US2058350A - Two-stroke internal combustion engine - Google Patents

Two-stroke internal combustion engine Download PDF

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US2058350A
US2058350A US73945A US7394536A US2058350A US 2058350 A US2058350 A US 2058350A US 73945 A US73945 A US 73945A US 7394536 A US7394536 A US 7394536A US 2058350 A US2058350 A US 2058350A
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cylinder
air
transfer passage
port
exhaust
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Petter Percival Waddams
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Petters Ltd
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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
    • F02B25/00Engines characterised by using fresh charge for scavenging cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2700/00Measures relating to the combustion process without indication of the kind of fuel or with more than one fuel
    • F02B2700/03Two stroke engines
    • F02B2700/031Two stroke engines with measures for removing exhaust gases from the cylinder

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  • This invention relates to two-stroke internal combustion engines and has for its main object to provide an improved construction of the kind in which the suction eifect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the cylinder.
  • Another object of the present invention is to overcome difiiculty arising in such cases.
  • a two-stroke internal combustion engine ac- I cording to the present invention is furnished with an air inlet port or ports in the cylinder wall, and a transfer passage through which the said air inlet port or ports, or a port or ports in the cylinder wall and independent of the said air inlet,
  • port or ports in the cylinder wall are in open communication with the crank case into which air is drawn and compressed without intermission at all engine speeds, air being supplied to the cylinder not only indirectly from the crank case through the transfer passage but also directly through the said air inlet ports from an external source, that is to say without previous compression in the crank case.
  • the exhaust gases are preferably discharged from the working chamber through an exhaust port in the cylinder head and controlled by a positively operated exhaust valve, the air being conveniently supplied to the cylinder through a set of air inlet ports which substantially completely surround the cylinder.
  • the air inlet port or ports are in open communication, through the transfer passage, with the crank case, and a breather port is provided controlled by a non-return valve past which air can flow from the atmosphere to the air inlet port or ports and to the transfer passage, the crank case being sealed so that crank case compression takes place at all engine speeds.
  • Figure 3 is a sectional plan on the line III-III of Figure 1, but with the outer casing of the cylinder omitted,
  • Figure 4 is a view similar to that shown in Figure 1 but of a modified construction
  • Figure 5 is a sectional plan through the cylinder ports of Figure 3.
  • the exhaust port B is arranged in a combustion chamber or pocket C whose diameter is less than that of the cylinder bore, say, approximately two-thirds of the internal diameter of the cylinder A, the "fuel being inzu jected tangentially into the combustion chamber 0 by a fuel injection device indicated at C
  • the piston A is connected by a connecting rod A to a crankshaft A, the crank case A being sealed for the purpose hereinafter described.
  • the gallery D is furnished with a breather port D which is controlled by a pressure operated non-return valve D of.
  • the exhaust valve B is positively operated through a rocking lever E from a tappet rod E longitudinally movable in a porthole A formed by a sleeve E passing through the gallery D the rod E bearing at its lower end on a plunker E which bears directly on a cam E driven from the crankshaft of the engine.
  • the cylinder is surrendered by an outer casing E which is provided with a suitable opening or openings for the ad-
  • the casing E may mission of air to the port D act as an air intake silencer.
  • the timing of the exhaust valve B and the opening of the air inlet ports D and the length of the exhaust conduit B are such that at normal 55.
  • each exhaust period substantially coincides with an outward pressure surge in the exhaust pipe B
  • the exhaust system may comprise a pipe of substantially constant cross-sectional area and approximately 9 feet in length connected directly to the exhaust port B and leading to an expansion chamber or to the atmosphere or to a further pipe the cross-sectional area of .which increases progressively towards its outlet end.
  • the exhaust valve 28 is opened soon after the piston A has passed its mid-position during the firing stroke, say, 86 of crank angle before the outer dead centre.
  • the outward pressure surge which then takes place in. the exhaust conduit 18 evacuates and produces a depression in the cylinder A.
  • the piston A uncovers the air inlet ports D before the end of the flring stroke, say, 45 prior to the outer dead centre.
