US1004836A - Air-cooled explosion-engine. - Google Patents
Air-cooled explosion-engine. Download PDFInfo
- Publication number
- US1004836A US1004836A US53082509A US1909530825A US1004836A US 1004836 A US1004836 A US 1004836A US 53082509 A US53082509 A US 53082509A US 1909530825 A US1909530825 A US 1909530825A US 1004836 A US1004836 A US 1004836A
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- US
- United States
- Prior art keywords
- cylinder
- air
- explosion
- piston
- engine
- 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
- 238000004880 explosion Methods 0.000 description 35
- 230000006835 compression Effects 0.000 description 17
- 238000007906 compression Methods 0.000 description 17
- 238000001816 cooling Methods 0.000 description 11
- 238000005192 partition Methods 0.000 description 5
- 230000029058 respiratory gaseous exchange Effects 0.000 description 4
- 238000009991 scouring Methods 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P1/00—Air cooling
- F01P1/02—Arrangements for cooling cylinders or cylinder heads, e.g. ducting cooling-air from its pressure source to cylinders or along cylinders
Definitions
- Patented ocee, 1911 Patented ocee, 1911.
- Fig. 5 is a view similar to Fig. 2 showing the piston at the end of the stroke;
- Fig. 6 is a cross-section of the cylinder on the line 6-6 in Fig. 5; and
- Fig. 7 is a similar view on the line 7-7 in Fi 5.
- the invention is illustrated in connection with a two-cycle explosion engine but it is possible to use it on a four-cycle engine. Further, this invention has no connection with any particular system of supplying fuel to the engine and hence no further reference to the fuel will be made.
- the frame of the engine comprises an explosion cylinder 1; a circulation or respiration cylinder 2; and a closed crank-case 3.
- This frame is preferably made in three separate castings as shown, suitably secured together.
- the cylinder 1 has thin inner walls and is provided with a number of radiating cooling flanges 4: on its upper end and these flanges join the vertical flanges or partitlons 5 which surround the cylinder 1 and connect it to the heavy outer-wall .6 of thecylinder casting.
- the heavy outer wall 6 of the cylinder casting does not extend to the top of the cylinder 1.
- the passages between the partitions 5 are open at both ends and form cooling ports.
- the partitions extend about one-half way down the cylinder where the cooling ports between them merge into a large chamber 7.
- the inlet passage 8 and the exhaust passage 9 pass through this chamber 7 into the cylinder 1 near the bottom of the stroke and are suitably walled from the chamber 7 so that no communication can be had therewith. Also air passages pass through the two cooling bars 10 in the passages 8 and 9.
- the piston 11 fits the cylinder 1 in the usual manner and is of the common plunger form and is provided with a baffle plate 12 on its top.
- the circulation or respiration cylinder 2 is of larger diameter than the explosion cylinder 1 and-is open at its upper end to the chamber7 and the air passages 10.
- the piston 11 joins with the circulation piston 13 which works in the cylinder 2 and draws air down between the partitions 5 into and through the chamber 7 and then forces this warmed air out again on the return stroke thus simulating the complete respiration cycle.
- a by-pass passage 14 is made in the upper part of the circulation cylinder 2 around the piston 13, when it is at the beginning of its stroke, the purpose of which is to draw some of this warmed air into the crank case if desired, and the quantity of air thus drawn in can be controlled as hereinafter described.
- the crank-case 3 is of substantially the usual construction common in two-cycle engines, and has the usual passage 8 leading therefrom to the inlet portin the lower end of the cylinder 1.
- the air is normally admitted to the crank-case through an inlet valve 15 against the action of a spring 16.
- this spring 16 is wound on the shank 17 of the valve 15 between the nut '18 thereof and a loose washer 19.
- This washer 19 bears on the forked end on a bell-crank lever 20, suitably pivoted adjacent to the valve, in such-a manner as to allow the degree of compression of said spring to be adjusted as desired: in- Figs. 2 and 5 the spring is in its loosest position, while in Fig.
