US1618808A - Apparatus for burning powdered fuel - Google Patents
Apparatus for burning powdered fuel Download PDFInfo
- Publication number
- US1618808A US1618808A US17163A US1716325A US1618808A US 1618808 A US1618808 A US 1618808A US 17163 A US17163 A US 17163A US 1716325 A US1716325 A US 1716325A US 1618808 A US1618808 A US 1618808A
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- US
- United States
- Prior art keywords
- retort
- air
- wall
- fuel
- chamber
- 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
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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
- F23C3/006—Combustion apparatus characterised by the shape of the combustion chamber the chamber being arranged for cyclonic combustion
- F23C3/008—Combustion apparatus characterised by the shape of the combustion chamber the chamber being arranged for cyclonic combustion for pulverulent fuel
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S48/00—Gas: heating and illuminating
- Y10S48/04—Powdered fuel injection
Definitions
- My invention relates to improvements in apparatus for burning powdered fuel,. and 'the object of the improvements is to provide an apparatus in' which the efliciency of the combustion and the life of the apparatus are increased.
- my invention consists in providing a combustion chamber which is provided at one end with means for supplying powdered fuel, and which has air for supporting combustlon supplied thereto through passages IDEIClP III the side wall of the chamber and in a direction circumferential of the jet of powdered fuel flowing through said chamber.
- Fig. 1 is a sectional elevation of the apparatusas used in connection with a steam boiler
- v p Fig. 2 is a section taken on theiline 2-2 of Flg. 1.
- the in combustion apparatus comprises a combustion chamber 1 having a cylindrical wall 2 made from refractory material. At one end of the. said chamber a tubular inlet 4 of annular cross-section opens into the com- ?5 bust-ion chamber. said inlet having an intake pipe 6 and including a helical vane 5 adaptcd to impart whirling movement to the fuel.
- the wall 2 of the chamber is provided with transverse passages 3 for the admission of to air for supporting combustion, and in the example shown inthe figures and more particularly in Fig. 1, the direction of the said passages and the helical passage provided by the vane 5 are such that the air and the f fuel are whirled around within the combustion chamber in the same direction.
- the central part of thetubular member 4 has a cross-sectional area such as to permit access therethrough to the combastion chamber, and it is normally closed by a gate 7.
- the combustion chamber is provided with a bottom discharge 8 for ashes, sa1d discharge being located adjacent tothe fire tube ,9 of a steam boiler 10 adapted to be heated from the combustion chamber 1.
- the cylindrical wall 2 is provided with a jacket 11, and the annular chamber 12 thus provided is divided by partitions 13 into chambers, each of the chambers being connected with the air supply main 14 by a pipe 15 comprising regulating means such as butterfly valves 16. Further, each chamber has a supply of steam through a pipe 17 including a cock 18 and connected with a steam supply pipe 19. As appears more particularly from Fig. 1 the inner wall of the annular inlet flares outwardly at its delivery end, so that the fuel is delivered into the combustion chamber in outward direction. l
- the fuel is admitted into the combustion cham: ber 1 through the pipe 4 along a spiral path. and when admitted to the saidchamber it is thrown against the wall 2. Within the chamber it is mixed with the air admitted through the passages 3 in tangential direction, and the mixture flows along a helical line of small pitch towards the fire tube 9.
- An agilparatus for the burning of powdered e1 comprising a cylindrical retort having tangential slots through its cylindrical wall, a jacket extending about said cylindrical slotted wall and forming an annular air spaeetherewith, annular partitions for dividing said air space into adjoining oompartments, an air supply under pressure to each compartment w lerehy to mtroduoe air through the tangential slots and into the retort in a stream about the axis of the retort, and an annular inlet for the powdered material to the end of the retort and substantially coaxial therewith, said annular inlet havin an out-turned'inner portion for deflecting the powdered material toward the cylindrical slotted wall of the retort immediately on introduction of the material to the retort.
- An apparatus for the burning of powdered fuel comprising a cylindrical retort having tangential slots through its cylindrical wall, a jacket extending about said cylindrical slotted walland forming an annular air s ace therewith, annular partitions for dividing said air space into adjoining compartments, an air supply under ressure to each compartment whereby to introduce air through the tangential slots and into the retort in a stream about the powdered materi to the end of the retort and substantially coaxial therewith, said annular inlet having an out-turned inner portion for deflecting the powdered material toward the cylindrical slotted wall of the retort immediately on introduction of the material to the retort and a spiral vane in said annular inlet for impart-mg to the powdered material prior to introduction'into the retort a rotary movement about the axis of the retort.