  • the air charge now rushes into the previously evacuated cylinder, rotating therein due to the tangential arrangement of the air inlet ports D/and scavenges andrecharges the cylinder A with a rotating. charge.
  • both the exhaust port B and the air inlet ports D are closed substantially simultaneously and before the return pressure surge in the exhaust conduit 25 reaches the exhaust port 3*.
  • the compression stroke now continues, the fuel being injected, say 18 of crank angle before the inner dead centre.
  • each induction period takes place only during an outward pressure surge in the exhaust conduit B and the return of the exhaust gases from the conduit B due to an inward pressure surge is prevented.
  • the eifect produced by the exhaust gases flowing from the cylinder A through the exhaust conduit B may not be sumcient to ensure effective evacuation, scavenging and recharging of the working chamber.
  • crank case A which is sealed as above indicated, is permanently in open communication with the gallery D through an air transfer passage F the cross-section of which is restricted so as to be less than the cross-section available for the flow of air through the breather port D when the non-return valve D is open.
  • the upper end of the transfer passage F leads into the gallery 13 at a point adjacent to the breather port D
  • the effect created by the exhaust gas flowing out through the exhaust pipe B will cause a depression within the cylinder A so that when the air inlet ports D are uncovered by the piston A the non-return valve D opens and air flows directly from the atmosphere past the non-return valve D and through the air admission.
  • crank case compression takes 'place without intermission at all engine speeds and the delivery of air from the crank case A through the transfer passage F is not therefore interrupted even when the normal engine speed has been attained, the necessary air will, at normal running speeds, flow directly from the atmosphere past the non-return valve D to the air inlet ports D.
  • the suction effect created by the exhaust gases flowing out of the working chamber through the exhaust pipe D is not sumcient to induce the air necessary for effectively scavenging and recharging the working chamber, the necessary air is still supplied under pressure from the crank case A through the transfer passage F.
  • crank case G is furnished with a breather port G automatically controlled by a non-return valve G.
  • the crank chamber communicates through a transfer passage H with a chamber H isolated from the chamber J from which the air, flowing from the atmosphere past a nonreturn valve J enters the cylinders through main air inlet ports J and tangential passages similar to those described with reference to Figure 3.
  • a nonreturn valve J enters the cylinders through main air inlet ports J and tangential passages similar to those described with reference to Figure 3.
  • the suction effect of the exhaust gases flowing out of the cylinder may be insuflicient to induce suflicient air through the main air inlet ports J, the delivery of air continues from the crank chamber through the auxiliary ports K thereby ensuring satisfactory scavenging and recharging of the cylinder.
  • a cylinder having at least one air inlet port in the wall thereof and at least one exhaust port, a piston arranged to reciprocate wi hin the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with a port in the least one exhaust port, a non-return valve past.
  • a cylinder having at least one main inlet port in the wall thereof and at least one exhaust port, a piston arranged to reciprocate within the cylinder, a crank chamber having a breather port, and a non-return valve past which air can fiow'from the atmosphere through the said breather port into the crank chamberwhich is in open communication, through a transfer passage, with at least one auxiliary air inlet port in the cylinder wall and independent of the said main air inlet port, air being supplied to the cylinder not only directly through the main air inlet port in the cylinder wall from an external source, but also indirectly from the crank chamber through the transfer passage and auxiliary air inlet port, air being drawn past the nonreturn valve into the crank case, compressed therein and delivered to the auxiliary inlet port without intermission at all engine speeds.
  • a cylinder having at least one air inlet port in the wall thereof and at least one exhaust port, a piston arranged to recip'rocate within the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with the said air inlet port in the cylinder wall, air being supplied to the cylinder not only indirectly from the crank chamber through the transfer passage to the air inlet port, but also directly through the said air inlet port from an external source.
