. Combustion chamber and thermal vapor stream producing apparatus and method
US4212163A (en) * 1978-06-16 1980-07-15 Mikina Stanley J Heat engine
US5154597A (en) * 1987-03-13 1992-10-13 Vth Ag Verfahrenstechnik Fur Heizung Burner for combustion of gasified liquid fuels
US5015173A (en) * 1988-06-09 1991-05-14 Vth Ag Verfahrenstechnik Fur Heizung Burner for the combustion of liquids in the gaseous state
US5257926A (en) * 1991-12-17 1993-11-02 Gideon Drimer Fast, safe, pyrogenic external torch assembly
US20100300103A1 (en) * 2002-10-10 2010-12-02 LLP Combustion, LLC System for vaporization of liquid fuels for combustion and method of use
US8225611B2 (en) 2002-10-10 2012-07-24 Lpp Combustion, Llc System for vaporization of liquid fuels for combustion and method of use
US20060154189A1 (en) * 2004-12-08 2006-07-13 Ramotowski Michael J Method and apparatus for conditioning liquid hydrocarbon fuels
US8702420B2 (en) * 2004-12-08 2014-04-22 Lpp Combustion, Llc Method and apparatus for conditioning liquid hydrocarbon fuels
US9803854B2 (en) 2004-12-08 2017-10-31 Lpp Combustion, Llc. Method and apparatus for conditioning liquid hydrocarbon fuels
US20070254966A1 (en) * 2006-05-01 2007-11-01 Lpp Combustion Llc Integrated system and method for production and vaporization of liquid hydrocarbon fuels for combustion
US8529646B2 (en) 2006-05-01 2013-09-10 Lpp Combustion Llc Integrated system and method for production and vaporization of liquid hydrocarbon fuels for combustion

Similar Documents

Publication Publication Date Title
US1755846A (en) Gas feeder
US4789331A (en) Liquid fuel burner
US4047511A (en) Perfect fuel gasification device for use in combination with a combustion apparatus of internal combustion engine
US2715436A (en) Resonant pulse jet combustion heating device
US2644512A (en) Burner device having heat exchange and gas flow control means for maintaining pyrophoric ignition therein
US1250160A (en) Heating apparatus.
GB848203A (en) Improvements in and relating to liquid fuel burning devices
US2162432A (en) Method of burning oil as gas
US1560550A (en) Hydrocarbon burner
US1377989A (en) Method of operating internal-combustion engines
US1402243A (en) Method of burning fuel and apparatus therefor
US1146679A (en) Oil-vaporizer for combustion-engines.
US1453669A (en) Engine preheater
US1815432A (en) Internal combustion engine
US1400485A (en) Internal-combustion engine
JPS54161129A (en) Linear liquid fuel gasification type combustor
US977208A (en) Method of combustion of oil and gas mixtures.
SU1560923A1 (en) Combustion chamber of gas-turbine engine
US1364696A (en) Combination gas and steam-power engine
US1750571A (en) Internal-combustion engine
JPS58124046A (en) Structure of burner for stirling engine
US433807A (en) Fabrik
US2455221A (en) Blast torch
US783727A (en) Burner.
US1207897A (en) Heater for combustion-engines.