US936409A - Internal-combustion engine. - Google Patents

Internal-combustion engine. Download PDF

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Publication number
US936409A
US936409A US39547407A US1907395474A US936409A US 936409 A US936409 A US 936409A US 39547407 A US39547407 A US 39547407A US 1907395474 A US1907395474 A US 1907395474A US 936409 A US936409 A US 936409A
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cylinder
cylinders
crank shaft
explosion
engine
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US39547407A
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Ellsworth Chapman
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/04Engines with variable distances between pistons at top dead-centre positions and cylinder heads
    • F02B75/048Engines with variable distances between pistons at top dead-centre positions and cylinder heads by means of a variable crank stroke length

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  • This invention relates to two-cycle internal the object of my improvements is, to provide an engine of this kind that shall have no springs or valves, and one in which the charge shall always' be compressed to the same density.
  • y invention consists in a two-cycle ex'- plosive engine
  • cranks either singly or 1n series, so constructed that the distance between the cylinder head and the center line of the crank shall be adjustable.
  • My invention further consists in a novel two cycle engine sition of the shaft with reference to the cylinder shall determine the amount of the explosive charge.
  • Figure l is a vertical cross sect-ion on the line A-B of Fig. 2.
  • Fig. 2 is a' longitudinal cross section of the cylinders on the line C D of Fig. 1.
  • Fig. 3 is a transverse vertical section on the line E-F of Fig. 2.
  • Fig. 4 is an elevation of the cylinders, looking at them from the upper side of Fig. 2.
  • the cylinders and their supporting flanges are shown attached to an engine bed.
  • the cylinders are formed in two parts, the upper cylinder 1 which is the explosion cylinder, and the lower cylinder 2 which is the compression cylinder. All the cylinders may be cast as one piece or sepa-
  • the cylinder heads 3 are v to the bed 7 of the engine.
  • Jackets 5 form circulating chambers around the explosion cylinders.
  • Flanges 6 connect An apron 8 is secured to the lower side of the bed and prevents waste of lubricating and fuel oils.
  • the ends 9 and cross bars l() of the bed form bearings for the eccentric sleeves 11 and 12. These sleeves are split, and on them are secured the gears 13.
  • These sleeves form the bearing for the crank shaft 14, which shaft is provided with crank pins 15.
  • Connecting rods 16 are pivoted on the crank pins and on ,the wrist pins 17 of the pistons.
  • the pistons have the parts 18 to fit the explosion cylinders and the parts 19 to lit the compression cylinders.
  • the compression cylinders are formed with ports 28, 31, and 34 which connect with the pipe 22 Awhich extends tothe carbureter. engine just above the compression cylinders is an exhaust pipe 24 which connects to the explosion cylinders through ports 25.
  • Conducting pipes between the compression chainber cylinder of one engine and the explosion cylinder of another are also formed on or secured to the cylinder casting. These pipes are three in number in the drawings and are shown in Fig. 2.
  • the conductor 26 extends from port 27 at the top of the left hand compression cylinder to the port 20 of the right hand explosion chamber.
  • The-conductor 29 extends from the port 30 at the top of the right hand compression cylinder tothe intake ports .21 of the middle-explosion cylinder, and the conductor 32 extends.
  • each of said cylinders having intake ports, a frame to support said cylinders, a crank shaft mounted in said frame, pistons adapted to reciprocate'within said cylinders, jconnections between crank shaft andl pistons, and means for controllin the distance between said crank shaft and intake ports whereby the admission of the explosive fluid into said cylinders may be controlled by said pistons.
  • An internal combustion engine comprising a cylinder having an inlet port, a piston adapted to cover and uncover the port, and means for adjusting the piston relative to the inlet port to vary the amount of charge admitted to the cylinder through the port.
  • An internal combustion engine comprising a cylinder having an inlet port, a piston in the cylinder adapted to close and open the port, a crank shaft, meansv connecting ,the piston and crank shaft, and means for adjusting the crank shaft and piston relative to the inlet port to vary the f amount of charge admitted to the cylinder.