  • a cylinder having at least one inlet port in the wall thereof and at least one exhaust port, a non-return valve past which air can flow from the atmosphere to the said inlet port, a'piston arranged to reciprocate within the cylinder, and a sealed crank chamber in open communication, through a transfer passage, with the said inlet port in the cylinder wall, air being drawn past the non-return valve not only into the cylinder but also through the transfer paschamber
  • a cylinder having at least one inlet port in the wall thereof and at least one exhaust port, a non-return valve past which air can flow from the atmosphere to the said inlet port, a piston arranged to reciprocate within the cylinder, and a sealed crank chamber in open communication with the said air inlet port in the cylinder wall through a transfer passage the cross-section available for the
  • a cylinder having at least one air inlet port in the wall thereof and at least one exhaust port in the cylinder head, a positively operated exhaust valve controlling the said exhaust p'ort, a piston arranged to reciprocate within the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with the said air inlet port in the cylinder wall, air being supplied to the cylinder not only indirectly from the crank chamber through the transfer passage to the air inlet port, but also directly through the said air inlet port from an external source.
  • a cylinder having air inlet ports in the cylinder wall and extending substantially completely around the cylinder and an exhaust port, a piston arranged to reciprocate within the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with at least one port in the cylinder wall, air flowing into the cylinder not only indirectly from the crank chamber through the transfer passage but. also directly through the inlet port in the cylinder wall from an external source.
  • a cylinder having air inlet ports in the wall thereof and-extending substantially completely around the cylinder and at least one exhaust port, a non-return valve past which air can flow from the atmosphere to the said inlet ports, a piston arranged to reciprocate within the cylinder, and a sealed crank.
  • a cylinder having main air inlet ports in the wall thereof and extending substantially completely around the cylinder in the wall thereof and at least one exhaust port, a piston arranged to reciprocate within the cylinder, a crank chamber having a breather port, and 'a non-return valve past which air can flow from the atmosphere through the said breather port, the crank chamber being in open communication, through a transfer passage, with at least one auxiliary air inlet port in the cylinder wall and independent of the said main air inlet port, air flowing to the cylinder not only directly through the 'main air inlet port in the cylinder wall from an external source, but also indirectly from the crank chamber through the transfer passage and auxiliary air inlet port, air being drawn past the non-return valve into the crank case, compressed therein and delivered to the auxiliary air inlet port without intermission at all

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)

Description

Oct. 20, 1936. P. w. PETTER TWO-STROKE INTERNAL COMBUSTION ENGINE 3 Sheets-Sheet 1 Filed April -11, 1936 Fig 1.
Oct. 20, 1936. w p -i' 2,058,350
TWO-STROKE INTERNAL COMBUSTION ENGINE Filed April 11, 1936 3 Sheets-Sheet 2 Fig.2.
ATTORNEW Oct. 20, 1936. P. w. PETTER TWO-STROKE INTERNAL COMBUSTION ENGINE.
Filed April 11, 1936 3 Sheets-Sheet 5 Patented Oct. 20, 1936 UNITED STATES 2,058,350 TWO-STROKE INTERNAL COMBUSTION ENG NE Percival Waddams Petter, Stoke-Bub-Hamdon,
England, assignor to Petters England, a company of Great Limited, Yeovil,
Britain Application April 11, 1936, Serial No. 73,945 In Great Britain April 25, 1935 12 Claims. (Cl. 123-65) This invention relates to two-stroke internal combustion engines and has for its main object to provide an improved construction of the kind in which the suction eifect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the cylinder.
When an engine of this type is being started, that is to say is operating at low speed, the suction eilect of the outflowing exhaust gases may not be enough to ensure emcient evacuation, scavenging and induction of the new charge. This diillculty may arise also when the engine is desired occasionally to deal with peak loads causing a temporary reduction in speed. Another object of the present invention is to overcome difiiculty arising in such cases.
A two-stroke internal combustion engine ac- I cording to the present invention is furnished with an air inlet port or ports in the cylinder wall, and a transfer passage through which the said air inlet port or ports, or a port or ports in the cylinder wall and independent of the said air inlet,
port or ports in the cylinder wall, are in open communication with the crank case into which air is drawn and compressed without intermission at all engine speeds, air being supplied to the cylinder not only indirectly from the crank case through the transfer passage but also directly through the said air inlet ports from an external source, that is to say without previous compression in the crank case. The exhaust gases are preferably discharged from the working chamber through an exhaust port in the cylinder head and controlled by a positively operated exhaust valve, the air being conveniently supplied to the cylinder through a set of air inlet ports which substantially completely surround the cylinder.
