US1342922A - Gas-engine - Google Patents
Gas-engine Download PDFInfo
- Publication number
- US1342922A US1342922A US1342922DA US1342922A US 1342922 A US1342922 A US 1342922A US 1342922D A US1342922D A US 1342922DA US 1342922 A US1342922 A US 1342922A
- Authority
- US
- United States
- Prior art keywords
- cylinder
- air
- cylinders
- 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
- 239000007789 gas Substances 0.000 description 24
- 238000001816 cooling Methods 0.000 description 14
- 239000000203 mixture Substances 0.000 description 14
- 230000002000 scavenging Effects 0.000 description 10
- 229910001018 Cast iron Inorganic materials 0.000 description 6
- 239000002360 explosive Substances 0.000 description 6
- 210000000614 Ribs Anatomy 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 241000764238 Isis Species 0.000 description 2
- 241000428533 Rhis Species 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000000875 corresponding Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000001939 inductive effect Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 229920003245 polyoctenamer Polymers 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
Images
Definitions
- rlhis invention relates to gas engines of the rotary cylinder type such as used for airplanes and has for its object to provide for more efficiently and uniformly cooling the cylinders by currents of air induced by centrifugal force through longitudinal air passageways positioned around the cylinders.
- Another object of the invention is to secure ellicient scavenging of the burnt gases from the cylinder with an engine of the two cycle type.
- the invention consists of the gas engine, its parts and combinations of parts as herein claimed and all equivalents.
- Figure 1 is a sectional view of a gas engine embodying the present invention with one cylinder sectioned showing the piston thereof at the end of its working stroke;
- Fig. 2 is a similar' view of a slightly modified form thereof with the piston at the end of its compression stroke;
- Fig. 8 is an end View of one cylinder
- Fig. l is a transverse "sectional view thereof showing the construction of the cooling jacket.
- sheet metal casing 18 connects the inner ends of the jackets 16 to form an inclos'ure' therewith through which air passes for cooling the cylinders.
- Upen'ings 19 are formed in the ends of the casing 18 near the center and through them air enters the casing and passes out through the narrow passageways between the fins 17 around the cylinders, being forcibly propelled by the rapid rotation of the cylinders and the casing acting on the principle of the blower pump. rhis outward current of air evenly distributed around each cylinder serves to cool the cylinder walls uniformly and to prevent the distortion that occurs when they are not covered.
- Parallel metal disks 18 are placed at opposite sides of' the cylinders in contact with the jackets 16 and extending from the casing 18 to the outer ends of the cylinders to prevent a disturbance of the air by the travel of the cylinders with a conseqiunuresistance to the movements of the rotor.
- the cylinder head 20 is cylindrical and extends a considerable distance within the end of the cylinder 12 with its sidewalls concentric with the side walls of the cylinder to form an annular space between them.
- rlChe piston 13 is provided with a sleevelike cylindrical extension 21 tting within a cylinder'
- the an- Vward movement of the piston register with openings 26 in the cylinder 12 to admit compressed air or an explosive charge either from the casing 18 direct as in Fig. 2, or from pipes 27 from a blower or other supply means as in Fig. 1.
- the fuel may be introduced into the cylinder either with the air through registering openings 25 and 26, or in a ⁇ liquid form through a valve-controlled pipe 28'passing through the cylinder head V20.
- a spark plug 29 is also provided in the cylinder head.
- the compression stroke of the piston carries the openings 25 out of register with the openings 26 and closes the exhaust passageway between the end of the piston extension sleeve 21 and the cylinder head 2O so that during the travel of the sleeve 21 in contact with the pistonV rings 23 the air or charge of explosive mixture is compressed above the piston. If only air has been introduced at the inner end of the cylinder, liquidfuel is injected through the pipe 2S. The explosion of the compressed charge is effected by the spark plug as usual either just before or after the piston has reached the end of its outward stroke and the expanding burnt gases are exhausted before the piston reaches the end of its power stroke, or as soon as the extension sleeve 21 passes the end of the cylinder head.
Landscapes
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
v G. L. MEYER.
GAS ENGINE. APPLICATION FILED APH. II, IsIs.
