US1814802A - Starting system for internal combustion engines - Google Patents
Starting system for internal combustion engines Download PDFInfo
- Publication number
- US1814802A US1814802A US379450A US37945029A US1814802A US 1814802 A US1814802 A US 1814802A US 379450 A US379450 A US 379450A US 37945029 A US37945029 A US 37945029A US 1814802 A US1814802 A US 1814802A
- Authority
- US
- United States
- Prior art keywords
- engine
- blower
- polyhedron
- internal combustion
- starting system
- 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
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N19/00—Starting aids for combustion engines, not otherwise provided for
- F02N19/001—Arrangements thereof
Definitions
- ATTORNEY sets of cylinders disposed in side-by-side res polyhedron.
- My invention relates to internal combustion engines and particularly to starting systems therefor and it has for an object to provide apparatus of the character designated which shall operate reliably and effectively and which shall be readily applicable to Varions types and forms of internal combustion GIIUIIIBS.
- FIG. 1 is alongitudinal view, in section, of a polyhedral form of engine provided with one form of starting system arranged in accordance with my invention
- Fig. 2 is a transverse, sectional view, taken on the line IIII of Fig. 1;
- Fig. 3 is an end View, in elevation, of the engine and starting system shown in Fig. 1;
- Fig. 1 is atransverse View, in elevation, of the transmission mechanism embodied in the engine shown in Fig. 1.
- crank shafts 13 being located at the corner regons of the polygon and extending-longitudinally of the several assembled polygon aggregates.
- pistons 14 and 15 are provided in each cylinder 12 .
- the engine shown in the drawings may be operated upon either the Diesel or the Otto cycle or upon the two-cycle or four-cycle principles, it is assumed in the present embodiment that the engine operates upon the tWo-cycle principle and upon the Diesel cycle.
- the fuel is injected into each cylinder through an admission port 17 located in a central portion thereof and between the opposed pistons. Located on opposite sides of the admission port 17,
- each cylinder is respective series of inlet and exhaust ports 18 and 19.
- the ports 18 and 19 are arranged to be covered and uncovered by the pistons associated therewith,
- the inlet ports 18 are 10-.
- exhaust ports of each cylinder are opened before the admission ports and closed before the latter. In this way, thorough scavenging and supercharging of each of the engine cylinders may be readily effected.
- each of the crank shafts 13 is provided'with a suitable crank case 23; and, as shown in Fig.1, located at an intermediate or central portion of each crank shaft 13, is adrive gear 24.
- Each of the drive gears 24 mesh, through suitable idler gears 25, with the external teeth of a master ring gear 26 located on the longitudinal axis of the polyhedron, all as particularly shown in Fig. 4.
- a drive shaft 27 Secured to and rotatable withthe master ring gear 26 is a drive shaft 27 which projects outwardly of the polyhedron and which is operatively connected to a driven element such as, for example, a propeller 28.
- a suitable thrust and steady bearing 29 supported from the engine structure by means of diagonally extending stay rods 31.
- a suitable thrust and steady bearing 29 supported from the engine structure by means of diagonally extending stay rods 31.
- the internal teeth of the master ring gear 26 mesh with a plurality of circumferentially spaced pinions 30 located .on fixed pinion shafts 31'.
- Each pinion 3O drives a gear 40, all of the gears meshing with. a common sun gear 50.
- the sun gear is operatively connected to a shaft 31 of a blower 32, the gearing being so proportioned, as is apparent from the drawings. that theblower operates at a greater speed than the engine crank shafts.
- the blower 32 is preferably disposed within the polyhedron defined by the engine cylinders in order that the entire engine structure may be made as compact as possible.
- blower apparatus While various types of blower apparatus may be employed, I.have shown, by way ofexample, a blower having three runners 33," all driven from the common shaft 31 and operating in parallel to discharge fluid under pressure through an annular duct 34 to master distributing manifold 35. Air is supplied to the blower 32 from an intake reservoir .36 having radially extending ducts 37 projecting through the discharge duct 34 and commumeating with the eyes 38 of the respective runners.
- erial No. 298,778 entitled Scavenging and supe-rcharging system for internal combustion engines, and assigned to the Westinghouse Electric and Manufacturin Company;.
- the master distributing manifold 35 is provided with a plurality of tangentially extending branch ducts 41 communicating, respectively, with the intake manifolds 22.
