US798855A - Combustion-chamber. - Google Patents
Combustion-chamber. Download PDFInfo
- Publication number
- US798855A US798855A US7804201A US1901078042A US798855A US 798855 A US798855 A US 798855A US 7804201 A US7804201 A US 7804201A US 1901078042 A US1901078042 A US 1901078042A US 798855 A US798855 A US 798855A
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- US
- United States
- Prior art keywords
- chamber
- combustion
- air
- inner chamber
- jacket
- 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
- 238000002485 combustion reaction Methods 0.000 description 18
- 239000007789 gas Substances 0.000 description 9
- 239000012530 fluid Substances 0.000 description 7
- 239000000446 fuel Substances 0.000 description 6
- 239000002184 metal Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 241000005139 Lycium andersonii Species 0.000 description 1
- 241000488982 Monotropa uniflora Species 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000000266 injurious effect Effects 0.000 description 1
- 239000000320 mechanical mixture Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 239000000341 volatile oil Substances 0.000 description 1
- 238000010792 warming Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
Definitions
- This invention relates generally to internal-combustion engines, and particularly to the combustion-chamber for producing the working fluid Yfor internal-combustion engines; and it has 'for its object to provide a combustion-chaniber separated or removed from the working chamber and Vfrom the compression-chamber, but connected to said chambers, in which the working fluid is produced ready Yfor use, so that it may be conducted to the engine in a nlanner similar to the delivery Of steam from a boiler to an engine, thus insuring perfect combustion and avoiding the injurious eflect of combined heat and pressure acting upon the metal; and it consists of the parts and combinations of parts hereinafter described and claimed.
- Figure l is a longitudinal vertical section through my improved combustion-chamber; Fig. 9., a transverse vertical section on the line Q 2, Fig. l; and Figs. and -l sectional views of modified forms of one part of the invention.
- l employ air compressors and reservoirs for the compressed air which are water-jacketcdg butl entirely avoid the use of such jackets on the engine and the combustion-chamber, the compressed air, partly cooled, being' conducted directly to the combustion-chamber and serving to reduce the temperature of the products of combustion as well as to take up the heat radiated from said chamber and which is now usually taken up by a water-jacket and goes to waste, whereas l utilize said heat by converting it into work.
- the combustion-chamber proper comprises an inner chamber A and an outer chamber B, the former being closed at one end and in cominunication with the outer chamber at its other end, while the outer chamber is closed at both ends and surrounds and extends beyond the inner chamber at each end, as clearly shown.
- Any suitable means may be employed to support the inner chambercentrally within the outer chamber, so as to provide a space between said chambers at all points, and l show as a convenient means for so supporting the inner chamber a series of webs extending' from said inner chamber and resting against the inner surface of said outer chamber.
- a block or plug U having a passage centrally therethrough which at both ends is formed fiaring, as at c c', Fig. l, the mouth c being of the greatest diameter, so as to cause the fluids to be sprayed and mingled in theinner chamber as they issue from the passage.
- the inner and outer chambers are preferably cylindrical in shape, and the inner chamber is preferably made in two parts and joined by a coupling' (l.
- the outer chamber Bis closed at one end by the head a, bolted in place, while the other end is preferably closed by a head cast therewith.
- a jacket l Surrounding and inclosing the chambers A and B is a jacket l), which support-s the shell of chamber B centrally in said jacket by the webs j, projecting lfrom said shell.
- One end of the jacket D is closed by a head y, securely bolted to a flange on the jacket, and the other end is preferably formed dome-shaped, so as to provide a somewhat enlarged chamber or space /1 at the end of chamber B, with which space said chamber B has communication through a series of openings r', foi'med in the end wall of said chamber B.
- l( represents a pipe through which airis fed to the interior of jacket D.
- the diameter of the jacket is such that a space y' is provided at all points surrounllling the chamber B, and which space has direct communication with the space /t at the end of the chamber B.
- E represents a pipe which leads from an air-compressor (not shown) through the head f/ of the jacket and head e of chamber B and IOO extends back and forth in the space between the chambers A and 'B the full length oi' the inner chamber, said coil thus formed terminating in the closed end of said chamber A at 5, so as to discharge within said chamber the supply of air necessary to support combustion.
- F represents a fluid-fuel pipe lead ing th rough the heads f/ and c and entering the inner chamber A in front of the block C and terminating in a nozzle Z, which discharges into the flaring mouth of the opening in said block.
- G represents the wires of any suitable electrical sparking device H, arranged within the inner chamber in advance of the block C to ignite the mixture.
