US1244566A - Internal-combustion engine. - Google Patents
Internal-combustion engine. Download PDFInfo
- Publication number
- US1244566A US1244566A US15124517A US15124517A US1244566A US 1244566 A US1244566 A US 1244566A US 15124517 A US15124517 A US 15124517A US 15124517 A US15124517 A US 15124517A US 1244566 A US1244566 A US 1244566A
- Authority
- US
- United States
- Prior art keywords
- piston
- fins
- fuel
- combustion engine
- internal
- 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 title description 11
- 239000000446 fuel Substances 0.000 description 15
- 239000000203 mixture Substances 0.000 description 9
- 230000006835 compression Effects 0.000 description 8
- 238000007906 compression Methods 0.000 description 8
- 239000007789 gas Substances 0.000 description 4
- 229930195733 hydrocarbon Natural products 0.000 description 4
- 150000002430 hydrocarbons Chemical class 0.000 description 4
- 239000004215 Carbon black (E152) Substances 0.000 description 3
- 241000723554 Pontia occidentalis Species 0.000 description 3
- 239000002360 explosive Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 238000002309 gasification Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000010298 pulverizing process Methods 0.000 description 2
- 241000792859 Enema Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 239000007920 enema Substances 0.000 description 1
- 229940095399 enema Drugs 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 239000010959 steel 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
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
-
- 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
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
Definitions
- This invention relates to certain improvements in internal combustion engines and refers more particularly to a fuel gasifymg device onthe head of the piston, the main object of which is to permit the use of the cheaper grades of gasolene and other inferior hydrocarbons, at the same time to produce as high, if not a higher, degree of combustibility and explosive power than would be produced by the higher grades or more expensive hydrocarbon fuels.
- FIG. 1 is a perspective view of the piston equipped with one form of my improved fuel gasifying device.
- Fig. 2 is a vertical sectional view of the cylinder and piston of an internal combustion engine showing the same fuel gasifying device.
- the preferred form of my invention shown in Figs. 1 and 2 may be attached to the head of any of the standard forms of pistons now in common use in internal combustion engines and comprises a comparatively thin sheet metal plate -'1 of steel or other suitable metal capable of withstanding the heat to which it is subjected without appreciable deformation and is provided with a circumferential series of substantially radial fins or wings 2 and another circumferential series of axially extending wings or fins 3 alternating with the radial wings -2.
- All of these fins or wings 2- and 3 are. integrally united at their bases to the main body of the plate 1 and are preferably formed by making radial slits in the plate from the periphery inwardly along radial lines toward the center and then bending the alternate segments, as 3, axially, or at right angles to the plane of the main body while the wings or fins -2 are preferably deflected slightly from said plane away from the head of the piston so that the disk is somewhat concavo-convex with its convex side adjacent the piston head, as (a), and clamped to the center thereof by bolt -4, said bolt being held in spaced relation to the head of the piston by means of an interposed washer or equivalent spac- 'mg device 5-, the purpose of which is to allow the free circulation of the in-flowing fuel across the bottom and top of the plate to reduce liability of overheating said plate to incandescence by the combustion of the explosive mixture.
- the general plan of the disk plate 1- is circular and of less diameter than that of the piston to which it is secured so as not to interfere-in any way with the free action of said piston, at the same time leaving an annular space between its periphery and side walls of the cylinder, as (A) to allow the in-flowing fuel to travel entirely around the same.
- the axial deflection of the free ends of the wings or fins 3.leaves a space of corresponding width between the radial wings or fins 2, the purpose of which is to cause a more thorough agitation of the liquid fuel and air when flowing into the combustion chamber to produce a similar effect as the piston moves toward the head,
- the piston is shown by full lines at the limit of its power stroke and by dotted lines at the limit of its inward or compression stroke and from these two positions, it
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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
G. W. WHITE. INTERNAL COMBUSTION ENGiNE.
APPLICATION FILED FEB.27.1917.
1,244,566. Patented Oct. 30, 1911 in w D IN NT0R GEORGE W. WHITE, 01E SYRACUSE, NEW YORK.
mrnnnan-comnusrron Enema.
Specification of Letters Patent.
Patented Oct. 30, 1917.
Application filed February 27, 1917. Serial No. 151,245.
To all whom it may concern:
Be it known that I, GEORGE W. WHITE, a citizen of the United States of America, and resident of Syracuse, in the county of Onondaga, ,in the State of New York, have invented new and useful Improvements in Internal-Combustion Engines, of which the following, taken in connection with the accompanying drawings, is a full, clear, and exact description.
This invention relates to certain improvements in internal combustion engines and refers more particularly to a fuel gasifymg device onthe head of the piston, the main object of which is to permit the use of the cheaper grades of gasolene and other inferior hydrocarbons, at the same time to produce as high, if not a higher, degree of combustibility and explosive power than would be produced by the higher grades or more expensive hydrocarbon fuels.
In other words, I have sought to provide the piston with a simple and comparatively inexpensive attachment whereby an inferior fuel will be more thoroughly atomized and brought into a more effective mixture w1th the in-fiowing air after their introduction into the combustion chamber and at the same time gradually increasing the gasification of such mixtureduring the compression stroke of the piston, so that the maximum degree of gasification occurs at about the same time that the mixture is underhighest compression by the action of the piston; Other objects and advantages relative to specific parts of the device will be brought out in the following description.
In the drawings- Figure 1 is a perspective view of the piston equipped with one form of my improved fuel gasifying device.
Fig. 2 is a vertical sectional view of the cylinder and piston of an internal combustion engine showing the same fuel gasifying device.