Patented June 8, 1920. 2 SHEETS-SHEET I.
w/T/vesss ffm@ 754 MM@ Patented June 8, QZ.
2 SHEETS-SHEET 2.
/lVVE/V TOR G. L. MEYER.
GAS ENGINE. APPLICATION FILED APII. II. I9I8.
www
QAM #am GEORGE L. lVIEYEIt, OF MILW'AUKEE, VISCONBIN.
oas-ENGINE.
ppla'tzion filed April 11,
To all whom t may concern:
Be it known that l, Gnoncn L. MEYER, citizen of the United States, and resident of lllilwaukee, in the county of Milwaukee and State of lisconsin, have invented new and useful Improvements in Gras-Engines, of which the following is a description, reference being had to theY accompanying drawings, which are a part of this specilication.
rlhis invention relates to gas engines of the rotary cylinder type such as used for airplanes and has for its object to provide for more efficiently and uniformly cooling the cylinders by currents of air induced by centrifugal force through longitudinal air passageways positioned around the cylinders. e
Another object of the invention is to secure ellicient scavenging of the burnt gases from the cylinder with an engine of the two cycle type.
lilith the above and other objects in view, the invention consists of the gas engine, its parts and combinations of parts as herein claimed and all equivalents.
Referring to the accompanying drawings in which like characters of reference indicate the same parts indifferent views:
Figure 1 isa sectional view of a gas engine embodying the present invention with one cylinder sectioned showing the piston thereof at the end of its working stroke;
Fig. 2 is a similar' view of a slightly modified form thereof with the piston at the end of its compression stroke;
Fig. 8 is an end View of one cylinder; and,
Fig. l is a transverse "sectional view thereof showing the construction of the cooling jacket. e
ln these drawings 10 indicatesV a stationary crank shaft and 11 isy the rotor mounted to rotate therearound las usual, and carrying the radially positioned cylinders 12. The pistons 13 in the cylinders are connected by their connecting rods 14 with the crank 15 of the crank shaft. ln usual practice the cylinders are left without covering so that cooling may be effected by their rapid travel through the air. This, however, causes unequal cooling with a correspond ing distortion of the cylinders, for the cooling effect is greater at that portion of the cylinder which is in advance. The distortion from the true cylindrical shape of thc cylinder walls causes binding with the pis- Speoicaton of Letters Patent.
Patented J une te, i929.
1918. Serial No. 227,928.
rounding each cylinder and spaced there4 from by fitting around numerous longitudinally extending radial fins or ribs 17 around the cylinder and preferably integral with the walls thereof, as shown in Fig. e. sheet metal casing 18 connects the inner ends of the jackets 16 to form an inclos'ure' therewith through which air passes for cooling the cylinders. Upen'ings 19 are formed in the ends of the casing 18 near the center and through them air enters the casing and passes out through the narrow passageways between the fins 17 around the cylinders, being forcibly propelled by the rapid rotation of the cylinders and the casing acting on the principle of the blower pump. rhis outward current of air evenly distributed around each cylinder serves to cool the cylinder walls uniformly and to prevent the distortion that occurs when they are not covered.