Preferably, however, the air inlet port or ports are in open communication, through the transfer passage, with the crank case, and a breather port is provided controlled by a non-return valve past which air can flow from the atmosphere to the air inlet port or ports and to the transfer passage, the crank case being sealed so that crank case compression takes place at all engine speeds.
The in ention may be applied to engines of the vaporized charge spark ignition type or to engines of the compression ignition type, but one construction according to the invention and as applied to an engine of the compression ignition type is illustrated by wayof example in the accompanying drawings, in which Figure 1 illustrates the engine partly in vertical section in a plane containing the crankshaft, Figure 2 is a vertical section at right angles to the crankshaft,
Figure 3 is a sectional plan on the line III-III of Figure 1, but with the outer casing of the cylinder omitted,
Figure 4 is a view similar to that shown in Figure 1 but of a modified construction, and
Figure 5 is a sectional plan through the cylinder ports of Figure 3.
In the'construction illustrated in Figures 1, 2,
and time engine comprises a cylinder A in the head B of which is provided an exhaust port 3 controlled by a positively operated poppet valve 3*, the exhaust port B communicating with an ,15
exhaust pipe or conduit B The exhaust port B is arranged in a combustion chamber or pocket C whose diameter is less than that of the cylinder bore, say, approximately two-thirds of the internal diameter of the cylinder A, the "fuel being inzu jected tangentially into the combustion chamber 0 by a fuel injection device indicated at C The piston A is connected by a connecting rod A to a crankshaft A, the crank case A being sealed for the purpose hereinafter described. Arranged into the internal combustion chamber C by the fuel injection device C The gallery D is furnished with a breather port D which is controlled by a pressure operated non-return valve D of. the plate type so that air can be drawn from the atmosphere through the breather port D past the 40 non-return valve D into the gallery D The exhaust valve B is positively operated through a rocking lever E from a tappet rod E longitudinally movable in a porthole A formed by a sleeve E passing through the gallery D the rod E bearing at its lower end on a plunker E which bears directly on a cam E driven from the crankshaft of the engine. The cylinder is surrendered by an outer casing E which is provided with a suitable opening or openings for the ad- The casing E may mission of air to the port D act as an air intake silencer.
The timing of the exhaust valve B and the opening of the air inlet ports D and the length of the exhaust conduit B are such that at normal 55.
The passages leading to the air 30 speed, or within the normal speed range of the engine, each exhaust period substantially coincides with an outward pressure surge in the exhaust pipe B Thus, for example, for an engine having a bore of 4 inches and a stroke of 6 inches and the normal speed of which is to be in the region of 1,000 revolutions per minute, the exhaust system may comprise a pipe of substantially constant cross-sectional area and approximately 9 feet in length connected directly to the exhaust port B and leading to an expansion chamber or to the atmosphere or to a further pipe the cross-sectional area of .which increases progressively towards its outlet end.
The exhaust valve 28 is opened soon after the piston A has passed its mid-position during the firing stroke, say, 86 of crank angle before the outer dead centre. The outward pressure surge which then takes place in. the exhaust conduit 18 evacuates and produces a depression in the cylinder A. The piston A uncovers the air inlet ports D before the end of the flring stroke, say, 45 prior to the outer dead centre. The air charge now rushes into the previously evacuated cylinder, rotating therein due to the tangential arrangement of the air inlet ports D/and scavenges andrecharges the cylinder A with a rotating. charge.
' On the succeeding compression stroke, say, 45 of crank angle after the outer dead centre, both the exhaust port B and the air inlet ports D are closed substantially simultaneously and before the return pressure surge in the exhaust conduit 25 reaches the exhaust port 3*. The compression stroke now continues, the fuel being injected, say 18 of crank angle before the inner dead centre.
At normal speeds of the engine therefore each induction period takes place only during an outward pressure surge in the exhaust conduit B and the return of the exhaust gases from the conduit B due to an inward pressure surge is prevented. At low speeds or during starting, however, the eifect produced by the exhaust gases flowing from the cylinder A through the exhaust conduit B may not be sumcient to ensure effective evacuation, scavenging and recharging of the working chamber.
