WO2012061894A1 - Two stroke engine porting arrangement - Google Patents
Two stroke engine porting arrangement Download PDFInfo
- Publication number
- WO2012061894A1 WO2012061894A1 PCT/AU2011/001456 AU2011001456W WO2012061894A1 WO 2012061894 A1 WO2012061894 A1 WO 2012061894A1 AU 2011001456 W AU2011001456 W AU 2011001456W WO 2012061894 A1 WO2012061894 A1 WO 2012061894A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- piston
- gas transfer
- cylinder
- port
- separator plate
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
- F02B33/06—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps
- F02B33/10—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps with the pumping cylinder situated between working cylinder and crankcase, or with the pumping cylinder surrounding working cylinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
- F02B25/02—Engines characterised by using fresh charge for scavenging cylinders using unidirectional scavenging
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
- F02B25/14—Engines characterised by using fresh charge for scavenging cylinders using reverse-flow scavenging, e.g. with both outlet and inlet ports arranged near bottom of piston stroke
- F02B25/16—Engines characterised by using fresh charge for scavenging cylinders using reverse-flow scavenging, e.g. with both outlet and inlet ports arranged near bottom of piston stroke the charge flowing upward essentially along cylinder wall opposite the inlet ports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
- F02B25/26—Multi-cylinder engines other than those provided for in, or of interest apart from, groups F02B25/02 - F02B25/24
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
- F02B33/06—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps
- F02B33/10—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps with the pumping cylinder situated between working cylinder and crankcase, or with the pumping cylinder surrounding working cylinder
- F02B33/12—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps with the pumping cylinder situated between working cylinder and crankcase, or with the pumping cylinder surrounding working cylinder the rear face of working piston acting as pumping member and co-operating with a pumping chamber isolated from crankcase, the connecting-rod passing through the chamber and co-operating with movable isolating member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
- F02B33/06—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps
- F02B33/20—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps with pumping-cylinder axis arranged at an angle to working-cylinder axis, e.g. at an angle of 90 degrees
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/32—Engines characterised by connections between pistons and main shafts and not specific to preceding main groups
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/116—Intake manifolds for engines with cylinders in V-arrangement or arranged oppositely relative to the main shaft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
Definitions
- the present invention relates to two-stroke engines and, more particularly, to the transfer of gasses within the cylinder of such engines.
- Two-stroke engines typically cannot use a pressurised lubrication system and instead, oil is added to the air/fuel mixture to allow lubrication of the piston within the cylinder and the roller bearings on the crankshaft.
- a lack of a pressurised lubrication system requires roller bearings on the crankshaft and con-rods which are able to operate in the oil/fuel mix, unlike cheaper and simpler slipper bearings. This requires a heavy and expensive crankshaft assembly, to permit roller-bearing fitment .
- the present applicant has disclosed a twin cylinder two-stroke engine arrangement in which each cylinder is divided into upper and lower cylinder sections by a fixed separator plate, with each piston moving reclprocatingly in the upper section between the separator plate and the cylinder head.
- a gas transfer port system for a cylinder of a two-stroke internal combustion engine; said cylinder provided with a fixed separator plate dividing said cylinder into an upper section and a lower section; a piston in said cylinder reciprocating between said separator plate and a cylinder head; and wherein an annular skirt descending from said separator plate forms at least a portion of an annular well " between said skirt and an internal surface of said cylinder; said well sealed at the bottom such that said cylinder is isolated from a crankcase of said engine; said gas transfer port system including at least one long gas transfer port connecting a lower portion of said annular well with a gas transfer port outlet aperture in a wall of said cylinder.
- said long gas transfer port is one of at least one pair of gas transfer ports; each said pair of gas transfer ports including a short gas transfer port and a said long gas transfer port .
- said fixed separator plate forms an upper closure of said annular skirt; the diameter of an outer surface of said annular skirt being smaller than the bore of said cylinder, such that an annular well is formed between said outer surface and said bore of said cylinder for at least a part of the circumference of said annular skirt.
- said fixed separator plate and said annular skirt isolate said upper section of said cylinder from a crankcase of said engine/ a lower edge of said annular skirt sealing against an annular ledge at a base of said cylinder.
- said well is of sufficient depth to accommodate an exhaust control , skirt when said piston descends to BDC; said exhaust control skirt depending from an underside rim of said piston.
- an exhaust port of said cylinder is arranged diametrically opposite an inlet port of said cylinder.
- said cylinder is provided with four pairs of said gas transfer ports; said four pairs arranged in two diametrically opposing pairs of pairs between said exhaust port and said inlet port.
- each said short gas transfer port has ' an inlet aperture proximate an upper surface of said separator plate; said short gas transfer port having an outlet aperture above an upper surface of said piston when said piston is at BDC.
- each said long gas transfer port has an inlet proximate the bottom of said annular well; said long gas transfer port having an outlet aperture common with said outlet aperture of a corresponding short gas transfer port of said pair of gas transfer ports.