- the volume of air which is thus forced into the cylinder 1 is greater than the volume displaced by the piston 11, because the plsto-n 13 is greater in diameter than is the piston 11 and I prefer to make the volume of this scouring air somewhat greater than the entire volume of the cylinder 1 so that the burned gases will be entirely exhausted and even some of this fresh air will be” passed through the exhaust passage 9.
- a partial vacuum is made in the crank-case 3, as soon. as the port 8 is closed, thus causing the atmospheric pressure on the valve 15 to overcome the pressure of the spring 16 and to open the valve to draw in cold air into the crank-case.
- the amount of air will be substantially equal to the volume displaced by the piston 13 in its travel.
- an explosion engine .the combination with an explosion cylinder and piston working therein; radiation surfaces arranged thereon; an outer wall surrounding said radiation surfaces a part of their length; a circulation or compression cylinder coaxial with and of larger diameter than said explosion cylinder -a assage communicating with the space etween the outer and inner.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Description
A. E. WOLCOTT. AIR GOOLED EXPLOSION ENGINE.
APPLICATION FILED DEO..1, 1909.
- Patented Oct. 3, 1911.-
2 snnms-snngzw 1.
Arron/vi) A. E. WOLGOTT.
AIR OOOLED EXPLOSION ENGINE.
APPLIOATION FILED DEG. 1, 1909.
Patented 0st. 3, 1911.
2 SHEETS-SHEET 2.
, WITN SSES.- v INVENTOR.
44/6 Line/60% UNITE STATEd rn'rnnr onrron.
ALVEN E. WOLCO'IT, 0F LOWELL, WASHINGTON.
AIR-COOLED EXPLOSION-ENGINE.
Specification of Letters Patent.
Patented ocee, 1911.
Application filed December 1, 1909. Serial No. 530,825.
To all whom it may concern:
Be it known that I, ALVEN E. WoLoo'r'r,a citizen of the United States of America, residing at Lowell, in the county of Snohomish and State of Washington, have invented certain new and useful Improvements in Air-Cooled Explosion-Engines, of which the following is a specification, reference being had therein to the accompanying drawmg. This invention relates to explosion engines and has special reference to the means for cooling the engine by the circulation of air.
The objects of my invention are, first, to secure an absolute circulation of cold air uniformly around the outside of-the explosion cylinder; second, to secure an adequate supply of fresh air to scour the inside of the cylinder and free it from the hot burned gases of the explosion; and third, to provide means for regulating the temperature of this scouring air supply. I attain these and other objects by the devices, mechanisms, and arrangements illustrated in the accompanying drawings, in which- Figure 1 is a plan of an explosion engine made in accordance with my invention; Fig. 2 is a vertical cross-section thereof showing the piston at the beginning of the stroke; Fig. 3 is a section of the intake valve mechanism showing the valve spring tightened; Fig. 4 is a crosssection thereof on the line fir-4 in Fig. 3; Fig. 5 is a view similar to Fig. 2 showing the piston at the end of the stroke; Fig. 6 is a cross-section of the cylinder on the line 6-6 in Fig. 5; and Fig. 7 is a similar view on the line 7-7 in Fi 5.
Similar numerals of re erence refer to similar parts throughout the several views.
The invention is illustrated in connection with a two-cycle explosion engine but it is possible to use it on a four-cycle engine. Further, this invention has no connection with any particular system of supplying fuel to the engine and hence no further reference to the fuel will be made.
