US399569A - sghiltz - Google Patents
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- US399569A US399569A US399569DA US399569A US 399569 A US399569 A US 399569A US 399569D A US399569D A US 399569DA US 399569 A US399569 A US 399569A
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- Prior art keywords
- petroleum
- canal
- chamber
- engine
- evaporating
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- 239000003208 petroleum Substances 0.000 description 43
- 239000000203 mixture Substances 0.000 description 17
- 238000001704 evaporation Methods 0.000 description 13
- 239000000446 fuel Substances 0.000 description 12
- 239000007788 liquid Substances 0.000 description 11
- 238000002485 combustion reaction Methods 0.000 description 10
- 239000003921 oil Substances 0.000 description 9
- 238000005192 partition Methods 0.000 description 7
- 238000004891 communication Methods 0.000 description 5
- 238000004880 explosion Methods 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000003034 coal gas Substances 0.000 description 3
- 238000009833 condensation Methods 0.000 description 3
- 230000005494 condensation Effects 0.000 description 3
- 230000008020 evaporation Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 239000003595 mist Substances 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000002480 mineral oil Substances 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 239000000341 volatile oil Substances 0.000 description 2
- 101100389815 Caenorhabditis elegans eva-1 gene Proteins 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 241000005139 Lycium andersonii Species 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910021538 borax Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000000110 cooling liquid Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000010685 fatty oil Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000013528 metallic particle Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000011780 sodium chloride Substances 0.000 description 1
- 239000004328 sodium tetraborate Substances 0.000 description 1
- 235000010339 sodium tetraborate Nutrition 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/14—Engines characterised by precombustion chambers with compression ignition
Definitions
- PETROLEUM ENGINE PETROLEUM ENGINE.
- My invention relates to the means of producing' a good intlannnable mixture of petroleum-vapor and air for petroleuni-motors.
- the scientific base of my invention is the tact that petroleum,which has almost the saine chemical composition as coal-gas (Cnll'pi-t) and (litters trom the same only by its physica-l properties, may be employed as a source of motive power exactly like coal-gas it' the petroleum is tirst converted into a vapor or tine spray by the combined action ot' mechanical means and heat and mixed with air in the required proportion.
- 'lhe invention has, therefore, for its object to evapora-te or iinely disperse the petroleum, to mix it with the required quantity of air, to prevent its condensation-in short, to form and maintain a good combustible petroleum mixture.
- the combustion-chamber need only have a temperature of 100O eeiiitigrade but for using illu minatiilg-petroleum, of which from twenty to twcntytive per cent. remain unevaporated at 800o cent-igrade, the temperature of the combustion-chamber mustbe much higher than 1000.
- ot cooling the combuStien-chamber which has hitherto been usual in gas and petroleum engines it should be heated, but for the workingcylinder a suitable cooling ⁇ is indispensable.
- lt is also necessary to prevent the excessive heating of the combustion-chamber, which may be done by a jacket containing water under pressure, or a saline solution, or petroleum having a boiling-point above 100C Celsius.
- the vapors formed t'rom this water may be used for injection behind the working-11iiston, and the vapors oi' petroleum are conducted into the evaporating canal, hereinafter described.
- the strong heating of the coinbustion-chamber and of the auxiliary appliances is employed not only to prevent the condensation of petroleum vapor, but also for the rapid evaporation of the petroleum and for mixing it uniformly with atmospheric air.
- the evapora-tion is effected by causing the petroleum to passinto an evapora-ti11g-canal heated bythe heat of the explosion-chamber, the supply of petroleum being accurately measured for each stroke and regulated by a governor.
- the petroleum is rst rapidly dispersed by a strong air-current produced by the engine, after which itis evaporated as completely as possible, and at the same time mixed with the heated air, and the mixture thus obtained is driven into the combustion-chamber of the engine, where it is to be exploded to drive the working-piston forward.