  • An internal combustion engine comprising a cylinder having an inlet port, a piston in the cylinder, adaptedfto control the port, a crank shaft, means connecting the piston and crank shaft, rotatable members in which the kcrank shaft is eccentrically journaled, and means for rotating the members through the arc of a circle to vary the relation of the piston and inlet port.
  • An internal combustion engine comprising a cylinder having an inlet port, a piston in the cylinder adapted to control the port, a crank shaft, means connectingthe piston and which the crank shaft extends, rotatable members received in the journals, means for preventing endwise movement of the rotatable members, journaled in the members, and means for rotating the members to vary the relation of the piston and inlet port.
  • crank shaft eccentrically crank shaft journals through' prisinga cylinder having .an inlet port, a I
  • piston controlling the port,- and ineens for adjusting the piston and cylinder one relative to the other, to vary the speed of the engine.
  • a two-Cycle engine comprising a ey1in der having an inlet port therein, u, piston adapted. to Cover and uncover the inlet port7 ⁇ a crank shaft with which the piston is conneeted, rotatable bearings in which the shaft is eeeentrieally ournaiedyand means for ro- 10 tuting the bearings.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

E. CHAPMAN. INTERNAL GOMBUSTION ENGINE. AHLIUATION FILED o0T.z, 1907.
Patented Get. 12, 1909. 2 SHEETS-SHEET 1.
'FIC-iE- nnzut n 1:
A E. CHAPMAN.
INTERNAL GOMBUSTION ENGINE. APPLIOATION FILED 00T.2, 1907.
936 4:09. Patented Oct. 12, 1909, Z SHEETS-SHEET 2.
ilus
combustion engines, and
ELLswoRTH CHAPMAN,
OF PONTIAC, MICHIGAN.
INTERNAL-CMBUSTION ENGINE.
Specification of Letters Patent.
Patented Oct. 12, 1909.
Application filed October 2, 1907. Serial No. 395,474.
To' all whom it may concern:
Be it known that I, ELLswoRTH CHAPMAN, a citizen of the United States, and a resident of Pontiac, in the county of Oakland and State of Michigan, have invented a new and useful Internal-Combustion Engine, of which the following is a specification.
This invention relates to two-cycle internal the object of my improvements is, to provide an engine of this kind that shall have no springs or valves, and one in which the charge shall always' be compressed to the same density.
' rately as desired.
y invention consists in a two-cycle ex'- plosive engine,
with cylinders either singly or 1n series, so constructed that the distance between the cylinder head and the center line of the crank shall be adjustable.
My invention further consists in a novel two cycle engine sition of the shaft with reference to the cylinder shall determine the amount of the explosive charge.
I attain this object and embody the invention in the construction illustrated in the accompanying drawings, in which Figure l is a vertical cross sect-ion on the line A-B of Fig. 2. Fig. 2 is a' longitudinal cross section of the cylinders on the line C D of Fig. 1. Fig. 3 is a transverse vertical section on the line E-F of Fig. 2. Fig. 4 is an elevation of the cylinders, looking at them from the upper side of Fig. 2.
Similar parts throughout the several views.
v In two cycle engines, thecharge is coinpressed before being admitted into the explosion cylinder and the rush of such admission forces out the burned gases of the previous explosion. In the present construction means are shown for compressing charges for each of several cylinders independently and for compressing the exact amount of explosive mixture desired. The amount of vapor which is admitted to the explosion cylinder is determined by the relative positions of the crank shaft and the explosion cylinder. n
In the drawings, the cylinders and their supporting flanges are shown attached to an engine bed. The cylinders are formed in two parts, the upper cylinder 1 which is the explosion cylinder, and the lower cylinder 2 which is the compression cylinder. All the cylinders may be cast as one piece or sepa- The cylinder heads 3 are v to the bed 7 of the engine.