- the blower drive shaft 31 rojects outwardly beyond the outer wall 0 the master distributing manifold 35 and is provided at its extremity with a jaw coupling 42 arranged to cooperate with a jaw coupling 43 of a starting motor 44.
- the starting motor 44 may be any conventional type; and, in the present embodiment, I have shown by way of example, a starting motor of the inertia type.
- the inertia starter 44 is provided with a lever 45 for cranking the same and an operating rod 46 for engaging the starter jaw 43 with the jaw 42 of the blower shaft when the starter has been brought up'to speed.
- the inertia starter 44 is first of all actuated by the crank handle 45' until such time as the required amount of inertia has been developed, whereupon the operating rod 46 is moved and the jaw 43 thrown into engagement with the jaw 42 of the blower shaft. Movement of the blower shaft results in moving all of the crank shafts of the engine, the arrangement of the gearing being such that v the crank shafts move at a relatively slower speed than the blower shaft. Adequate movement of the crank shafts is effective to cause ignition of the fuel in the engine cylinders and operation of the engine ensues.
- Operation of theengine causes the blower shaft 31 to be driven at a speed greater than the engine crank shafts and the jaw 43 of P the inertia starter is kicked out and the starter disconnected from the engine.
- the blower 32 distributes air under pressureto the distributing manifold 35 and thence to the respective cylinder manifolds 22.
- the pistons of the respective cylinders move outwardly upon their working strokes in predetermined timed sequence; and, upon the exhaust ports 19 of each cylinder being uncovered by their associated piston 15, the burnt gases are liberated to the exhaust manifold 21.
- the admis sion ports 18 are opened and the air under pressure supplied by the blower 32 sweeps the burnt gases remaining in the cylinder outwardly through the exhaust ports 19. This scavenging process continues until the exhaust piston 15 closes the exhaust ports 19 during its return stroke but, the admission ports 18 being still open, the air supplied by the blower 32 continues to enter the cylinder and serves to supercharge the same.
- crank shafts interposed between adjacent cylinders and extending longitudinally of the polyhedron and transmission means extending transversely of the polyhedron and located centrally of the ends thereof for interconnecting the crank shafts for operation in unison, of a blower disposed within the polyhedron, a starting mechanism located exteriorly of the polyhedron, and means, in-
- cluding speed transformation means for connecting both the blower and the starter to the engine crank shafts, said connecting" means embodying at least a portion of said transmission means.
- crank shafts interposed between adjacent cylinders and extending longitudinally of the polyhedron and transmission means extendmg transversely of the polyhedron and located centrally of theends thereof for interconnecting the crank shafts for operation in unison, of a. blower including a blower shaft disposed within. the polyhedron, a starter disposed coaxial with the blower-and operatively connected to the blower shaft, and means, including speed transformation means, for operatively connecting the blower shaft to the engine crank shafts.
- crankshafts interposed between adjacent cylinders and .extending longitudinally of the polyhedron and transmissiom means extending transversely of the polyhedron and located centrally'of the ends thereof for inter- I connecting the crank shafts for operation in unison,of a blower located within the polyhedron and having a blower shaft disposed coaxial with the polyhedron, a starter disposed exteriorly of the polyhedron and connected tothe blower shaft, and means including speed transformation means for operatively connecting the blower shaftto the engine crank shafts.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Description
H. T. HERR July 14, 1931.
STARTING SYSTEM FOR INTERNAL COMBUSTION ENGINES Filed July 19, 1929 2 Sheets-Sheet l INVENTOR HI HERR- WITNESS BY CL. Q, ATTORNEY July 14, 1931. H. T. HERR 1 STARTING SYSTEM FOR INTERNAL COMBUSTION ENGINE IS Filed Jul}; 19, 1929 2 Sheets-Sheet 2 WITNESS INVENTOR 5 HI HERR I BY (31.9mm
ATTORNEY sets of cylinders disposed in side-by-side res polyhedron.
Patented July 14, 1931! ounce HERBERT T. HERB, OF PHILADELPHIA, PENNSYLVANIA, ASSIGNOR T0 WESTINGHOUSE ELECTRIC & MANUFACTURING COMPANY, A CORPORATION OF PENNSYLVANIA STARTING SYSTEM FOR INTERNAL COMBUSTION ENGINES Application filed July 19, 1929. Serial No. 379,450.
My invention relates to internal combustion engines and particularly to starting systems therefor and it has for an object to provide apparatus of the character designated which shall operate reliably and effectively and which shall be readily applicable to Varions types and forms of internal combustion GIIUIIIBS.