- the m etallic can als or receptacles for evaporating the petroleum must be hermetically closed against the combustion or explosion chamber, and mustVJ be so constructed as to rapidly absorb heat from the products of combustion, and must have a large internal surface for rapidly transmitting the heat to the petroleum and air contained in the said vessels.
- the evaporating canal or vessels may either be situated in the interior of the combustionchamber, as will be illustrated hereinafter, or
- the evaporating-vessel situated in the interior of the combustion-chamber absorbs heat directly from the gases of combustion with its whole outer surface, and may become much hotter than the walls of the combustion-chamber; but the evaporatng-canal, which surrounds the combustion-chamber, is heated on one side only through the walls of the explosion-chamber, and its temperature cannot, therefore, exceed that of the walls of the combustion-chamber. It is advantageous, but not necessary, that the walls of the external evaporating-canal should form one cast ing with the explosion-chamber of the engine.
- the partitions of the external evaporatingcanal may also be made separately of iron, copper, or a suitable alloy, and the necessary metallic connection for the transmission of heat from the combustion-chamber may be obtained by casting-that is to say, by placing the said partitions in the mold in which the combustion-Chamber is to be cast, the borders of the said partitions having been previously coated with tin or cleaned with borax.
- Figure l represents a vertical section of an engine h( ving an explosion-chamber provided with an internal and an external evaporatingcanal, the shape and size of which may be varied, as described above.
- This 'ligure shows the working-piston P sucking in a combustible mixture from the outer opening, e', through the internal helical canal, N, coiled outer jacket-canal, V, and the slide-valve S into the combustion-chamber@ of the engine, where it is compressed by the piston and ignited by an outer flame through aperture Z in the ordinary manner.
- the petroleum runs from the vessel F into the small petroleumpump p, which supplies measured quantities to the funnel-opening e, mentioned above.
- a is the discharge-valve, worked by means of a pair of rods, a a2, a balance-lever, a3, a cam, E, and a spring, g, from the spur-wheell D, which serves as a crank-disk for the connecting-rod d of the distribution slide-valve S.
- b is a lever which actuates the piston-rod c of the oil-pump p, and which may be worked from the rod c, or by other convenient means.
- the spur-wheel D is driven by a Wheel, E', mounted on crank-shaft F.
- Fig. 2 shows another shape of the internal evaporating canal or vessel, N, into which the oil is introduced by a thin pipe, n.
- the oil and air pass rst through the zigzag-shaped inner canal, N, and then' .through the helical outer evaporating-canal, V.
- R is a waterjacket for the combustion-chamber C, as mentioned above.
- Fig. is a horizontal section of a combustion-chamber with inner and outer evaporatingcanal, the former being circular and the latter zigzag-shaped.
- the course of the air with petroleum is indicated by arrows.
- the oil and air may of course be conducted iirst through the inner and then through the outer canal, as illustrated, or vice versa, or a IOO portion of the canal may be employed to heat the air or the petroleum separately before the two are brought together.
- Figs. 4 and 5 show a helical orcoiled jacketcanal, V.
- the arrows indicate the directio of the air-current.
- Fig. 6 is a horizontal section of the coolingreservoir R, iilled with saline water, petroleum, or other convenient cooling-liquid, as mentioned above.
- Fig. 7 is a horizontal and Fig. -S a vertical section, showing a vertical zigzag canal, V, which is open alternately above and below.
- Each evaporating-canal is hermetically separated from the explosion-chamber.
- the inlet is outside of the jacket in order to conduct air and petroleum through the canal, which serves as an evaporating and mixing space.
- Fig. 9 is a partial vertical section showing how the slide-valve S of Fig. l may be replaced by an admission-valve, m, an exhaustvalve, n, and igniting apparatus w.
- the described evaporating-canals must be of such a width that the air driven or sucked through them at every stroke or cycle of the engine and heated thereby, will rapidly disperse the petroleum simultaneously supplied to the canal, the oil being thus spread over the metallic walls and evaporated almost sud- IIO denly, (as much as is capable of evaporation,) thus forming with air a combustible mixture, which is then conveyed from the jacket into the explosion-chamber, as described above.