- a single gas transfer port is arranged aligned axially with an outlet aperture of said inlet port,- said single gas transfer port extending from below said upper surface of said separator plate to above said upper surface of said piston when said piston is at BDC; an outlet aperture of said inlet port communicating with said single gas transfer port.
- said piston is provided with an inlet port control skirt; said inlet port control skirt depending from said lower edge of said piston sufficient to block passage of gas from between an underside of said piston and said upper surface of said separator plate, into said outlet aperture of said inlet port when said piston descends to BDC; said skirt extending below said upper surface of said separator plate when said piston is at BDC,
- passages .of said short and long gas transfer ports are curved proximate said common outlet apertures such that gas flows issuing from said common outlet apertures are biased in flow direction towards and above said inlet port.
- a portion of said annular well is blocked so as to reduce the volume of said well; said reduction in volume increasing the available compression ratio of said cylinder.
- an underside of said piston is shaped with angled surfaces sweeping upward from a diametric centreline lying between an inlet port side and an exhaust port side of said cylinder; said angled surfaces directing gas flow from between said underside of said piston and said upper surface of said separator plate into said inlet apertures of said short gas transfer ports as said piston approaches BDC.
- a method of transferring gasses from an underside of a piston of a cylinder of a two-stroke engine including the steps of providing at least one long gas transfer ports extending from an inlet aperture proximate a bottom portion of an annular well to an outlet aperture located above an upper surface of said piaton when said piston is at BDC; said annular well formed between an inside surface of said cylinder and an annular skirt depending from a fixed separator plate.
- said long gas transfer port is one of a pair of gas transfer ports; a second of said pair of transfer ports being a short gas transfer port extending from a level below an underside of said piston to said outlet aperture above said upper surface of said piston when said piston is at BDC in said cylinder; said short gas transfer port having an outlet aperture common with said long gas transfer port.
- said annular well at least partially surrounds said annular skirt depending from said fixed separator plate; said separator plate and said annular skirt isolating an upper section of said cylinder from a crankcase of said engine.
- a charge of gas comprising air or an air/fuel mixture is drawn . through an inlet port into a volume defined by said annular well and between said underside of said piston and an upper surface of said fixed separator plate, as said piston rises toward TDC.
- said charge of gas is compressed into said volume as said piston descends from TDC towards BDC; pressure in said pair of gas transfer ports rising to , a maximum until said upper surface of said piston descends below an upper edge of said outlet aperture of said pair of gas transfer ports; said charge then commencing issuing from said outlet aperture.
- transfer of said charge is boosted by a rapid rise in pressure as separation between said underside of said piston and said upper surface of said separator plate approaches a minimum; said rapid rise in pressure causing an accelerated transfer of said gas through said short transfer port.
- a single gas transfer port directs a flow of said charge across an upper surface of said piston as said piston approaches BDC; said single gas transfer port communicating with an outlet aperture of an inlet port of said cylinder; said single gas transfer port extending from a level below said separator plate to a level above said upper surface of said piston.
- said piston is provided with a short inlet port skirt depending from an edge of said piston; said short inlet skirt substantially coextensive with said outlet aperture of said inlet ' port when said piston is at BDC.
- Figure 1 is a simplified schematic representation of a two-stroke internal combustion engine employing the porting arrangement of the invention
- Figure 2 is a sectioned view of paired cylinders and associated components of a two-stroke engine incorporating the porting arrangement of Figure 1
- Figure 3 is further sectioned view of the paired cylinders of Figure 2.
- the porting system of the present invention is applied to paired cylinders 10 and 12 of a two-stroke engine 14.
- Engines employing the invention may be two cylinder or other combinations of paired cylinders, thus four, six or eight cylinder engines for example, although the porting arrangement of the invention may be applied also to single cylinder engines.
- the following description focuses on one of the cylinders (the iret cylinder" and its associated features) of cylinders paired in "V" formation, in which the pistons move at 180o separation BO that when the first cylinder is at top dead centre (TDC) the other is at bottom dead centre (BDC) .
- the engine 14 is provided with an inlet pivot valve 16 arrangement previously described in the applicant's earlier filing AU2009238261.
- the porting arrangement of the present invention adds significantly to the Working, integrity and efficiency of the pivot valve invention.
- the porting system of the present invention is applicable to engines in which each of the cylinders is divided by a fixed separator plate 1 ⁇ into upper and lower cylinder sections 22 and 24 respectively, with the piston 20 reciprocating in the upper section 22 between the separator plate 18 and cylinder head 26 (removed in Figure 2) .
- the piston 20 divides its upper cylinder section 22 into a combustion chamber portion 19 above the piston and an induction or pressure chamber portion 17 between the underside of the piston 20 and the upper surface of the separator plate 18.
- the guide element 30 is pivotally connected by a gudgeon pin 32 to a connecting rod 34, which in turn is rotationally connected to a crankshaft journal 36, in the normal manner.