so constructed that the poreference characters refer to like provided with openings 4, to receive the spark plugs, and the usual water passages. Jackets 5 form circulating chambers around the explosion cylinders. Flanges 6 connect An apron 8 is secured to the lower side of the bed and prevents waste of lubricating and fuel oils. The ends 9 and cross bars l() of the bed form bearings for the eccentric sleeves 11 and 12. These sleeves are split, and on them are secured the gears 13. These sleeves form the bearing for the crank shaft 14, which shaft is provided with crank pins 15. Connecting rods 16 are pivoted on the crank pins and on ,the wrist pins 17 of the pistons. The pistons have the parts 18 to fit the explosion cylinders and the parts 19 to lit the compression cylinders. The compression cylinders are formed with ports 28, 31, and 34 which connect with the pipe 22 Awhich extends tothe carbureter. engine just above the compression cylinders is an exhaust pipe 24 which connects to the explosion cylinders through ports 25. Conducting pipes between the compression chainber cylinder of one engine and the explosion cylinder of another are also formed on or secured to the cylinder casting. These pipes are three in number in the drawings and are shown in Fig. 2. The conductor 26 extends from port 27 at the top of the left hand compression cylinder to the port 20 of the right hand explosion chamber. The-conductor 29 extends from the port 30 at the top of the right hand compression cylinder tothe intake ports .21 of the middle-explosion cylinder, and the conductor 32 extends. from the port 33 at the top of the middle compression cylinder to the intake ports 35 of the left hand explosion cylinder. The size of these Formed on or secured to the ports will be determined `by the cxplosive mixture and by the speed the engine is to run. Journaled in the bed is a shaft 36 having a gear 37 secured to it for each'gear 13 on the eccentric sleeves 11 and l2. It will be seen that upon turning this shaft 36 all the sleeves 11 and 12 will also turn and the distance between the cylinder heads 3 and the crank shaft 14 may thereby be regulated. The upper ends of the pistons arev cut out, as shown in Fig. 3, in order vto deflect the explosion charge upward and to permit the escape of the burned gases through the exhaust ports. When the parts are in normal position, the
-engines will draw full charge into the comgases.
Y explosion chambers pression chambers, and as the crank pins are so positioned that the pin of the left hand engine, Figs. 1 and 2, is 120 degrees in ad- Vance of the pin of the right hand engine, the compression piston 19 of the left hand cylinder will have completed its compression and the maxlmum pressure will have traveled to the intake port 20 before this ort of the right hand cylinder 1 is opened. sult will be that the compressed explosive mixture will rush in and displacethe burned Having the cranks separated 120 degrees always gives full compression in the conducting pipes 26, 29 and 82 at the opening at the intake ports, permitting the blast of ex losive mixture to flow up against the cylin er head before spreading, resulting in a more complete cleaning out of the burned gases. taken into the cylinders, depends largely upon the size of the intake ports. If the eccentric sleeves 11 and 12 are turned from the positions shown, the distance between the center line of the crank shaft and the ports will ,be lessened. This will result in the intake ports of both compression and explosion cylinders being 'opened both a less amount and for a less period of time. The amount of vapor that passes vintothe compression and explosion cylinders will there'- fore be reduced. At the same time the Edistance betwen the crank shaft and the ports is reduced, the distance between the crank shaft and the cylinder heads will also be reduced. As the length of the reciprocating parts remains constant, the dimensions of the at the upper end of the .explosion cylinders will vary with the size of the ports and the quantity of the explosive mixture. of the explosive mixture will remain practically constant at the time of explosion, resulting in an economical use of the fuel which is ynot possible with a delayed spark or with slight compression owing to throttling the intake.
Having now -explained my improvement, what I claim as my invention and desire to secure by Letters Patent is :--4
1. In an internal combustion engine, the combination of a compression cylinder, an explosion cylinder, each of said cylinders having intake ports, a frame to support said cylinders, a crank shaft mounted in said frame, pistons adapted to reciprocate'within said cylinders, jconnections between crank shaft andl pistons, and means for controllin the distance between said crank shaft and intake ports whereby the admission of the explosive fluid into said cylinders may be controlled by said pistons.
2. In an explosion engine, the combination of a frame, a series of eccentric sleeves rotatably mounted 1n sald frame, means for revolving said sleeves, a crank shaft journaled he re-.-
The amounty of explosive vapor, j
The result is, that the density.
in said sleeves and provided with a number of cranks evenly spaced, a series of compression cylinders mounted on said frame, a series of explosion cylinders adjacent to said compression cylinders said cylinders having intake and exhaust ports, and pistons connected to said cranks, the admission of explosive gases to said cylinders being controlled by the position of said crank shaft through said pistons.