The frame of the engine comprises an explosion cylinder 1; a circulation or respiration cylinder 2; and a closed crank-case 3. This frame is preferably made in three separate castings as shown, suitably secured together. The cylinder 1 has thin inner walls and is provided with a number of radiating cooling flanges 4: on its upper end and these flanges join the vertical flanges or partitlons 5 which surround the cylinder 1 and connect it to the heavy outer-wall .6 of thecylinder casting. The heavy outer wall 6 of the cylinder casting does not extend to the top of the cylinder 1. The passages between the partitions 5 are open at both ends and form cooling ports. The partitions extend about one-half way down the cylinder where the cooling ports between them merge into a large chamber 7. The inlet passage 8 and the exhaust passage 9 pass through this chamber 7 into the cylinder 1 near the bottom of the stroke and are suitably walled from the chamber 7 so that no communication can be had therewith. Also air passages pass through the two cooling bars 10 in the passages 8 and 9. The piston 11 fits the cylinder 1 in the usual manner and is of the common plunger form and is provided with a baffle plate 12 on its top. The circulation or respiration cylinder 2 is of larger diameter than the explosion cylinder 1 and-is open at its upper end to the chamber7 and the air passages 10. The piston 11 joins with the circulation piston 13 which works in the cylinder 2 and draws air down between the partitions 5 into and through the chamber 7 and then forces this warmed air out again on the return stroke thus simulating the complete respiration cycle. A by-pass passage 14 is made in the upper part of the circulation cylinder 2 around the piston 13, when it is at the beginning of its stroke, the purpose of which is to draw some of this warmed air into the crank case if desired, and the quantity of air thus drawn in can be controlled as hereinafter described.
The crank-case 3 is of substantially the usual construction common in two-cycle engines, and has the usual passage 8 leading therefrom to the inlet portin the lower end of the cylinder 1. The air is normally admitted to the crank-case through an inlet valve 15 against the action of a spring 16. As illustrated in Figs. 2, 3, 1, and 5, this spring 16 is wound on the shank 17 of the valve 15 between the nut '18 thereof and a loose washer 19. This washer 19 bears on the forked end on a bell-crank lever 20, suitably pivoted adjacent to the valve, in such-a manner as to allow the degree of compression of said spring to be adjusted as desired: in- Figs. 2 and 5 the spring is in its loosest position, while in Fig. it has been course and inhales fresh cold air down the sides of the hot cylinder between the partitions 5.- This cold air comes from above and around the top of the cylinder. As soon as this air reaches the cooling orts between the outer wall 6 and the thin inner wall of the cylinder 1 its speed is increased until it reaches the chamber 7 whereit is again reduced. This warm air is then ex-' haled from the above cooling ports on the return stroke of the piston 13 so that said piston establishes respiration of the cooling air. Meantime the downward stroke of the piston compresses thev cold airin the crankcase 3 until the inlet port 8 of the cylinder 1 is uncovered by the piston 11, and this cold air is then transferred to the cylinder 1, further cooling the said cylinder. The volume of air which is thus forced into the cylinder 1 is greater than the volume displaced by the piston 11, because the plsto-n 13 is greater in diameter than is the piston 11 and I prefer to make the volume of this scouring air somewhat greater than the entire volume of the cylinder 1 so that the burned gases will be entirely exhausted and even some of this fresh air will be" passed through the exhaust passage 9. Then on the upward stroke of the piston 13 a partial vacuumis made in the crank-case 3, as soon. as the port 8 is closed, thus causing the atmospheric pressure on the valve 15 to overcome the pressure of the spring 16 and to open the valve to draw in cold air into the crank-case. The amount of air will be substantially equal to the volume displaced by the piston 13 in its travel. If now, when the piston 13 has passed between the ports of the by-pass 14, the pressure within the crank-case 3 is less than the atmospheric pressure, then some of the warmed air in the chamber 7 and between the partitions 5 will be drawn into the crank-case and will mix with the cold air therein and will slightly warm it. By manipulating the lever 20 the spring 16 may be tightened so that but com-' paratively little cold air will enter the crank-case past the valve 15, and'in that case a larger quantity of warmed air will be drawn thereinto through the cooling ports. In this 'way the temperature of this securing and charging air can be regulated to suit the changes in temperature of the atmosphere and other climatic or extraneous circumstances. Further, the temperature of the exhaust port 9 is reduced by the hollow cooling bar 10 therein.