ln order to further utilize the centrifugal force of therapidly rotating cylinders, provision is made for scavenging the cylinder by opening both ends thereof so as to admit air or explosive mixture the inner end of the cylinder or the end nearer the crank shaft and to exhaust the burnt gases at the other end. W ith this object in view the cylinder head 20 is cylindrical and extends a considerable distance within the end of the cylinder 12 with its sidewalls concentric with the side walls of the cylinder to form an annular space between them. rlChe piston 13 is provided with a sleevelike cylindrical extension 21 tting within a cylinder' The an- Vward movement of the piston register with openings 26 in the cylinder 12 to admit compressed air or an explosive charge either from the casing 18 direct as in Fig. 2, or from pipes 27 from a blower or other supply means as in Fig. 1. The fuel may be introduced into the cylinder either with the air through registering openings 25 and 26, or in a` liquid form through a valve-controlled pipe 28'passing through the cylinder head V20. A spark plug 29 is also provided in the cylinder head. Y
' In operation the compression stroke of the piston carries the openings 25 out of register with the openings 26 and closes the exhaust passageway between the end of the piston extension sleeve 21 and the cylinder head 2O so that during the travel of the sleeve 21 in contact with the pistonV rings 23 the air or charge of explosive mixture is compressed above the piston. If only air has been introduced at the inner end of the cylinder, liquidfuel is injected through the pipe 2S. The explosion of the compressed charge is effected by the spark plug as usual either just before or after the piston has reached the end of its outward stroke and the expanding burnt gases are exhausted before the piston reaches the end of its power stroke, or as soon as the extension sleeve 21 passes the end of the cylinder head. Residual pressure within the cylinder will thus be vented before the openings 25 and 26 come'into register. IVhe'n these openings register there is a quick scavenging action due to the rush of air through said openings and the outflow of exhaust gases Y through the annular space between the cylinder head and the cylinder with the assistance of the centrifugal force of the rotating cylinders tending to produce outwardly directed currents of air for cooling and scav-l engingthe cylinder.` Furthermore, the arrangement Vof thev jacket 16 tightly fitting on the radial longitudinally extending ribs or ns of the cylinder serves to greatly strengthen the cylinder, enabling the use of a cast iron cylinder instead of a steel cylinder which is usually employed on account of its greater strength. The cast iron cylinder with a cast iron piston is found to be a better combination for the purpose as there is less likelihood of scoring and their bearing surfaces take a glaze, reducing friction and increasing eiiciency.
I desire it to be understood that the invention is not limited to any specific form or arrangement of parts Vexcept in so far as such limitations are specified in the claims.
IVhat I claim as new and desire to secure by Letters Patent is:
1. In a gas engine of the rotary cylinder type, the-combination with the rotary cylinder, of a hollow jacket surrounding the cylinder and open at both ends, a scavenge port in the cylinder, means for controlling the passage of scavenging air to the interior of the cylinder, and means for simultaneously conducting air both to the scavenge port and through the jacket under the influence of the centrifugal force of the rotating cylinder. j 2. In a gas engine of the rotary vcylinder type, the combination with the rotary cylinder of an inclosed crank casefhaving an air inlet, a hollow jacketsurrounding the cylinder and communicating at its. inner end with the crank case and open at its outer end, scavenge ports in the cylinder in communication with the crankcase, and means for controlling the passage of scavenging lair through said ports, the rotation ofthe cylinder simultaneously inducing by centrifugal force the passage of air through the jacket and through the interior of the cylinder.
3. In a gas engine of the rotary cylinder type, the combination, with the rotary cylinder, of a hollow jacket surrounding the cylinder and open at both ends, a casing communicating with the cylinder and jacket,
and means under the influence of centrifu-V gal force of the rotating cylinder for supplying both the interior of the jacket and cylinder with air from said casing.
In testimony whereof I ax my signature in presence ofl two witnesses. Y GEORGEL. MEYER.
Witnesses: 2 R. S. C. CALDWELL,
H. D. CHASE.
ioo
Publications (1)
Publication Number | Publication Date |
---|---|
US1342922A true US1342922A (en) | 1920-06-08 |
Family
ID=3395604
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US1342922D Expired - Lifetime US1342922A (en) | Gas-engine |
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US (1) | US1342922A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442237A (en) * | 1945-09-15 | 1948-05-25 | Harold Andresen | Internal-combustion engine |
US2665668A (en) * | 1949-03-22 | 1954-01-12 | Patrick C Ward | Engine |
US5000132A (en) * | 1990-07-09 | 1991-03-19 | Jiro Takashima | Scavenging system for a two-stroke internal combustion engine |
-
0
- US US1342922D patent/US1342922A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442237A (en) * | 1945-09-15 | 1948-05-25 | Harold Andresen | Internal-combustion engine |
US2665668A (en) * | 1949-03-22 | 1954-01-12 | Patrick C Ward | Engine |
US5000132A (en) * | 1990-07-09 | 1991-03-19 | Jiro Takashima | Scavenging system for a two-stroke internal combustion engine |
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