With a view to overcoming this diiilculty the crank case A which is sealed as above indicated, is permanently in open communication with the gallery D through an air transfer passage F the cross-section of which is restricted so as to be less than the cross-section available for the flow of air through the breather port D when the non-return valve D is open. As shown, the upper end of the transfer passage F leads into the gallery 13 at a point adjacent to the breather port D At normal speeds of the engine the effect created by the exhaust gas flowing out through the exhaust pipe B will cause a depression within the cylinder A so that when the air inlet ports D are uncovered by the piston A the non-return valve D opens and air flows directly from the atmosphere past the non-return valve D and through the air admission. ports D into the cylinder, the air rotating within the .cylinder in the direction of the arrow shown in Figure 3, that is to say the'same direction as that in which the fuel is injected by the device C At low engine speeds or during starting when the effect of the exhaust gases flowingout through the exhaust pipes B- may not be sufficient to cause induction of sufficient air past the non-return valve D air is drawn during the instroke oi the piston A past the non-return valve D and through the transfer passage F into the crank case A. On the succeeding outstroke of the piston A this air is compressed in the crank case and is delivered -under pressure through the transfer passage F and air inlet ports D into the cylinder.
Thus, though crank case compression takes 'place without intermission at all engine speeds and the delivery of air from the crank case A through the transfer passage F is not therefore interrupted even when the normal engine speed has been attained, the necessary air will, at normal running speeds, flow directly from the atmosphere past the non-return valve D to the air inlet ports D. During starting and low engine speeds however when the suction effect created by the exhaust gases flowing out of the working chamber through the exhaust pipe D is not sumcient to induce the air necessary for effectively scavenging and recharging the working chamber, the necessary air is still supplied under pressure from the crank case A through the transfer passage F.
It will therefore be seen that effective scavenging and recharging of the working chamber is ensured throughout the speed range of the engine whilst the necessity for providing either additional apparatus for supplying air to the engine or means for interrupting the supply of air from the crank case through the transfer passage to the cylinder is obviated. Since, in some instances, there may be a tendency for lubricant to find its way from the crank case through the transfer passage to the air inlet ports, means such for example as a battle or bames may be provided, say, in the transfer passage or between the transfer passage and the crank case, for the purpose of preventing the upward flow of lubricant from the crank case through the transfer passage.
In the construction illustrated in Figures 4 and 5 the crank case G is furnished with a breather port G automatically controlled by a non-return valve G. The crank chamber communicates through a transfer passage H with a chamber H isolated from the chamber J from which the air, flowing from the atmosphere past a nonreturn valve J enters the cylinders through main air inlet ports J and tangential passages similar to those described with reference to Figure 3. During normal running air enters the-cylinder not only directly from the atmosphere through the main air inlet ports J but also indirectly, under pressure, from the crank chamberthrough the transfer passage H and auxiliary ports K in the cylinder wall. Though at low engine speeds, however, the suction effect of the exhaust gases flowing out of the cylinder may be insuflicient to induce suflicient air through the main air inlet ports J, the delivery of air continues from the crank chamber through the auxiliary ports K thereby ensuring satisfactory scavenging and recharging of the cylinder.
What I claim as my invention and desire to secure by Letters Patent is:-
1. In a two-stroke internal combustion engine of the type in which the suction effect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having at least one air inlet port in the wall thereof and at least one exhaust port, a piston arranged to reciprocate wi hin the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with a port in the least one exhaust port, a non-return valve past.
which air can flow from the atmosphere to the said inlet port, a piston arranged to reciprocate within the cylinder, and a sealed crank chamber in open communication, through a transfer passage, with a port 'in the cylinder'wall, air flowing past the non-return valve not only into the cylinder but also through the transfer passage into thecrank chamber and from which air is delivered back under pressure through the transfer passage to the cylinder, the air being thus drawn into and delivered from the crankchamber within open communication with a port in the cylinder wall through a transfer passage the crosssection available for the flow of air through which is less than the cross-section available for the flow of air past the non-return valve when this is open, air flowing past the non-return valve not only into the cylinder but also through the transfer passage into the crank chamber from which air is delivered back under pressure through the transfer passage to the cylinder, the air being thus drawn into and delivered from the crank chamber without intermission at all engine speeds.