- An a paratus for the burning of powdered uel comprising a cylindrical retort having tangential slots through its cylindrical wall, a jacket extending about said cylindrical slotted wall and forming an annular air s ace therewith, annular artitions'tfor divi ing said air space into a joinmg compartments, an an supply under pressure to each compartment whereby to introduce air through the tangential slots and into the retort in a stream about the axis of the retort, an annular inlet for the powdered material to the end of the retort and substantially coaxial therewith, said annular inlet having an out-turned inner portion for deflecting the wdered material toward the c lindrical s otted wall of the retort immediately on introduction of the partments.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Description
Feb. .22 1927,
' 1,618,808 E. BURG APPARATUS. FOR BURNING POWDERED FUEL Filed March 21 1925 /"i WL I literacy Patented Feb. 22, 1927.
UNITED STATES PATENT OFFIQ/E.
' EUGEN BUR-G, OI ESSEN-ON-THE RUHB, GERMANY- APPABA'1US FOR BURNING POWDERED FUEL.
Application filed March 21, 1925, Serial No. 17,163, and in Germany March 28, 1924.
My invention relates to improvements in apparatus for burning powdered fuel,. and 'the object of the improvements is to provide an apparatus in' which the efliciency of the combustion and the life of the apparatus are increased. With this object in view my invention consists in providing a combustion chamber which is provided at one end with means for supplying powdered fuel, and which has air for supporting combustlon supplied thereto through passages IDEIClP III the side wall of the chamber and in a direction circumferential of the jet of powdered fuel flowing through said chamber. In the preferred form of the invention the supply of the powdered fuel'is made such as to 1mpart to the jet of fuel a whirling path For the purpose of explaining the invention, an example embodying the same has .been shown invthe accompanying drawing, in which the same reference characters have been used in all the views to indicate corresponding parts In said drawing.
Fig. 1 is a sectional elevation of the apparatusas used in connection with a steam boiler, and v p Fig. 2 is a section taken on theiline 2-2 of Flg. 1.
- In theexample shown in the drawing the in combustion apparatus comprises a combustion chamber 1 having a cylindrical wall 2 made from refractory material. At one end of the. said chamber a tubular inlet 4 of annular cross-section opens into the com- ?5 bust-ion chamber. said inlet having an intake pipe 6 and including a helical vane 5 adaptcd to impart whirling movement to the fuel. The wall 2 of the chamber is provided with transverse passages 3 for the admission of to air for supporting combustion, and in the example shown inthe figures and more particularly in Fig. 1, the direction of the said passages and the helical passage provided by the vane 5 are such that the air and the f fuel are whirled around within the combustion chamber in the same direction. But I wish it to be understood that I do not limit myself to this'feature, and that in some cases I dispose the said passages'relatively to eachother in such a way that air and-fuel are whirled around in opposite directions. The central part of thetubular member 4 has a cross-sectional area such as to permit access therethrough to the combastion chamber, and it is normally closed by a gate 7. At the end opposite to the fuel .inlet the combustion chamber is provided with a bottom discharge 8 for ashes, sa1d discharge being located adjacent tothe fire tube ,9 of a steam boiler 10 adapted to be heated from the combustion chamber 1. The cylindrical wall 2 is provided with a jacket 11, and the annular chamber 12 thus provided is divided by partitions 13 into chambers, each of the chambers being connected with the air supply main 14 by a pipe 15 comprising regulating means such as butterfly valves 16. Further, each chamber has a supply of steam through a pipe 17 including a cock 18 and connected with a steam supply pipe 19. As appears more particularly from Fig. 1 the inner wall of the annular inlet flares outwardly at its delivery end, so that the fuel is delivered into the combustion chamber in outward direction. l
In the operation of' the apparatus the fuel is admitted into the combustion cham: ber 1 through the pipe 4 along a spiral path. and when admitted to the saidchamber it is thrown against the wall 2. Within the chamber it is mixed with the air admitted through the passages 3 in tangential direction, and the mixture flows along a helical line of small pitch towards the fire tube 9.