It has for still another object to provide a system of the character designated so arranged that there may be readily embodied therein various types of motor devices such as, for example, mechanical, electrical, hydraulic, etc., for initiating the starting movement. a
It has for still another object to provide a system of the character designated which shallbe especially applicable to engines of the multi-cylinder type and which shall pro- Vide for applying the starting torque to an. intermediate or central portion of the crank shafts of engines of this character in order that the stresses setup in the engine crank shaft incidentto starting may be lessened.
It has for still another object to provide a starting system which shall be especially applicable to engines embodying two or more crank shafts and more especially to engines of the square or polygon type, that is, engines composed of a plurality of polygonal lation and defining a polyhedron, the crank shafts being located between ad acent cylinders and extending longitudinally of the It has for still another object to provide a system of the character designated, which shall be especially applicable to engines provided with scavenging or supercharging blower apparatus driven from the engine and at a greater speed than the engine in that I propose to utilize the drive mechanism between the blower and the engine to connect the starter to the engine, thereby simplifying the construction of the starting system and lessening the weight thereof.
These and other objects are effected by my invention, as will be apparent from the following description and claims taken in connection with the accompanying drawings,
forming a part of this application, in which Fig. 1 is alongitudinal view, in section, of a polyhedral form of engine provided with one form of starting system arranged in accordance with my invention;
Fig. 2 is a transverse, sectional view, taken on the line IIII of Fig. 1;
Fig. 3 is an end View, in elevation, of the engine and starting system shown in Fig. 1; an
Fig. 1 is atransverse View, in elevation, of the transmission mechanism embodied in the engine shown in Fig. 1.
Feferring to the drawings, I show in Fig. 1, an engine composed of aplurality of polygon aggregates 11 disposed in side-by-side relation and forming a polyhedron. As-
12 arranged so that their axes define a polygon, suitable crank shafts 13 being located at the corner regons of the polygon and extending-longitudinally of the several assembled polygon aggregates. Provided in each cylinder 12 are opposed pistons 14 and 15 connected through suitableoonnecting rods 16 to adjacent crank shafts.
Although the engine shown in the drawings may be operated upon either the Diesel or the Otto cycle or upon the two-cycle or four-cycle principles, it is assumed in the present embodiment that the engine operates upon the tWo-cycle principle and upon the Diesel cycle. Hence, the fuel is injected into each cylinder through an admission port 17 located in a central portion thereof and between the opposed pistons. Located on opposite sides of the admission port 17,
of each cylinder, are respective series of inlet and exhaust ports 18 and 19. The ports 18 and 19 are arranged to be covered and uncovered by the pistons associated therewith,
and, preferably, the inlet ports 18 are 10-.
inc
bit
maining crank shafts. As disclosed and claimed in U. S. Patent No. 1,701,360 for internal combustion engine and assigned to.
exhaust ports of each cylinder are opened before the admission ports and closed before the latter. In this way, thorough scavenging and supercharging of each of the engine cylinders may be readily effected.
Associated with the exhaust ports in the respective cylinders are'exhaust manifolds 21 and associated with the inlet ports 18 are admission manifolds 22. Each of the crank shafts 13 is provided'with a suitable crank case 23; and, as shown in Fig.1, located at an intermediate or central portion of each crank shaft 13, is adrive gear 24. Each of the drive gears 24 mesh, through suitable idler gears 25, with the external teeth of a master ring gear 26 located on the longitudinal axis of the polyhedron, all as particularly shown in Fig. 4. Secured to and rotatable withthe master ring gear 26 is a drive shaft 27 which projects outwardly of the polyhedron and which is operatively connected to a driven element such as, for example, a propeller 28. Associated with the propeller 28 is a suitable thrust and steady bearing 29 supported from the engine structure by means of diagonally extending stay rods 31. For a more detailed description of the construction of the transmission mechanism for interconnecting the crank shafts and as Well as for the structure supporting the propeller and connecting the same to the engine, reference may be had to my copending application, Serial No. 370,606, filed June 13, 1929, entitled Internal combustion engine an d assigned to the Westinghouse Electric and Manufacturing Company.