The preferred form of my invention shown in Figs. 1 and 2 may be attached to the head of any of the standard forms of pistons now in common use in internal combustion engines and comprises a comparatively thin sheet metal plate -'1 of steel or other suitable metal capable of withstanding the heat to which it is subjected without appreciable deformation and is provided with a circumferential series of substantially radial fins or wings 2 and another circumferential series of axially extending wings or fins 3 alternating with the radial wings -2.
All of these fins or wings 2- and 3 are. integrally united at their bases to the main body of the plate 1 and are preferably formed by making radial slits in the plate from the periphery inwardly along radial lines toward the center and then bending the alternate segments, as 3, axially, or at right angles to the plane of the main body while the wings or fins -2 are preferably deflected slightly from said plane away from the head of the piston so that the disk is somewhat concavo-convex with its convex side adjacent the piston head, as (a), and clamped to the center thereof by bolt -4, said bolt being held in spaced relation to the head of the piston by means of an interposed washer or equivalent spac- 'mg device 5-, the purpose of which is to allow the free circulation of the in-flowing fuel across the bottom and top of the plate to reduce liability of overheating said plate to incandescence by the combustion of the explosive mixture.
The general plan of the disk plate 1- is circular and of less diameter than that of the piston to which it is secured so as not to interfere-in any way with the free action of said piston, at the same time leaving an annular space between its periphery and side walls of the cylinder, as (A) to allow the in-flowing fuel to travel entirely around the same.
The axial deflection of the free ends of the wings or fins 3.leaves a space of corresponding width between the radial wings or fins 2, the purpose of which is to cause a more thorough agitation of the liquid fuel and air when flowing into the combustion chamber to produce a similar effect as the piston moves toward the head,
of the cylinder where the spark plug, as (b) is located, that is, the fuel and air are free to flow around and between the radial fins 2- and also around and between the axially extending fins 3, the effect of which is to thoroughly pulverize the hydrocarbon and produce a more thorough mixture thereof with the air, thus greatly increasing the combustibility of the mixture.
The piston is shown by full lines at the limit of its power stroke and by dotted lines at the limit of its inward or compression stroke and from these two positions, it
will be readily understood that as the fuel is drawn into the combustion chamber during the suction stroke, either in a t-cycle or .Z-cycle engine, the particular arrangement of the two sets of fins, those of each being in spaced relation, allows the in-fiowing fuels to impinge against the sides of said fins, thereby producing a pulverization. of the hydrocarbon and thoroughly mixing the same with the air as previously described.
It is also evident that as the piston advances toward the head of the cylinder, the fuel will be further penetrated and agitated by the fins ,2 and -3- as the compression of the mixture gradually increases and as the highly compressed gases are penetrated by said fins, the heat imparted thereto by the previous explosions will be transmitted to said gases and thereby increasing their expansive force and power as the piston reaches the limit of its compression stroke so that the combined effect of pulverizing or atomizing the. fuel and thereby increasing its ability to more thoroughly mix with the air together with the heating of the mixture by the penetration of the heated fins thereinto while under a maximum degree of compression will cause the production from a relatively inferior fuel of a higher degree of power equal to or greater than that which might be produced by the highest grade of gasolene without my attachment.
At each explosion of the mixture,rthese fins become highly heated but this heat is menace somewhat reduced as the piston recedes increased explosive force of the gas as the piston approaches or reaches the limit of its compression stroke with the result that the highly heated and highly compressed gases produce an extremely high degree of power upon ignition which takes place simultaneously with the maximum degree of compression, all of which permits the use of a relatively low grade and comparatively inexpensive fuel without sacrifice of power.
What I claim is In an internal combustion engine, the combination of a cylinder, a piston movable therein, a plate secured to the head of the piston and provided with a set of radially extending fins and another, set of axially Eitending fins alternating with the radial s. In witness whereof I have hereunto set my hand this 24th day of February 1917. GEORGE W. WHITE. Witnesses:
H. E. CHASE, M. Vrom Howmno.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15124517A US1244566A (en) | 1917-02-27 | 1917-02-27 | Internal-combustion engine. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15124517A US1244566A (en) | 1917-02-27 | 1917-02-27 | Internal-combustion engine. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1244566A true US1244566A (en) | 1917-10-30 |
Family
ID=3312353
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15124517A Expired - Lifetime US1244566A (en) | 1917-02-27 | 1917-02-27 | Internal-combustion engine. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1244566A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3177861A (en) * | 1963-07-29 | 1965-04-13 | Southwest Res Inst | Internal combustion engine |
| US20070095201A1 (en) * | 2005-11-03 | 2007-05-03 | Donahue Richard J | Piston |
| US7293497B2 (en) | 2005-11-03 | 2007-11-13 | Dresser, Inc. | Piston |
-
1917
- 1917-02-27 US US15124517A patent/US1244566A/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3177861A (en) * | 1963-07-29 | 1965-04-13 | Southwest Res Inst | Internal combustion engine |
| US20070095201A1 (en) * | 2005-11-03 | 2007-05-03 | Donahue Richard J | Piston |
| US7293497B2 (en) | 2005-11-03 | 2007-11-13 | Dresser, Inc. | Piston |
| US7302884B2 (en) | 2005-11-03 | 2007-12-04 | Dresser, Inc. | Piston |
| US20080028929A1 (en) * | 2005-11-03 | 2008-02-07 | Dresser, Inc. | Piston |
| US7493850B2 (en) | 2005-11-03 | 2009-02-24 | Dresser, Inc. | Piston |
| US7506575B2 (en) | 2005-11-03 | 2009-03-24 | Dresser, Inc. | Piston |
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