By centrifugal action the solid particles of the fuel are thrown towards the wall of the combustion chamber, so that they move along a comparatively long path while being continuously brought into contact with fresh air. The volatile and readily ignited por tions move through the axial portion ofthe combustion chamber where their path is comparatively short. The ashes are separated from the combustion gases only at the end of-thd combustion chamber and above the discharge 8, because earlier separation is prevented by the tangential current of air. The air admitted through the wall of the chamber has a cooling action,' so that the wall is in a less degree subject to thedestructive action of the heat. The steam admitted from the pipe 19 is heated within the wall i 2, and it is decomposed within the said wall stood that I do not limit myself to. the construction shown in the drawing.
I claim: 1. An agilparatus for the burning of powdered e1 comprising a cylindrical retort having tangential slots through its cylindrical wall, a jacket extending about said cylindrical slotted wall and forming an annular air spaeetherewith, annular partitions for dividing said air space into adjoining oompartments, an air supply under pressure to each compartment w lerehy to mtroduoe air through the tangential slots and into the retort in a stream about the axis of the retort, and an annular inlet for the powdered material to the end of the retort and substantially coaxial therewith, said annular inlet havin an out-turned'inner portion for deflecting the powdered material toward the cylindrical slotted wall of the retort immediately on introduction of the material to the retort.
Y 2. An apparatus for the burning of powdered fuel comprising a cylindrical retort having tangential slots through its cylindrical wall, a jacket extending about said cylindrical slotted walland forming an annular air s ace therewith, annular partitions for dividing said air space into adjoining compartments, an air supply under ressure to each compartment whereby to introduce air through the tangential slots and into the retort in a stream about the powdered materi to the end of the retort and substantially coaxial therewith, said annular inlet having an out-turned inner portion for deflecting the powdered material toward the cylindrical slotted wall of the retort immediately on introduction of the material to the retort and a spiral vane in said annular inlet for impart-mg to the powdered material prior to introduction'into the retort a rotary movement about the axis of the retort. i
3. An a paratus for the burning of powdered uel comprising a cylindrical retort having tangential slots through its cylindrical wall, a jacket extending about said cylindrical slotted wall and forming an annular air s ace therewith, annular artitions'tfor divi ing said air space into a joinmg compartments, an an supply under pressure to each compartment whereby to introduce air through the tangential slots and into the retort in a stream about the axis of the retort, an annular inlet for the powdered material to the end of the retort and substantially coaxial therewith, said annular inlet having an out-turned inner portion for deflecting the wdered material toward the c lindrical s otted wall of the retort immediately on introduction of the partments.
In testimony whereotI hereunto aflix my signature.
' EUGEN BURG.-
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1618808X | 1924-03-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1618808A true US1618808A (en) | 1927-02-22 |
Family
ID=7737344
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US17163A Expired - Lifetime US1618808A (en) | 1924-03-28 | 1925-03-21 | Apparatus for burning powdered fuel |
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US (1) | US1618808A (en) |
Cited By (72)