As shown particularly in Fig. 4, the internal teeth of the master ring gear 26 mesh with a plurality of circumferentially spaced pinions 30 located .on fixed pinion shafts 31'. Each pinion 3O drives a gear 40, all of the gears meshing with. a common sun gear 50. The sun gear is operatively connected to a shaft 31 of a blower 32, the gearing being so proportioned, as is apparent from the drawings. that theblower operates at a greater speed than the engine crank shafts. The blower 32 is preferably disposed within the polyhedron defined by the engine cylinders in order that the entire engine structure may be made as compact as possible. While various types of blower apparatus may be employed, I.have shown, by way ofexample, a blower having three runners 33," all driven from the common shaft 31 and operating in parallel to discharge fluid under pressure through an annular duct 34 to master distributing manifold 35. Air is supplied to the blower 32 from an intake reservoir .36 having radially extending ducts 37 projecting through the discharge duct 34 and commumeating with the eyes 38 of the respective runners. For a more detailed description of the construction and operation of my blower apparatus, reference ma be had to my copending application, erial No. 298,778, entitled Scavenging and supe-rcharging system for internal combustion engines, and assigned to the Westinghouse Electric and Manufacturin Company;. As shown parti-cularly in Fig. 3, the master distributing manifold 35 is provided with a plurality of tangentially extending branch ducts 41 communicating, respectively, with the intake manifolds 22.
Preferably, the blower drive shaft 31 rojects outwardly beyond the outer wall 0 the master distributing manifold 35 and is provided at its extremity with a jaw coupling 42 arranged to cooperate with a jaw coupling 43 of a starting motor 44. The starting motor 44 may be any conventional type; and, in the present embodiment, I have shown by way of example, a starting motor of the inertia type. As is Well understood in the art, the inertia starter 44 is provided with a lever 45 for cranking the same and an operating rod 46 for engaging the starter jaw 43 with the jaw 42 of the blower shaft when the starter has been brought up'to speed.
From the foregoing description, the method of operating my improved starting system will be apparent. Assuming that the engine is idle and that it is desired to start the same, the inertia starter 44 is first of all actuated by the crank handle 45' until such time as the required amount of inertia has been developed, whereupon the operating rod 46 is moved and the jaw 43 thrown into engagement with the jaw 42 of the blower shaft. Movement of the blower shaft results in moving all of the crank shafts of the engine, the arrangement of the gearing being such that v the crank shafts move at a relatively slower speed than the blower shaft. Adequate movement of the crank shafts is effective to cause ignition of the fuel in the engine cylinders and operation of the engine ensues.
Operation of theengine causes the blower shaft 31 to be driven at a speed greater than the engine crank shafts and the jaw 43 of P the inertia starter is kicked out and the starter disconnected from the engine. During the operation of the engine, the blower 32 distributes air under pressureto the distributing manifold 35 and thence to the respective cylinder manifolds 22.
. In the operation of the engine, the pistons of the respective cylinders move outwardly upon their working strokes in predetermined timed sequence; and, upon the exhaust ports 19 of each cylinder being uncovered by their associated piston 15, the burnt gases are liberated to the exhaust manifold 21. After opening of the exhaust ports 19,,the admis sion ports 18 are opened and the air under pressure supplied by the blower 32 sweeps the burnt gases remaining in the cylinder outwardly through the exhaust ports 19. This scavenging process continues until the exhaust piston 15 closes the exhaust ports 19 during its return stroke but, the admission ports 18 being still open, the air supplied by the blower 32 continues to enter the cylinder and serves to supercharge the same. The supercharging process continues until such time as the admission ports 18 are closed by their associated piston 14 whereupon the pistons 14 and 15 move toward each other upon their compression stroke. At a suitable point in the compression stroke, the fuel is injected into the compressed air obtaining in the cylinder and ignition again takes place in accordance with the well known principles of the Diesel cycle.
From the foregoing, it will be apparent that I have provided a starting system which is especially applicable to engines equipped with blowers or superchargers in that the transmission mechanism utilized for driving the blower or supercharger at a speed greater than theengine is utilized during times of starting to drive the engine at a speed less than that of the starting motor. In this way, only one transmission mechanism is required for both the blower drive and the starting system and hence the weight and the space occupied by the starting system is materially reduced, a feature that is especially desirable with engines employed in the propulsion of aircraft.
It will be further apparentth'at I have provided a starting system which isespecially applicable to engines wherein :a plurality of aligned cylinders are associated'with a com mon crank shaft in that thestarting 'torque' is provided at a central or intermediate portion of the crank shaft, rather than at an end portion, and hence the stresses set up in the crankshaft inc-ident to starting are lessened.