- a block of refractory material I is secured to the end wall of chamber H in line with the inner chamber to protect the said end wall from the direct action of the hot gases.
- J represents a pipe through which the products of combustion or hot gases are conducted to the cylinder of an engine or elsewhere, as desired for use.
- air which has been compressed and cooled as nearly simultaneously as possible at a point removed from the combustionchamber enters the pipe E under pressure and circulates through the coil to be heated by the gases in the outer chamber B before entering' the inner chamber and thus aid combustion.
- the fluid fuel is fed through pipe F under pressure and is discharged through the nozzle l into the flaring-mouthed passage of block C and is sprayed into inner chamber A.
- the heated air from the coil enters the inner chamber at /a and passes through the passage in block C and is mixed or mingled with oil spray and ignited by the sparker H, and the products of combustion pass out of said inner chamber and into chamber B and from the latter to the engine through pipe J.
- the air-jacket D receives the cooled compressed air through pipe K, and it circulates in the space surrounding the outer chamber B and takes up the heat radiated from said chamber B and cond ucts it through the space j' to the chamber or space L, from which it escapes into the said chamber B through the opening z', where it is converted into work.
- Fig. 3 I show a chamber M at the end of the outer cylinder into which cooled compressed air enters through a pipe O and escapes into the said chamber in order to reduce the temperature ot' the'hot gases, and in Fig. 4; I show pipes N, which are intended to convey cooled air directly to the said chamber B without the intervention of a chamber M or space t.
- the theory ot' this invention is to divide the combustion-chamber into two or more separate zones of equal heat,the inner chamber being intended to receive the air (after it has been warmed by circulation in the outer chamber) and the Huid fuel in the form of a spray.
- the inner chamber being intended to receive the air (after it has been warmed by circulation in the outer chamber) and the Huid fuel in the form of a spray.
- the cool compressed air entering the jacket and liowing over the surface of the outer chamber takes up a large part of the heat which Vthe outer chamber would otherwise lose by radiation and carries it back to the outer chamber, where it mingles with the hot gas and, forming with it a mechanical mixture of such temperature as the metal oi' the cylinder can stand, goes to the working chamber to give up its heat in the form of work.
- the coil of pipe is merely one way for exposing the incoming air which is to be used to support combustion to a higher temperature in order by the aid oi' warming vthe air to make combustion ot' the less volatile oils more certain.
- the aim of this invention is to provide-a combustion-chamber capable of control and manipulation, it being designed to have no limit to the temperature of combustion and to reduce this maximum temperature to any desired degree ot' temperature by mingling cooler compressed air with the products of combustion. In this way the advantages of the extreme temperature as an aid to combustion and of a more moderate temperature for use can be obtained.
- a Combustion -chziniber Comprising an i with said outer chamber, and an exhaust or deinner und an outer chamber, an air-pipe livery p ipeleading from said onterehzunber. IO leading into the outer chamber and forming In testimony whereoil I aliiix inysignuture in a Coil about the inner chamber and terininatpresence of two witnesses. ing within the inner chamber, a Huid-fuel JOHN F. fEN'lW/VORII'I. pipe delivering within said inner chamber, a fitnessesz suitable igniter within the inner chamber, an M. L. SPELLMAN, :nrpicket surrounding ⁇ and in communication i HUGH M. STERLING.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
PATBNTBD SEPT. 5, 1905.
J. F. WENTWORTH. COMBUSTION CHAMBER.
APPLICATION FILED 00T. 9. 1901.
UNTEB? STATES Pif-Filial i. lrl" OFFOE.
COIVIBUSTION-CHAIVIBER.
Speccaton of Letters Patent.
Patented Sept. 5, 1905.
Application led October 9, 1901. Serial No. 78,042.
Be it known that I, JOHN F. \Vi-iNTwoR'rn, a citizen of the United States, residing at fashingtom in the District of Columbia, have invented certain new and useful lmprovements in Combristicii-Chambers; and l do declare the following to be a full, clear, and eXact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
This invention relates generally to internal-combustion engines, and particularly to the combustion-chamber for producing the working fluid Yfor internal-combustion engines; and it has 'for its object to provide a combustion-chaniber separated or removed from the working chamber and Vfrom the compression-chamber, but connected to said chambers, in which the working fluid is produced ready Yfor use, so that it may be conducted to the engine in a nlanner similar to the delivery Of steam from a boiler to an engine, thus insuring perfect combustion and avoiding the injurious eflect of combined heat and pressure acting upon the metal; and it consists of the parts and combinations of parts hereinafter described and claimed.
ln the accompanying drawings, forming a pai't of this specification, Figure l is a longitudinal vertical section through my improved combustion-chamber; Fig. 9., a transverse vertical section on the line Q 2, Fig. l; and Figs. and -l sectional views of modified forms of one part of the invention.