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US2420999A (en) * | 1942-08-11 | 1947-05-27 | Phillips Petroleum Co | Apparatus for the manufacture of amorphous carbon |
US2464791A (en) * | 1943-11-05 | 1949-03-22 | Claude A Bonvillian | Apparatus for the combustion of fuel |
US2468415A (en) * | 1945-08-17 | 1949-04-26 | Daniel E Stair | Method of and apparatus for burning coal |
US2469272A (en) * | 1946-09-06 | 1949-05-03 | Gilbert & Barker Mfg Co | Pressure atomizing oil burner |
US2473347A (en) * | 1943-04-08 | 1949-06-14 | Cleaver Brooks Co | Air directing means in gun type burners |
US2476507A (en) * | 1946-10-30 | 1949-07-19 | Benjamin J Parmele | Cyclone burner |
US2479240A (en) * | 1941-03-07 | 1949-08-16 | Babcock & Wilcox Co | Fuel burning apparatus |
US2485207A (en) * | 1946-09-06 | 1949-10-18 | Gilbert & Barker Mfg Co | Air control for tubular combustion chambers of oil burners |
US2488911A (en) * | 1946-11-09 | 1949-11-22 | Surface Combustion Corp | Combustion apparatus for use with turbines |
US2512196A (en) * | 1946-05-15 | 1950-06-20 | Comb Eng Superheater Inc | Air vane for fuel burners |
US2516063A (en) * | 1948-08-19 | 1950-07-18 | Gilbert & Barker Mfg Co | Pressure atomizing oil burner with a built-in combustion chamber |
US2539165A (en) * | 1946-11-30 | 1951-01-23 | Cyclotherm Corp | Dispersible fuel burner having a reverse gas flow flame stabilizer |
US2560074A (en) * | 1948-12-21 | 1951-07-10 | Lummus Co | Method and apparatus for burning fuel |
US2560076A (en) * | 1949-06-14 | 1951-07-10 | Lummus Co | Method and apparatus for burning fuel |
US2572829A (en) * | 1948-12-28 | 1951-10-30 | Phillips Petroleum Co | Coal gasification process and apparatus |
US2573910A (en) * | 1945-08-21 | 1951-11-06 | Comb Eng Superheater Inc | Method for burning pulverized coal |
US2578051A (en) * | 1943-07-03 | 1951-12-11 | Goetaverken Ab | Solid fuel furnace |
US2590660A (en) * | 1949-03-02 | 1952-03-25 | United Carbon Company Inc | Apparatus for the manufacture of carbon black |
US2594312A (en) * | 1944-08-31 | 1952-04-29 | Babcock & Wilcox Co | Fuel burning apparatus |
US2603949A (en) * | 1947-11-28 | 1952-07-22 | United Aircraft Corp | Combustion chamber with diverse air paths and vortices producing vanes therein for jet propulsion or gas turbine power plants |
US2616256A (en) * | 1946-09-16 | 1952-11-04 | Babcock & Wilcox Co | Gas turbine plant using solid ash-containing fuel |
US2625791A (en) * | 1946-08-17 | 1953-01-20 | Bituminous Coal Research | Coal pulverization and combustion apparatus for gas turbine power plants |
US2627719A (en) * | 1947-06-13 | 1953-02-10 | Edward A Stalker | Gas turbine combustion chamber having controlled laminar flow of air for combustion and insulation |
US2635564A (en) * | 1948-09-15 | 1953-04-21 | Power Jets Res & Dev Ltd | Combustion system for pulverulent fuel |
US2638745A (en) * | 1943-04-01 | 1953-05-19 | Power Jets Res & Dev Ltd | Gas turbine combustor having tangential air inlets for primary and secondary air |
US2656254A (en) * | 1948-12-11 | 1953-10-20 | Columbian Carbon | Carbon black |
US2659201A (en) * | 1947-11-26 | 1953-11-17 | Phillips Petroleum Co | Gas turbine combustion chamber with provision for turbulent mixing of air and fuel |
US2664402A (en) * | 1949-03-29 | 1953-12-29 | Phillips Petroleum Co | Protection of refractories in a reaction system from high temperatures by blanketing gases |
US2672012A (en) * | 1941-07-03 | 1954-03-16 | Babcock & Wilcox Co | Combustion chamber for air-borne solid fuel |
US2678615A (en) * | 1949-12-20 | 1954-05-18 | Rosenblad Corp | Method for burning sticky, watercontaining liquid fuel |
US2680951A (en) * | 1948-01-02 | 1954-06-15 | Power Jets Res & Dev Ltd | Combustion apparatus for burning particles of solid or heavy liquid fuel in a fast moving stream |
US2689605A (en) * | 1950-11-29 | 1954-09-21 | Selas Corp Of America | Furnace structure |