It will be st'pll further apparent that I have "provided a starting system which is especially'adapted for use with engines of the multi-crank shaft type in that the starting torque is simultaneously applied to severa-l crank shafts and hencethe forces imposed upon any one crank shaft are lessened.
It will also be apparent that 'Ihave devised a starting system which is especially applicable to engines of the square or polygon type inthat the transmission mechanism for interconnecting the crank shafts for operation in unison is utilized as a part of the starting system.
While I have shown my invention in but one form, it will be obvious to those skilled 1n the art that it is not so limited, but is susceptible of various changes and modifications, without departing from the spirit thereof, and I desire, therefore, that only such limitations shall be placed thereupon as are imposed by the prior art or as are specifically set forth in the appended claims.
What I claim is: v
1. The combination with an internal combustion engine embodying a plurality of polygonal sets of cylinders disposed in sideby-side relation and defining a polyhedron, crank shafts. interposed between adjacent cylinders and extending longitudinally of the polyhedron and transmission means extending transversely of the polyhedron and located centrally of the ends thereof for interconnecting the crank shafts for operation in unison, of a blower disposed within the polyhedron, a starting mechanism located exteriorly of the polyhedron, and means, in-
cluding speed transformation means, for connecting both the blower and the starter to the engine crank shafts, said connecting" means embodying at least a portion of said transmission means.
2. The combination with an internal combustion engine embodying a plurality of polygonal sets of cylinders disposed in sideby-side relation and defining a polyhedron, crank shafts interposed between adjacent cylinders and extending longitudinally of the polyhedron and transmission means extendmg transversely of the polyhedron and located centrally of theends thereof for interconnecting the crank shafts for operation in unison, of a. blower including a blower shaft disposed within. the polyhedron, a starter disposed coaxial with the blower-and operatively connected to the blower shaft, and means, including speed transformation means, for operatively connecting the blower shaft to the engine crank shafts.
8. The combination with an internal combustion engine embodying a plurality of polygonal sets of cylinders disposed in side by-side relation and defining a. polyhedron,
crankshafts interposed between adjacent cylinders and .extending longitudinally of the polyhedron and transmissiom means extending transversely of the polyhedron and located centrally'of the ends thereof for inter- I connecting the crank shafts for operation in unison,of a blower located within the polyhedron and having a blower shaft disposed coaxial with the polyhedron, a starter disposed exteriorly of the polyhedron and connected tothe blower shaft, and means including speed transformation means for operatively connecting the blower shaftto the engine crank shafts. i
In testimony whereof, I have hereunto subscribed my name this 5th day of July, 1929,
' HERBERT T. HERB.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US379450A US1814802A (en) | 1929-07-19 | 1929-07-19 | Starting system for internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US379450A US1814802A (en) | 1929-07-19 | 1929-07-19 | Starting system for internal combustion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
US1814802A true US1814802A (en) | 1931-07-14 |
Family
ID=23497312
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US379450A Expired - Lifetime US1814802A (en) | 1929-07-19 | 1929-07-19 | Starting system for internal combustion engines |
Country Status (1)
Country | Link |
---|---|
US (1) | US1814802A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442838A (en) * | 1944-06-08 | 1948-06-08 | Chrysler Corp | Drive construction |
US2462492A (en) * | 1942-08-24 | 1949-02-22 | Hamel Georges Roger | Multicylinder engine |
US2486927A (en) * | 1945-01-06 | 1949-11-01 | American Locomotive Co | Engine frame construction |
US2498767A (en) * | 1944-06-19 | 1950-02-28 | Chrysler Corp | Gearing for driving coaxial shafts |
US2607328A (en) * | 1948-12-23 | 1952-08-19 | Jencick Stephen | Diesel motor |