There are many advantages that result from this invention, among which may be hottest part of the cylinder, because the explosion is confined to the top thereof, thus keeping the temperature of the cylinder substantially uniform from top to bottom; third, the scouring is more complete on account of the excess quantity of fresh air admitted into the cylinder; fourth, the friction. in the explosion cylinder is confined entirely to the piston rings as there is practically no side pressure thereon because the side pressure is entirely taken up by the piston 13 which is in the cold circulation cylinder 2, thus further reducing the heatin the explosion cylinder; andififth, the ease with which the temperature of the scouring air is controlled.
Having described my invention, what I claim is;
1. In an explosion engine, the combination with an explosion cylinder and piston working therein; a compression or circulation cylinder of larger diameter than said explosion cylinder; a passage connecting said cylinders, to convey the cold compressed air from the compression cylinder to the explosion cylinder when the passage is opened; and a piston formed integral with the piston in said explosion cylinder and fitting said compression cylinder whereby a greater volume of cold air is forced into the explosion cylinder than is displaced by the piston therein.
2. In an explosion engine, the combination with an explosion cylinder and piston working therein; a compression or circulasaid cylinders, to convey the cold' com Y pressed air from the compression cylinder to the explosion cylinder when-the passage is opened; a check valve adapted to admit cold air to the compression cylinder; and a piston formed integral with the piston in said explosion cylinder and fitting said com-' pression cylinder whereby a greater'volume of cold air is forced into the explosion cyl-- I mder than is displaced by the piston therein.
. 3. In an explosion. engine, the combination with an explosion cylinder and piston working therein; a compression or circulation cylinder of larger diameter than said explosion cylinder; a passage connecting said cylinders, to conveythe cold compressed air from the compresion cylinder to the explosion cylinder when the passage is opened; an adjustable check valve adapted to admit cold air to the compression cyl-' inder when the'pressure therein is below a predetermined point; a piston formed integral with the plston in said explosion cylinder and fitting said compression cylinder n whereby a larger volunie'of cold air is forced intothe explosion cylinder than is displaced by the p1ston therein; and a bypass in said compressioncylinder and connecting said compression cylinder with the outer air when'fthe piston is at the beginning of its stroke.
4. Inv an explosion engine, .the combination with an explosion cylinder and piston working therein; radiation surfaces arranged thereon; an outer wall surrounding said radiation surfaces a part of their length; a circulation or compression cylinder coaxial with and of larger diameter than said explosion cylinder -a assage communicating with the space etween the outer and inner. walls of the explosion cylinder and leading into the compression cylinder at a point near the top thereof and adapted to admit the warmed air from the said' space into the compression cylinder; a passage connecting said cylinders to convey in presence 0 the cool compressed air from the compresslon cylinder to theexplosion cylinder when the passage is opened; an adjustable check valve adapted to admit cold air to the compression cylinder when the pressure therein is below a predetermined point; and a'piston formed integral with the piston in said explosion cylinder and fitting said compression cylinder whereby a greater volume of cool air is forced into the explosion cylinder than is displaced by the piston therein, and adapted to open the passage communicating between the compression cylinder and the space between the outer and inner walls of the explosion cylinder when it is at the beginning of its stroke. v
In testimon whereof 'I afiix my signature two witnesses.
ALVEN E. WOLCOTT. Witnesses:
R. T. WARNER,
C. J. SMITH.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US53082509A US1004836A (en) | 1909-12-01 | 1909-12-01 | Air-cooled explosion-engine. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US53082509A US1004836A (en) | 1909-12-01 | 1909-12-01 | Air-cooled explosion-engine. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1004836A true US1004836A (en) | 1911-10-03 |
Family
ID=3073150
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US53082509A Expired - Lifetime US1004836A (en) | 1909-12-01 | 1909-12-01 | Air-cooled explosion-engine. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1004836A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2736302A (en) * | 1950-01-11 | 1956-02-28 | Kloeckner Humboldt Deutz Ag | Air-cooled two-cycle internal-combustion engines |
-
1909
- 1909-12-01 US US53082509A patent/US1004836A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2736302A (en) * | 1950-01-11 | 1956-02-28 | Kloeckner Humboldt Deutz Ag | Air-cooled two-cycle internal-combustion engines |
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