US2692479A (en) * | 1948-04-09 | 1954-10-26 | Power Jets Res & Dev Ltd | Combustion apparatus for gas turbine plants using slow-burning fuel |
US2695496A (en) * | 1952-03-05 | 1954-11-30 | Daniel And Florence Guggenheim | Structure for feeding, intermingling, vaporizing, and igniting combustion liquids ina combustion chamber for rocket-type propulsion apparatus |
US2698050A (en) * | 1949-06-10 | 1954-12-28 | Lummus Co | Combustion for liquid fuels |
US2703275A (en) * | 1951-01-08 | 1955-03-01 | Martin A Elliott | Apparatus for conducting heterogeneous chemical reactions |
US2731955A (en) * | 1956-01-24 | Pulverized coal furnace | ||
US2738776A (en) * | 1951-06-13 | 1956-03-20 | Pollopas Patents Ltd | Furnace burners |
US2769411A (en) * | 1951-11-06 | 1956-11-06 | Rosenblad Corp | Fuel combustion process and apparatus |
US2777407A (en) * | 1951-10-02 | 1957-01-15 | Babcock & Wilcox Co | Fuel burning apparatus |
US2800092A (en) * | 1951-06-13 | 1957-07-23 | Pollopas Patents Ltd | Burning of pulverized fuel |
US2828608A (en) * | 1950-11-17 | 1958-04-01 | Power Jets Res & Dev Ltd | Improved construction of combustion chamber of the cyclone or vortex type |
US2861526A (en) * | 1952-11-19 | 1958-11-25 | Babcock & Wilcox Co | Fuel burning apparatus |
US2865820A (en) * | 1951-04-18 | 1958-12-23 | Koppers Co Inc | Method for heat treatment of finely divided solid media |
US2924512A (en) * | 1954-06-01 | 1960-02-09 | Phillips Petroleum Co | Carbon black apparatus |
US2927632A (en) * | 1955-02-09 | 1960-03-08 | Fraser Reginald Percy | Fuel combustion apparatus and the production of controlled gaseous effluents therefrom |
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US3453976A (en) * | 1967-01-30 | 1969-07-08 | Gen Incinerators Of California | Method and apparatus for destroying bulk paper and other bulk materials |
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US3685496A (en) * | 1969-09-23 | 1972-08-22 | Sulzer Ag | Steam boiler having a water space traversed by a flue gas duct |
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US4338782A (en) * | 1979-11-23 | 1982-07-13 | Marchand William C | Gas turbine combustion system utilizing renewable and non-critical solid fuels with residue remover to minimize environmental pollution |
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1925
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Cited By (80)
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---|---|---|---|---|
US2731955A (en) * | 1956-01-24 | Pulverized coal furnace | ||
US2479240A (en) * | 1941-03-07 | 1949-08-16 | Babcock & Wilcox Co | Fuel burning apparatus |
DE976588C (en) * | 1941-03-07 | 1963-12-05 | Babcock & Wilcox Dampfkessel W | Steam generator with melting chamber firing |
US2672012A (en) * | 1941-07-03 | 1954-03-16 | Babcock & Wilcox Co | Combustion chamber for air-borne solid fuel |
DE976236C (en) * | 1941-12-22 | 1963-05-16 | Phillips Petroleum Co | Process and device for the production of carbon black |
US2420999A (en) * | 1942-08-11 | 1947-05-27 | Phillips Petroleum Co | Apparatus for the manufacture of amorphous carbon |
US2638745A (en) * | 1943-04-01 | 1953-05-19 | Power Jets Res & Dev Ltd | Gas turbine combustor having tangential air inlets for primary and secondary air |
US2473347A (en) * | 1943-04-08 | 1949-06-14 | Cleaver Brooks Co | Air directing means in gun type burners |
US2578051A (en) * | 1943-07-03 | 1951-12-11 | Goetaverken Ab | Solid fuel furnace |
US2464791A (en) * | 1943-11-05 | 1949-03-22 | Claude A Bonvillian | Apparatus for the combustion of fuel |
US2594312A (en) * | 1944-08-31 | 1952-04-29 | Babcock & Wilcox Co | Fuel burning apparatus |
US2468415A (en) * | 1945-08-17 | 1949-04-26 | Daniel E Stair | Method of and apparatus for burning coal |
US2573910A (en) * | 1945-08-21 | 1951-11-06 | Comb Eng Superheater Inc | Method for burning pulverized coal |