- the trials with my engine have also shown that ignition takes place much more easily if the explosive mixture contains a small quantity of illuminating-gas or of volatile liquid fuel, and that crude pet-roleum may be used more easily than illuminating petroleum, no doubt on account of its admixture of volatile oils. Consequently, in order to utilize heavy mineral oils as a fuel forpetrole'u11i-engines, they may be diluted with volatile oils, and a combination of the internal with the external evaporating apparatus employed, as illustrated by Fig. l.
- cylinder may suck a mixture of air and petroleum through the evaporating-canal, then compress the mixture on the return-stroke, after which it is ignited and exploded, and the products of combustion are expelled on the fourth stroke.
- l. ln a hydrocarbonengine, a metallic evaporating-j aeket surro un di n g the explosionchamber of the engine and subdivided by transverse partitions, so as to increase the inner surface, substantially as described, and for the purpose specified.
- the combination of the explosion-chamber with (a) an evaporating-jacket separated from the eX- plosion-chamber by a metallic Wall only, and subdivided by transverse partitions, so as to form a helical or zigzag canal surrounding the explosion-chamber, said canal being provided With a valve adapted to produce and interrupt communication with the explosion-cham ber at every cycle of the engine, (b) an oil feederor pump adapted to introduce into the said evaporating-canal small exactly-measured quantities of liquid fuel at every cycle of the engine, and (c) a pump, preferably the Working-cylinder, 'for producing in the said canal at every cycle of the engine an airblast into or toward the explosion-chamber, substantially as described.
- the combination of the explosion chamber with (d) a metallic evaporating-canal separated from the explosion-space by asingle Wall, the said canal being partly formed by a helical or zigzag passage surrounding the explosion-chamber and partly situated in the interior of the latter, and furnished With a valve adapted to produce and interrupt communication with the explosion-chamber at every cycle of the engine, (b) an oil feeder or pump adapted to introduce into the said evaporating-canal small exactly-measured quantities of liquid fuel at every cycle of the engine, and (c) a pump, preferably the Working-cylinder, for producing in the said canal at every cycle of the engine an air-blast into or toward the explosion-chamber, substantially as described.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Description
(No Model.) 2 Sheets-Sheet l.
M. V. SGHILTZ.
PETROLEUM ENGINE.
No. 399,569. E I Mar. 12,1889.
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(No Model.)
2 Sheets-Sheet 2.. M. V. SCHILTZ. PETROLEUM ENGINE.
v910.399.569. Patented Mar. 12, 1889.
Wwf@ WW@ M m N. PETERS, Pnmmmngmpnnr. wunmgwn, n. c
limiten 8frnrns llATlllAS VITAL SCHILTZ,
Partnr Ormes.
OF COLOGNE, GERMANY.
PETROLEUM-18618! E.
SPECFICATIGN forming part of Letters Patent No. 399,569, dated March 12, 1889.
Application lled June 25, 1887. Serial No. 242,474. (No model.) Patented in Germany :111116 16, 1885, No. 86,044, and Anril 10, 1886, No. 38,121; in'l'anee August 121885,11@ 170,620,a11d July 3, 1886, No. 177,181; in Belgium August; 12, 1885, No. 69,892, and June 80, 1888,110. 78,679; in England October 27, 1885, No. 12,896, and August 16, 1886,110. 10,480; in Austria- Hungary November 10, 1885,11()l 30,859, and October 23, 1886, 110.1%),835, and in Italy February 4,1886, No. 19,209, and
May 10, 1887, No. 20,715.