Similar letters refer to similar parts throughout the several views.
In carrying out my invention l employ air compressors and reservoirs for the compressed air which are water-jacketcdg butl entirely avoid the use of such jackets on the engine and the combustion-chamber, the compressed air, partly cooled, being' conducted directly to the combustion-chamber and serving to reduce the temperature of the products of combustion as well as to take up the heat radiated from said chamber and which is now usually taken up by a water-jacket and goes to waste, whereas l utilize said heat by converting it into work.
In the drawings I have omitted the compression apparatus and the engine as well as valves Vfor controlling the fluid fuel and air and gases, as l make no claim for any novel features in such apparatus or devices.
Referring now to the drawings, the combustion-chamber proper comprises an inner chamber A and an outer chamber B, the former being closed at one end and in cominunication with the outer chamber at its other end, while the outer chamber is closed at both ends and surrounds and extends beyond the inner chamber at each end, as clearly shown. Any suitable means may be employed to support the inner chambercentrally within the outer chamber, so as to provide a space between said chambers at all points, and l show as a convenient means for so supporting the inner chamber a series of webs extending' from said inner chamber and resting against the inner surface of said outer chamber. At a suitable distance from the closed end of the chamber A is secured, preferably by screwing the same in place, a block or plug U, having a passage centrally therethrough which at both ends is formed fiaring, as at c c', Fig. l, the mouth c being of the greatest diameter, so as to cause the fluids to be sprayed and mingled in theinner chamber as they issue from the passage. The inner and outer chambers are preferably cylindrical in shape, and the inner chamber is preferably made in two parts and joined by a coupling' (l. The outer chamber Bis closed at one end by the head a, bolted in place, while the other end is preferably closed by a head cast therewith.
Surrounding and inclosing the chambers A and B is a jacket l), which support-s the shell of chamber B centrally in said jacket by the webs j, projecting lfrom said shell. One end of the jacket D is closed by a head y, securely bolted to a flange on the jacket, and the other end is preferably formed dome-shaped, so as to provide a somewhat enlarged chamber or space /1 at the end of chamber B, with which space said chamber B has communication through a series of openings r', foi'med in the end wall of said chamber B.
l( represents a pipe through which airis fed to the interior of jacket D. The diameter of the jacket is such that a space y' is provided at all points surrounllling the chamber B, and which space has direct communication with the space /t at the end of the chamber B.
E represents a pipe which leads from an air-compressor (not shown) through the head f/ of the jacket and head e of chamber B and IOO extends back and forth in the space between the chambers A and 'B the full length oi' the inner chamber, said coil thus formed terminating in the closed end of said chamber A at 5, so as to discharge within said chamber the supply of air necessary to support combustion. Y
F represents a fluid-fuel pipe lead ing th rough the heads f/ and c and entering the inner chamber A in front of the block C and terminating in a nozzle Z, which discharges into the flaring mouth of the opening in said block.
G represents the wires of any suitable electrical sparking device H, arranged within the inner chamber in advance of the block C to ignite the mixture. A block of refractory material I is secured to the end wall of chamber H in line with the inner chamber to protect the said end wall from the direct action of the hot gases.
J represents a pipe through which the products of combustion or hot gases are conducted to the cylinder of an engine or elsewhere, as desired for use.
In operation air which has been compressed and cooled as nearly simultaneously as possible at a point removed from the combustionchamber enters the pipe E under pressure and circulates through the coil to be heated by the gases in the outer chamber B before entering' the inner chamber and thus aid combustion. The fluid fuel is fed through pipe F under pressure and is discharged through the nozzle l into the flaring-mouthed passage of block C and is sprayed into inner chamber A. The heated air from the coil enters the inner chamber at /a and passes through the passage in block C and is mixed or mingled with oil spray and ignited by the sparker H, and the products of combustion pass out of said inner chamber and into chamber B and from the latter to the engine through pipe J. The air-jacket D receives the cooled compressed air through pipe K, and it circulates in the space surrounding the outer chamber B and takes up the heat radiated from said chamber B and cond ucts it through the space j' to the chamber or space L, from which it escapes into the said chamber B through the opening z', where it is converted into work.
In Fig. 3 I show a chamber M at the end of the outer cylinder into which cooled compressed air enters through a pipe O and escapes into the said chamber in order to reduce the temperature ot' the'hot gases, and in Fig. 4; I show pipes N, which are intended to convey cooled air directly to the said chamber B without the intervention of a chamber M or space t.