4. In a two-stroke internal combustion engine,
of the type in which the suction eifect created by the exhaust gases flowing out of .the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having at least one main inlet port in the wall thereof and at least one exhaust port, a piston arranged to reciprocate within the cylinder, a crank chamber having a breather port, and a non-return valve past which air can fiow'from the atmosphere through the said breather port into the crank chamberwhich is in open communication, through a transfer passage, with at least one auxiliary air inlet port in the cylinder wall and independent of the said main air inlet port, air being supplied to the cylinder not only directly through the main air inlet port in the cylinder wall from an external source, but also indirectly from the crank chamber through the transfer passage and auxiliary air inlet port, air being drawn past the nonreturn valve into the crank case, compressed therein and delivered to the auxiliary inlet port without intermission at all engine speeds.
5. In a two-stroke internal combustion engine of the type in which the suction eflect created by the exhaust gases flowing out of the worldng chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having at least one air inlet port in the wall thereof and at least one exhaust port, a piston arranged to recip'rocate within the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with the said air inlet port in the cylinder wall, air being supplied to the cylinder not only indirectly from the crank chamber through the transfer passage to the air inlet port, but also directly through the said air inlet port from an external source.
6. In a two-stroke internal combustion engine of the type in which the suction effect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having at least one inlet port in the wall thereof and at least one exhaust port, a non-return valve past which air can flow from the atmosphere to the said inlet port, a'piston arranged to reciprocate within the cylinder, and a sealed crank chamber in open communication, through a transfer passage, with the said inlet port in the cylinder wall, air being drawn past the non-return valve not only into the cylinder but also through the transfer paschamber, in combination, a cylinder having at least one inlet port in the wall thereof and at least one exhaust port, a non-return valve past which air can flow from the atmosphere to the said inlet port, a piston arranged to reciprocate within the cylinder, and a sealed crank chamber in open communication with the said air inlet port in the cylinder wall through a transfer passage the cross-section available for the flow of air through which is less than the cross-section available for the flow of air past the non-return valve, air flowing past the non-return valve not only into the cylinder but also through the transferpassage into the crank chamber from which air is delivered back under pressure through the transfer passage to the cylinder, the air being thus drawninto and delivered from the crank chamber without intermission at all engine speeds.
8. In a two-stroke internal combustion engine of the type in which the suction efiect created by the exhaust gases flowing out of the working chamber is utilized during normal running to inbeing in open communication, through a transfer passage, with at least one port in the cylinder wall,
air being supplied to the cylinder not only indirectly fronr the crank chamber through the transfer passage but also directly through the inlet port in the cylinder wall from an external source.
9. In a two-stroke internal combustion engine of the type in which the suction eilect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having at least one air inlet port in the wall thereof and at least one exhaust port in the cylinder head, a positively operated exhaust valve controlling the said exhaust p'ort, a piston arranged to reciprocate within the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with the said air inlet port in the cylinder wall, air being supplied to the cylinder not only indirectly from the crank chamber through the transfer passage to the air inlet port, but also directly through the said air inlet port from an external source.
10. In a two-stroke internal combustion engine of the type in which the suction eifect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having air inlet ports in the cylinder wall and extending substantially completely around the cylinder and an exhaust port, a piston arranged to reciprocate within the cylinder, and a crank chamber into which air is drawn and compressed without intermission at all engine speeds, the crank chamber being in open communication, through a transfer passage, with at least one port in the cylinder wall, air flowing into the cylinder not only indirectly from the crank chamber through the transfer passage but. also directly through the inlet port in the cylinder wall from an external source.
11. In a two-stroke internal. combustion engine of the type in which the suction effect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having air inlet ports in the wall thereof and-extending substantially completely around the cylinder and at least one exhaust port, a non-return valve past which air can flow from the atmosphere to the said inlet ports, a piston arranged to reciprocate within the cylinder, and a sealed crank. chamber in open communication, through a transfer passage, with a port in the cylinder wall, air flowing past the non-return valve not only into the cylinder but also through the transfer passage to the crank chamber from which air is delivered back under pressure through the transfer passage to the cylinder, the air being thus drawn into and delivered from the crank chamber without intermission at all engine speeds.