T0 all whom t nto/y concern;
Be it known that I, Mari-nas VITAL SCHILTZ, a subject of the Emperor o1 Germany, residing at Cologne, in the German Empire, have invented certain new and useful Improvements in VPetroleum-Eiigines, (tor which 1 have received Letters Patent in Germany, No. 80,044, dated June l0, 1885, and No. 3t,121 dated April 10,1880, in Great Britain, No 12,800, dated October 27, 1885, and No. 10,180, dated August 10, 1880; in France, No. 170,020, dated August 12, 1885, and No. 177,181, dated July 3, 1880; in Belgium, No. 00,802, dated August 12, 1885, and No. 78,070, dated .lune 30, 1880; in Austria- Hungary, No. 30,2300, dated November 10, 1885, and No. 10,8235, dated October 28, 1880, and in Italy, No. 10,200, dated February 4, 1880, and No. 20,715, dated lllay 10, 1887;) and l do hereby declare that the following a full, clear, and exact description of the invention, which will enable others skilled in the art to which it appertains to make and use the same.
My invention relates to the means of producing' a good intlannnable mixture of petroleum-vapor and air for petroleuni-motors.
The scientific base of my invention is the tact that petroleum,which has almost the saine chemical composition as coal-gas (Cnll'pi-t) and (litters trom the same only by its physica-l properties, may be employed as a source of motive power exactly like coal-gas it' the petroleum is tirst converted into a vapor or tine spray by the combined action ot' mechanical means and heat and mixed with air in the required proportion.
'lhe invention has, therefore, for its object to evapora-te or iinely disperse the petroleum, to mix it with the required quantity of air, to prevent its condensation-in short, to form and maintain a good combustible petroleum mixture.
Scientific .reseztrchesv with coal-gas have also shown that tor a good .ignition and combustion ot the mixture the gas and air must be mixed in certain delinite proportions. The same is the case with petroleum; but l'or maintaining a goed petroleum mixture it :is not only aecessary to supply petroleum-vapor and air in certain proportions, but also to prevent the condensation ot' petroleu11i-vapors by maintaining a certain temperature. lf a good petroleum mixture is suilieiently cooled to condense a portion of the gaseous petroleum in the shape of mist, the mixture is no longer easily inflammable and combustible, while on the other hand a weak mixture containingliquid particles may be rendered more in tiaminable bythe application ot heat. Consequently it is essential to maintain a certain temperature suiiiciently high to prevent condensation in all spaces and canals through which the petroleum mixture passes before its combustion. This temperature must be the higher the heavier the petroleum which is to be used as the source of power. For light petroleum the combustion-chamber need only have a temperature of 100O eeiiitigrade but for using illu minatiilg-petroleum, of which from twenty to twcntytive per cent. remain unevaporated at 800o cent-igrade, the temperature of the combustion-chamber mustbe much higher than 1000.
Instead ot cooling the combuStien-chamber, which has hitherto been usual in gas and petroleum engines it should be heated, but for the workingcylinder a suitable cooling` is indispensable. lt is also necessary to prevent the excessive heating of the combustion-chamber, which may be done by a jacket containing water under pressure, or a saline solution, or petroleum having a boiling-point above 100C Celsius. The vapors formed t'rom this water may be used for injection behind the working-11iiston, and the vapors oi' petroleum are conducted into the evaporating canal, hereinafter described. The strong heating of the coinbustion-chamber and of the auxiliary appliances is employed not only to prevent the condensation of petroleum vapor, but also for the rapid evaporation of the petroleum and for mixing it uniformly with atmospheric air.
As will be described later in detail, the evapora-tion is effected by causing the petroleum to passinto an evapora-ti11g-canal heated bythe heat of the explosion-chamber, the supply of petroleum being accurately measured for each stroke and regulated by a governor. In the evaporating-canal the petroleum is rst rapidly dispersed by a strong air-current produced by the engine, after which itis evaporated as completely as possible, and at the same time mixed with the heated air, and the mixture thus obtained is driven into the combustion-chamber of the engine, where it is to be exploded to drive the working-piston forward.