The theory ot' this invention is to divide the combustion-chamber into two or more separate zones of equal heat,the inner chamber being intended to receive the air (after it has been warmed by circulation in the outer chamber) and the Huid fuel in the form of a spray. By means of this previous heating of the air and allowing' the proper proportions or' air to enter with the fuel a very intense heat is obtained within the inner chamber, which heat is high enough to accomplish the complete combustion of any combustible fluid. The temperature obtained would be about 2, OOO@ Fahrenheit, and with a pressure of five hundred pounds per square inch or even much less there is no metal which can withstand the combined stress of pressure and this high temperature. In my improved combustionchamber as the product oi' combustion or the working fluid leaves this inner chamber it meets the surplus of cooled compressed air and mingling with it forms a gas of reduced temperature. This gas having' a temperature oi' about TOOo Fahrenheit can be contained in an ordinary metal reservoir. Hence this gas surrounding and being on all sides of the inner chamber takes away the effect of the pressure, leaving theinner chamber to stand only the effect of the heat, which can be accomplished by means of asbestos or some similar lining. The air-jacket when used is to prevent loss by radiation as much as is possible. The cool compressed air entering the jacket and liowing over the surface of the outer chamber takes up a large part of the heat which Vthe outer chamber would otherwise lose by radiation and carries it back to the outer chamber, where it mingles with the hot gas and, forming with it a mechanical mixture of such temperature as the metal oi' the cylinder can stand, goes to the working chamber to give up its heat in the form of work. The coil of pipe is merely one way for exposing the incoming air which is to be used to support combustion to a higher temperature in order by the aid oi' warming vthe air to make combustion ot' the less volatile oils more certain.
The aim of this invention is to provide-a combustion-chamber capable of control and manipulation, it being designed to have no limit to the temperature of combustion and to reduce this maximum temperature to any desired degree ot' temperature by mingling cooler compressed air with the products of combustion. In this way the advantages of the extreme temperature as an aid to combustion and of a more moderate temperature for use can be obtained.
Havingl thus described my invention, what I claim as new, and desire to secure by Letters -Patent, is-
TOO
1. An inner combustion-chamber, an outer commingling-chamber for air and products of combustion and an air-jacket inclosing and communicating with said chambers, and a compressed-air supply for said jacket.
2. A Combustion -chziniber Comprising an i with said outer chamber, and an exhaust or deinner und an outer chamber, an air-pipe livery p ipeleading from said onterehzunber. IO leading into the outer chamber and forming In testimony whereoil I aliiix inysignuture in a Coil about the inner chamber and terininatpresence of two witnesses. ing within the inner chamber, a Huid-fuel JOHN F. fEN'lW/VORII'I. pipe delivering within said inner chamber, a fitnessesz suitable igniter within the inner chamber, an M. L. SPELLMAN, :nrpicket surrounding` and in communication i HUGH M. STERLING.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US7804201A US798855A (en) | 1901-10-09 | 1901-10-09 | Combustion-chamber. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US7804201A US798855A (en) | 1901-10-09 | 1901-10-09 | Combustion-chamber. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US798855A true US798855A (en) | 1905-09-05 |
Family
ID=2867343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US7804201A Expired - Lifetime US798855A (en) | 1901-10-09 | 1901-10-09 | Combustion-chamber. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US798855A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2445466A (en) * | 1944-06-02 | 1948-07-20 | Solar Aircraft Co | Fluid fuel combustion device |
| US2718116A (en) * | 1951-04-20 | 1955-09-20 | Charles J Moses | Jet engine with coaxial fuel and air intake chambers |
| US2718754A (en) * | 1951-06-30 | 1955-09-27 | Exxon Research Engineering Co | Combustion system for combustion gas turbines |
| US2799988A (en) * | 1953-06-08 | 1957-07-23 | Power Generators Ltd | Catapult device |
-
1901
- 1901-10-09 US US7804201A patent/US798855A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2445466A (en) * | 1944-06-02 | 1948-07-20 | Solar Aircraft Co | Fluid fuel combustion device |
| US2718116A (en) * | 1951-04-20 | 1955-09-20 | Charles J Moses | Jet engine with coaxial fuel and air intake chambers |
| US2718754A (en) * | 1951-06-30 | 1955-09-27 | Exxon Research Engineering Co | Combustion system for combustion gas turbines |
| US2799988A (en) * | 1953-06-08 | 1957-07-23 | Power Generators Ltd | Catapult device |
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