12. In a two-stroke internal combustion engine of the type in which the suction efiect created by the exhaust gases flowing out of the working chamber is utilized during normal running to induce the succeeding charge into the working chamber, in combination, a cylinder having main air inlet ports in the wall thereof and extending substantially completely around the cylinder in the wall thereof and at least one exhaust port, a piston arranged to reciprocate within the cylinder, a crank chamber having a breather port, and 'a non-return valve past which air can flow from the atmosphere through the said breather port, the crank chamber being in open communication, through a transfer passage, with at least one auxiliary air inlet port in the cylinder wall and independent of the said main air inlet port, air flowing to the cylinder not only directly through the 'main air inlet port in the cylinder wall from an external source, but also indirectly from the crank chamber through the transfer passage and auxiliary air inlet port, air being drawn past the non-return valve into the crank case, compressed therein and delivered to the auxiliary air inlet port without intermission at all engine speeds.
PERCIVAL WADDAMS PETIER.
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US2484009A (en) * 1948-02-25 1949-10-11 Texas Co Internal-combustion engine and method of operating same
DE966044C (en) * 1951-06-15 1957-07-04 Texaco Development Corp Method for operating a two-stroke internal combustion engine
US3161173A (en) * 1962-12-31 1964-12-15 John J Horan Water craft and propulsion means therefor
US20110030647A1 (en) * 2009-08-07 2011-02-10 Suzuki Motor Corporation Internal combustion engine
US20110041799A1 (en) * 2009-08-20 2011-02-24 Cleeves James M High Swirl Engine
US20120073536A1 (en) * 2009-06-08 2012-03-29 Crosset Leon Internal combustion engine with spherical rotary valve
US20120174881A1 (en) * 2010-12-14 2012-07-12 Taylor Jack R Full expansion internal combustion engine
US8561581B2 (en) 2009-08-04 2013-10-22 Jack R. Taylor Two-stroke uniflow turbo-compound internal combustion engine
US8973539B2 (en) 2010-12-14 2015-03-10 Jack R. Taylor Full expansion internal combustion engine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2484009A (en) * 1948-02-25 1949-10-11 Texas Co Internal-combustion engine and method of operating same
DE966044C (en) * 1951-06-15 1957-07-04 Texaco Development Corp Method for operating a two-stroke internal combustion engine
US3161173A (en) * 1962-12-31 1964-12-15 John J Horan Water craft and propulsion means therefor
US20120073536A1 (en) * 2009-06-08 2012-03-29 Crosset Leon Internal combustion engine with spherical rotary valve
US8561581B2 (en) 2009-08-04 2013-10-22 Jack R. Taylor Two-stroke uniflow turbo-compound internal combustion engine
US8448623B2 (en) * 2009-08-07 2013-05-28 Suzuki Motor Corporation Internal combustion engine
US20110030647A1 (en) * 2009-08-07 2011-02-10 Suzuki Motor Corporation Internal combustion engine
EP2467586A2 (en) * 2009-08-20 2012-06-27 Pinnacle Engines, Inc. High swirl engine
US20110041799A1 (en) * 2009-08-20 2011-02-24 Cleeves James M High Swirl Engine
EP2467586A4 (en) * 2009-08-20 2014-10-08 Pinnacle Engines Inc High swirl engine
US9194288B2 (en) * 2009-08-20 2015-11-24 Pinnacle Engines, Inc. High swirl engine
US20120174881A1 (en) * 2010-12-14 2012-07-12 Taylor Jack R Full expansion internal combustion engine
US8550042B2 (en) * 2010-12-14 2013-10-08 Jack R. Taylor Full expansion internal combustion engine
CN103348110A (en) * 2010-12-14 2013-10-09 杰克.R.泰勒 Full expansion internal combustion engine
US8973539B2 (en) 2010-12-14 2015-03-10 Jack R. Taylor Full expansion internal combustion engine

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