The m etallic can als or receptacles for evaporating the petroleum must be hermetically closed against the combustion or explosion chamber, and mustVJ be so constructed as to rapidly absorb heat from the products of combustion, and must have a large internal surface for rapidly transmitting the heat to the petroleum and air contained in the said vessels.
The evaporating canal or vessels may either be situated in the interior of the combustionchamber, as will be illustrated hereinafter, or
they may surround the combustion-chamberl like a jacket, and form around the same a ringshaped, helical, or zigzag canal of a width depending on the required speed of the air-current. In both cases the evaporatingcanal is separated from the combustion-space by a metallic partition only. For veryheavy mineral oils these two methods of evaporation-that is to say, an inner and an outer evaporating-canal-may be combined in the same engine, as will be described hereinafter in detail.
The evaporating-vessel situated in the interior of the combustion-chamber absorbs heat directly from the gases of combustion with its whole outer surface, and may become much hotter than the walls of the combustion-chamber; but the evaporatng-canal, which surrounds the combustion-chamber, is heated on one side only through the walls of the explosion-chamber, and its temperature cannot, therefore, exceed that of the walls of the combustion-chamber. It is advantageous, but not necessary, that the walls of the external evaporating-canal should form one cast ing with the explosion-chamber of the engine. The partitions of the external evaporatingcanal may also be made separately of iron, copper, or a suitable alloy, and the necessary metallic connection for the transmission of heat from the combustion-chamber may be obtained by casting-that is to say, by placing the said partitions in the mold in which the combustion-Chamber is to be cast, the borders of the said partitions having been previously coated with tin or cleaned with borax.
In the accompanying drawings, Figure l represents a vertical section of an engine h( ving an explosion-chamber provided with an internal and an external evaporatingcanal, the shape and size of which may be varied, as described above. This 'ligure shows the working-piston P sucking in a combustible mixture from the outer opening, e', through the internal helical canal, N, coiled outer jacket-canal, V, and the slide-valve S into the combustion-chamber@ of the engine, where it is compressed by the piston and ignited by an outer flame through aperture Z in the ordinary manner. The petroleum runs from the vessel F into the small petroleumpump p, which supplies measured quantities to the funnel-opening e, mentioned above. a is the discharge-valve, worked by means of a pair of rods, a a2, a balance-lever, a3, a cam, E, and a spring, g, from the spur-wheell D, which serves as a crank-disk for the connecting-rod d of the distribution slide-valve S. b is a lever which actuates the piston-rod c of the oil-pump p, and which may be worked from the rod c, or by other convenient means. The spur-wheel D is driven by a Wheel, E', mounted on crank-shaft F.
Fig. 2 shows another shape of the internal evaporating canal or vessel, N, into which the oil is introduced by a thin pipe, n. The oil and air pass rst through the zigzag-shaped inner canal, N, and then' .through the helical outer evaporating-canal, V. R is a waterjacket for the combustion-chamber C, as mentioned above.
Fig. is a horizontal section of a combustion-chamber with inner and outer evaporatingcanal, the former being circular and the latter zigzag-shaped. The course of the air with petroleum is indicated by arrows. The oil and air may of course be conducted iirst through the inner and then through the outer canal, as illustrated, or vice versa, or a IOO portion of the canal may be employed to heat the air or the petroleum separately before the two are brought together.
Figs. 4 and 5 show a helical orcoiled jacketcanal, V. The arrows indicate the directio of the air-current.
Fig. 6 is a horizontal section of the coolingreservoir R, iilled with saline water, petroleum, or other convenient cooling-liquid, as mentioned above.
Fig. 7 is a horizontal and Fig. -S a vertical section, showing a vertical zigzag canal, V, which is open alternately above and below. Each evaporating-canal is hermetically separated from the explosion-chamber. The inlet is outside of the jacket in order to conduct air and petroleum through the canal, which serves as an evaporating and mixing space. These arrangements may be varied according to requirements.
Fig. 9 is a partial vertical section showing how the slide-valve S of Fig. l may be replaced by an admission-valve, m, an exhaustvalve, n, and igniting apparatus w.