3. The combination with a cylinder having an inlet port anda piston adapted to open and close said port, of means for adjusting the cylinder and piston, one relative to the other to vary the amount of charge admitted to the cylinder through the inlet port.
4. An internal combustion engine comprising a cylinder having an inlet port, a piston adapted to cover and uncover the port, and means for adjusting the piston relative to the inlet port to vary the amount of charge admitted to the cylinder through the port.
5.' An internal combustion engine comprising a cylinder having an inlet port, a piston in the cylinder adapted to close and open the port, a crank shaft, meansv connecting ,the piston and crank shaft, and means for adjusting the crank shaft and piston relative to the inlet port to vary the f amount of charge admitted to the cylinder.
6. An internal combustion engine comprising a cylinder having an inlet port, a piston in the cylinder, adaptedfto control the port, a crank shaft, means connecting the piston and crank shaft, rotatable members in which the kcrank shaft is eccentrically journaled, and means for rotating the members through the arc of a circle to vary the relation of the piston and inlet port.
7 An internal combustion engine comprising a cylinder having an inlet port, a piston in the cylinder adapted to control the port, a crank shaft, means connectingthe piston and which the crank shaft extends, rotatable members received in the journals, means for preventing endwise movement of the rotatable members, journaled in the members, and means for rotating the members to vary the relation of the piston and inlet port.
8. An internal combustion engine comthe crank shaft eccentrically crank shaft, journals through' prisinga cylinder having .an inlet port, a I
piston in the cylinder, adapted to control the port, a crank shaft, means connecting the iston and crank shaft, split sleeves rotataly mounted in the engine, in which sleeves the crank shaft `is eccentrically journaled, I
piston controlling the port,- and ineens for adjusting the piston and cylinder one relative to the other, to vary the speed of the engine.
10. A two-Cycle engine comprising a ey1in der having an inlet port therein, u, piston adapted. to Cover and uncover the inlet port7` a crank shaft with which the piston is conneeted, rotatable bearings in which the shaft is eeeentrieally ournaiedyand means for ro- 10 tuting the bearings. v
In testimony whereof, I have signed this specification in the presence of two subseribing Witnesses.
ELLSVORTH CHAPMAN. Vitnessesz ELIZABETH M. BROWN,
EDWARD N. PAGELSEN.
US39547407A 1907-10-02 1907-10-02 Internal-combustion engine. Expired - Lifetime US936409A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025840A (en) * 1957-04-10 1962-03-20 Casini Carlo Romano Carburetion engine with variablevolume combustion chamber
US6247430B1 (en) * 1997-10-31 2001-06-19 Fev Motorentechnik Gmbh & Co. Kommandgesellschaft Compression ratio setting device for an internal-combustion engine
US6260532B1 (en) 1998-09-28 2001-07-17 Edward Charles Mendler Rigid crankshaft cradle and actuator
US6443107B1 (en) 1999-05-27 2002-09-03 Edward Charles Mendler Rigid crankshaft cradle and actuator
US6637384B1 (en) 1999-11-12 2003-10-28 Edward Charles Mendler Rigid crankshaft cradle and actuator

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025840A (en) * 1957-04-10 1962-03-20 Casini Carlo Romano Carburetion engine with variablevolume combustion chamber
US6247430B1 (en) * 1997-10-31 2001-06-19 Fev Motorentechnik Gmbh & Co. Kommandgesellschaft Compression ratio setting device for an internal-combustion engine
US6260532B1 (en) 1998-09-28 2001-07-17 Edward Charles Mendler Rigid crankshaft cradle and actuator
US6443107B1 (en) 1999-05-27 2002-09-03 Edward Charles Mendler Rigid crankshaft cradle and actuator
US6637384B1 (en) 1999-11-12 2003-10-28 Edward Charles Mendler Rigid crankshaft cradle and actuator

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