US2512196A (en) * | 1946-05-15 | 1950-06-20 | Comb Eng Superheater Inc | Air vane for fuel burners |
US2625791A (en) * | 1946-08-17 | 1953-01-20 | Bituminous Coal Research | Coal pulverization and combustion apparatus for gas turbine power plants |
US2485207A (en) * | 1946-09-06 | 1949-10-18 | Gilbert & Barker Mfg Co | Air control for tubular combustion chambers of oil burners |
US2469272A (en) * | 1946-09-06 | 1949-05-03 | Gilbert & Barker Mfg Co | Pressure atomizing oil burner |
US2616256A (en) * | 1946-09-16 | 1952-11-04 | Babcock & Wilcox Co | Gas turbine plant using solid ash-containing fuel |
US2476507A (en) * | 1946-10-30 | 1949-07-19 | Benjamin J Parmele | Cyclone burner |
US2488911A (en) * | 1946-11-09 | 1949-11-22 | Surface Combustion Corp | Combustion apparatus for use with turbines |
US2539165A (en) * | 1946-11-30 | 1951-01-23 | Cyclotherm Corp | Dispersible fuel burner having a reverse gas flow flame stabilizer |
US2627719A (en) * | 1947-06-13 | 1953-02-10 | Edward A Stalker | Gas turbine combustion chamber having controlled laminar flow of air for combustion and insulation |
US2659201A (en) * | 1947-11-26 | 1953-11-17 | Phillips Petroleum Co | Gas turbine combustion chamber with provision for turbulent mixing of air and fuel |
US2603949A (en) * | 1947-11-28 | 1952-07-22 | United Aircraft Corp | Combustion chamber with diverse air paths and vortices producing vanes therein for jet propulsion or gas turbine power plants |
US2680951A (en) * | 1948-01-02 | 1954-06-15 | Power Jets Res & Dev Ltd | Combustion apparatus for burning particles of solid or heavy liquid fuel in a fast moving stream |
US2692479A (en) * | 1948-04-09 | 1954-10-26 | Power Jets Res & Dev Ltd | Combustion apparatus for gas turbine plants using slow-burning fuel |
US2516063A (en) * | 1948-08-19 | 1950-07-18 | Gilbert & Barker Mfg Co | Pressure atomizing oil burner with a built-in combustion chamber |
US2635564A (en) * | 1948-09-15 | 1953-04-21 | Power Jets Res & Dev Ltd | Combustion system for pulverulent fuel |
US2656254A (en) * | 1948-12-11 | 1953-10-20 | Columbian Carbon | Carbon black |
US2560074A (en) * | 1948-12-21 | 1951-07-10 | Lummus Co | Method and apparatus for burning fuel |
US2572829A (en) * | 1948-12-28 | 1951-10-30 | Phillips Petroleum Co | Coal gasification process and apparatus |
US2590660A (en) * | 1949-03-02 | 1952-03-25 | United Carbon Company Inc | Apparatus for the manufacture of carbon black |
US2664402A (en) * | 1949-03-29 | 1953-12-29 | Phillips Petroleum Co | Protection of refractories in a reaction system from high temperatures by blanketing gases |
US2698050A (en) * | 1949-06-10 | 1954-12-28 | Lummus Co | Combustion for liquid fuels |
US2560076A (en) * | 1949-06-14 | 1951-07-10 | Lummus Co | Method and apparatus for burning fuel |
US2678615A (en) * | 1949-12-20 | 1954-05-18 | Rosenblad Corp | Method for burning sticky, watercontaining liquid fuel |
US2828608A (en) * | 1950-11-17 | 1958-04-01 | Power Jets Res & Dev Ltd | Improved construction of combustion chamber of the cyclone or vortex type |
US2689605A (en) * | 1950-11-29 | 1954-09-21 | Selas Corp Of America | Furnace structure |
US2703275A (en) * | 1951-01-08 | 1955-03-01 | Martin A Elliott | Apparatus for conducting heterogeneous chemical reactions |
US2865820A (en) * | 1951-04-18 | 1958-12-23 | Koppers Co Inc | Method for heat treatment of finely divided solid media |
US2800092A (en) * | 1951-06-13 | 1957-07-23 | Pollopas Patents Ltd | Burning of pulverized fuel |
US2738776A (en) * | 1951-06-13 | 1956-03-20 | Pollopas Patents Ltd | Furnace burners |
US2777407A (en) * | 1951-10-02 | 1957-01-15 | Babcock & Wilcox Co | Fuel burning apparatus |
US2769411A (en) * | 1951-11-06 | 1956-11-06 | Rosenblad Corp | Fuel combustion process and apparatus |
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