The described evaporating-canals must be of such a width that the air driven or sucked through them at every stroke or cycle of the engine and heated thereby, will rapidly disperse the petroleum simultaneously supplied to the canal, the oil being thus spread over the metallic walls and evaporated almost sud- IIO denly, (as much as is capable of evaporation,) thus forming with air a combustible mixture, which is then conveyed from the jacket into the explosion-chamber, as described above.
In the lowest passages of the described evaporating-canals sm all particles of metalsas, for instance, iron shavings-niay be placed in order to favor the dispersion of petroleum.
An experiment with the described apparatus in the winter has shown that without the slightest heating ordinary illuminatingpetroleum of 0.81 specific gravity has been converted into a very fine mist without any residue, and it is evident, thereii'ore, that the particles of such a mist may be further divided or evaporated under the iniiucnee of heat and an air-current.
As the trials made by applying this apparatus to the engine have demonstrated that any kind of' liquid fuel-such as crude petroleum, illumina-ting-petrolcum, fatty oils, even" tar and parafiine-may bc equally well dispersed or evaj'lorated, provided that the said fuel is diluted with a more volatile liquid fuel, the use of cheap oils has been facilitated by the described appliances as soon as a good ignition is secured by an external flame. The trials with my engine have also shown that ignition takes place much more easily if the explosive mixture contains a small quantity of illuminating-gas or of volatile liquid fuel, and that crude pet-roleum may be used more easily than illuminating petroleum, no doubt on account of its admixture of volatile oils. Consequently, in order to utilize heavy mineral oils as a fuel forpetrole'u11i-engines, they may be diluted with volatile oils, and a combination of the internal with the external evaporating apparatus employed, as illustrated by Fig. l.
lf a mixture containing finely-divided but unevaporated petroleum is burned in a closed space, this combustion is less explosive than the combustion of purely gaseous fuel. This retarded combustion probably takes place in such a manner that the hydrogen of the gaseous fuel in the whole space burns earlier than the carbon and that the latter produces a sort of delayed combustion, the developed heat serving first for evaporating or destroying' the rest of the fuel. and sulilsequentl y for i gnitin g the same.
For the use of the described eva1' oiati11g appliances it is innnaterial whether the air and petroleum are conducted. through the canal by suction or by pressure. For an engine provided with a working and a pumping cylinder the best way is to cause the pump to suck pure air, and compress and force the same through the evaporatin g-can al (into which the petroleum is forced by a small pump) into the explosion-chamber of the engine. ln this case the air-pump need not be heated, because it does not contain any combustible mixture.
In an engine havin a single cylinder which serves alternately as a power-cylinder and as a pump-cylinder, as illustrated by Fig. l,this
cylinder may suck a mixture of air and petroleum through the evaporating-canal, then compress the mixture on the return-stroke, after which it is ignited and exploded, and the products of combustion are expelled on the fourth stroke.
For the regular working of the engine accumulation of liquid petroleum in the evaporating-eanal must be avoided, for this would cause variations in the quantity of petroleumvapors. Any petroleum which is not evaporated must be finely distributed by the sharp current of Aheated air and the metallic particles. The petroleum which has run to the bottom is sucked up again by the thin pipe i, Fig. -l, and the regularity of speed of the engine is then preserved by uniformly measuring oli' the quantity of petroleum necessary for cach stroke. This exact measurement might be effected by an automatically-goveriied valve or by a cock with a long plug which can be advanced axially more or less against its seat; but as the vibrations or shaking of the engine, the variations in the consistency orviscosity of the liquid, and changes of temperature would vary the quantity of liquid passing through the valve-opening at a constant position of the same, I prefer to measure and propel the liquid fuel bya small pump driven by the' engine, the said pump having a variable stroke and automatic valves of known construction. The regulation is then effected'by setting the pump out of ac tion when the engine runs too fast. These contrivances are only mentioned to render the explanation of my invention more easily intelligible; but they are not described in detail, because they do not present any novelty in themselves.