DE864939C (en) * | 1942-08-24 | 1953-01-29 | Georges Roger Hamel | Polygon machines with rows of cylinders attached to a common frame |
US2645897A (en) * | 1949-04-11 | 1953-07-21 | Napier & Son Ltd | Reciprocating internal-combustion engine operating on the two-stroke cycle with exhaust turbine |
DE750439C (en) * | 1943-04-08 | 1954-04-05 | Schweizerische Lokomotiv | Two-stroke opposed piston internal combustion engine |
US2736301A (en) * | 1949-04-02 | 1956-02-28 | Kloeckner Humboldt Deutz Ag | Blower for cooling an internal-combustion engine and scavenging or supercharging |
US3359957A (en) * | 1966-04-15 | 1967-12-26 | Mantzel Albrecht-Wolfgang | Four cylinder two-stroke opposing piston internal combustion engine |
US4419969A (en) * | 1979-07-31 | 1983-12-13 | Bundrick Jr Benjamin | Flexible cylinder-head internal combustion engine with cylinder compression adjustable for use with available fluid fuels |
US20040237913A1 (en) * | 2003-05-30 | 2004-12-02 | Nanninga Jeffrey Karl | Nanninga diesel |
EP2758639A4 (en) * | 2011-09-23 | 2015-03-18 | Dale Pelfrey Trustee Of The R Dale Pelfrey Trust R | Internal combustion engine |
-
1929
- 1929-07-19 US US379450A patent/US1814802A/en not_active Expired - Lifetime
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2462492A (en) * | 1942-08-24 | 1949-02-22 | Hamel Georges Roger | Multicylinder engine |
DE864939C (en) * | 1942-08-24 | 1953-01-29 | Georges Roger Hamel | Polygon machines with rows of cylinders attached to a common frame |
DE750439C (en) * | 1943-04-08 | 1954-04-05 | Schweizerische Lokomotiv | Two-stroke opposed piston internal combustion engine |
US2442838A (en) * | 1944-06-08 | 1948-06-08 | Chrysler Corp | Drive construction |
US2498767A (en) * | 1944-06-19 | 1950-02-28 | Chrysler Corp | Gearing for driving coaxial shafts |
US2486927A (en) * | 1945-01-06 | 1949-11-01 | American Locomotive Co | Engine frame construction |
US2607328A (en) * | 1948-12-23 | 1952-08-19 | Jencick Stephen | Diesel motor |
US2736301A (en) * | 1949-04-02 | 1956-02-28 | Kloeckner Humboldt Deutz Ag | Blower for cooling an internal-combustion engine and scavenging or supercharging |
US2645897A (en) * | 1949-04-11 | 1953-07-21 | Napier & Son Ltd | Reciprocating internal-combustion engine operating on the two-stroke cycle with exhaust turbine |
US3359957A (en) * | 1966-04-15 | 1967-12-26 | Mantzel Albrecht-Wolfgang | Four cylinder two-stroke opposing piston internal combustion engine |
US4419969A (en) * | 1979-07-31 | 1983-12-13 | Bundrick Jr Benjamin | Flexible cylinder-head internal combustion engine with cylinder compression adjustable for use with available fluid fuels |
US20040237913A1 (en) * | 2003-05-30 | 2004-12-02 | Nanninga Jeffrey Karl | Nanninga diesel |
EP2758639A4 (en) * | 2011-09-23 | 2015-03-18 | Dale Pelfrey Trustee Of The R Dale Pelfrey Trust R | Internal combustion engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1814802A (en) | Starting system for internal combustion engines | |
US2768616A (en) | Two cycle opposed piston internal combustion engine | |
DE102011013567B4 (en) | Internal combustion engine with split cycle | |
DE3412283A1 (en) | TURBO COMPOSITE ENGINE | |
US2983264A (en) | Cam engine valve means | |
US2853983A (en) | Internal combustion engine of opposed piston type | |
US2401858A (en) | Exhaust mechanism for internalcombustion engines | |
US8381692B2 (en) | Internal combustion engine with exhaust-phase power extraction serving cylinder pair(s) | |
US1681910A (en) | Internal-combustion engine | |
US3180077A (en) | Wave machine to initiate scavenging of internal combustion | |
US2474879A (en) | Internal-combustion engine | |
US1593571A (en) | Power plant comprising a gas engine and turbine | |
US1662828A (en) | Two-stroke-cycle internal-combustion engine | |
US2345056A (en) | Internal combustion engine | |
US2082780A (en) | Internal combustion engine | |
US2056056A (en) | Engine cylinder | |
US1765716A (en) | Power plant | |
US2984966A (en) | Compound internal combustion engine | |
US2696343A (en) | Internal-combustion engine with compressor | |
US2346207A (en) | Two-cycle internal combustion engine | |
US1129393A (en) | Internal-combustion motor. | |
US2230308A (en) | Internal combustion engine | |
US1393831A (en) | Internal-combustion engine | |
US2180898A (en) | Internal combustion engine | |
US1468819A (en) | Internal-combustion engine |