In my German patents, Nos. 25,036 and 26,621, l have described how the petroleum may be evapora-ted by means of open metallic cups placed in the combristicii-chamber, the said cups absorbing sufficient heat at the time of the explosion for rapidly evapora-ting the quantity of petroleum necessary for the subsequent explosion.
W'hat l claim as my invention, and wish to secure by Letters Patent, is-
l. ln a hydrocarbonengine, a metallic evaporating-j aeket surro un di n g the explosionchamber of the engine and subdivided by transverse partitions, so as to increase the inner surface, substantially as described, and for the purpose specified.
2. In a liydrocarbon-engine, the combination of the explosion-chamber with a metallic evaporating-jacket separated from the explosion-chamber by a single wall, and therefore directly heated by the explosions, the said jacket being subdivided by transverse partitions, so as to increase the inner evaporating-surface of the jacket and to lengthen in this way the evaporating-canal, the said evaporating canal being furnished with a valve adapted to produce and interrupt communication with the explosion-cllamber at IOO IIO
ing furnished with a valve adapted to pro-` duce and interrupt communication with the explosion-chamber at every cycle of the engine, (b) an oil feeder or pump adapted to introduce into the said evaporating-canal small exactly-measured quantities of liquid fuel at' every cycle of the engine, and (c) a pump, preferably the Working-cylinder, adapted to produce in the said canal at every cycle of the engine a sharp air-current into or toward the explosion-cli amber of the engine, substantially as described.
L In a hydrocarbon-engine, the combination of the explosion-chamber with (a) an evaporating-jacket separated from the eX- plosion-chamber by a metallic Wall only, and subdivided by transverse partitions, so as to form a helical or zigzag canal surrounding the explosion-chamber, said canal being provided With a valve adapted to produce and interrupt communication with the explosion-cham ber at every cycle of the engine, (b) an oil feederor pump adapted to introduce into the said evaporating-canal small exactly-measured quantities of liquid fuel at every cycle of the engine, and (c) a pump, preferably the Working-cylinder, 'for producing in the said canal at every cycle of the engine an airblast into or toward the explosion-chamber, substantially as described.
5. In a hydrocabonfengine, the combination of the explosion-chamber With (d) a helical 0r zigzag shaped evaporating-canal surrounding the explosion-chamber and cast in one piece With the same, said canal being furnished with a valve adapted to establish and interrupt communication With the explosionchamber at every cycle of the engine, (b) an oil feeder or pump adapted to introduce into the said evaporating canal small exactlymeasured quantities of liquid fuel at every cycle of the engine, and a pump, preferably the Working-cylinder, for producing in the said canal at every cycle of the engine an airblast into or toward the explosion-chamber, substantially as described.
G. In a hydrocarbon-engine, the combination of the explosion chamber with (d) a metallic evaporating-canal separated from the explosion-space by asingle Wall, the said canal being partly formed by a helical or zigzag passage surrounding the explosion-chamber and partly situated in the interior of the latter, and furnished With a valve adapted to produce and interrupt communication with the explosion-chamber at every cycle of the engine, (b) an oil feeder or pump adapted to introduce into the said evaporating-canal small exactly-measured quantities of liquid fuel at every cycle of the engine, and (c) a pump, preferably the Working-cylinder, for producing in the said canal at every cycle of the engine an air-blast into or toward the explosion-chamber, substantially as described.
In 'testimony whereof I have signed this specification in the presence of two subscribing Witnesses.
MATHIAS VITAL SCHILTZ.
Nitin esses:
EDUARD QUEICK, FRANZ WERTENBUCH.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US399569A true US399569A (en) | 1889-03-12 |
Family
ID=2468531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US399569D Expired - Lifetime US399569A (en) | sghiltz |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US399569A (en) |
-
0
- US US399569D patent/US399569A/en not_active Expired - Lifetime
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