- This lower section of the cylinder is of a smaller diameter than the bore of the upper cylinder section, and in effect is an insert into the main cylinder body, forming an inverted "beaker” or “thimble” shape comprising the separator plate 18 and an annular skirt 21 depending from the plate 18.
- the outer diameter of the annular skirt 21 is such as to form an annular well 23 between the bore of the main cylinder body and the annular skirt 21.
- This well 23 is of sufficient depth to accommodate an exhaust port control skirt 25 which depends from the underside rim of the piston 20, as is common in two-stroke engines.
- Each cylinder 10, 12, is provided with at least one long gas transfer port 44.
- the at least one long gas transfer port 44 is one of a pair of gas transfer ports 40.
- the other of the pair of gas transfer ports is a short transfer port 42.
- the long gas transfer port 44 of the pair of transfer ports extends from an aperture 46 proximate to the bottom of the annular well 23, to the shared common outlet aperture 45 of the short transfer port 42.
- the short transfer port 42 extends from an inlet aperture 43 located in the wall of the upper cylinder section between the upper surface of the fixed separator plate 18 and the underside of the piston 20, to an outlet aperture 45 in the cylinder wall above the upper surface of the piston when this is at BDC .
- the engine for application of the transfer port system of the present invention is a cross flow engine, in that the exhaust port: 48 and the inlet port 50 are located at diametrically opposite sides of the cylinder.
- the transfer port system of the invention may include multiple pairs, preferably, four pairs of short and long transfer ports, with two pairs of pairs located diametrically opposed between the exhaust port 48 and the inlet port 50, as can be seen from Figure 3.
- the lower edge of exhaust port 4B, inlet port 50 and the outlet apertures 45 of the four pairs of transfer ports are located at the same level in the cylinder wall as the upper surface of the piston 20 when this is at BDC.
- the locations of the upper edges of these ports are critical to the opening of the ports by the descending piston, to allow firstly the exhaust gasses to start to exit through the exhaust port, and then opening the transfer ports.
- the outlet aperture of the inlet port 50 lies somewhat below the level of the lower lip of the exhaust port 48.
- the passages 52 linking the short and long gas transfer ports from their respective inlet apertures to their common outlet aperture 45 are so curved, adjacent the outlet apertures, as to direct a flow of gas issuing from the apertures, towards the inlet port 50, assisting in the scavenging of exhaust gasses from the combustion chamber 22.
- the system of the invention provides the typical and common further single transfer port 54. This single gas transfer port 54 extends from a level below that of the upper surface of the fixed separator plate 18 to a point somewhat above the upper surface of the piston 20 when the piston is at BDC.
- This type of gas transfer port is commonly used in modern two-stroke engines and is known the booster transfer port. It forms a vertical projection of the inlet port 50, connecting the port with the combustion chamber 22 when the piston is near BDC, allowing further communication between the network of the transfer ports connecting the induction/pressure chamber portion 17 and the combustion chamber portion 19 respectively formed below and above the piston 20.
- the function of the booster transfer port 54 in known two ⁇ stroke engines is to increase charge transfer from the induction/pressure chamber portion to the combustion chamber portion of the cylinder, as well as to clear any residual burnt charges from the top of the piston. Because the gas issuing from this transfer port is directed towards exhaust port (unlike the paired transfer port passages as described below which direct their gas flow towards the inlet port side of the cylinder), the size of the booster port is kept relatively small, since any excess charge would be lost through the exhaust port, a condition known as short circuiting.
- this single gas transfer port 54 at the inlet port outlet has an additional function.
- the great outrush of an exhaust slug down the exhaust pipe after the piston 20 has opened the exhaust port 48 lowers the residual pressure in the combustion chamber portion 19 to below ambient atmospheric pressure, drawing in the fresh charge from the induction/pressure chamber portion 17 below the piston 20 through the paired transfer ports 40, as soon as the descending piston 20 clears the upper edges of the transfer port outlet apertures 45.
- the single transfer port 54 which is in effect an extension of the inlet port, then opens to clear any residual burnt gasses from the upper surface of the piston, which may be left behind due to the trajectories of the transfer ports which are aimed at the inlet side of the cylinder.
- the single gas transfer port 54 provides the most direct route from the exhaust port 48 to the inlet port 50, eo that the lowered pressure, or suction, is communicated via this single transfer port 54 with more immediacy to the still closed pivot valve 16, causing it to start opening.
- the piston on its rise from BDC can ⁇ draw-back", through the transfer ports 40, from the combustion chamber portion 19 to the induction/pressure chamber . portion 17, instead of from the inlet port 50, until such time as the ascending piston 20 rises past, and closes off the outlet apertures 45 of the transfer ports 40, and before the pivot valve 16 will open under the suction created only once the piston has passed this point.
- piston 20 is shaped with angled surfaces sweeping upward from a diametric centreline lying between an inlet port side and an exhaust port side of the cylinder. These angled surfaces direct gas flow from between the underside of the piston 20 and the upper surface of the fixed separator plate 18 towards the inlet apertures 43 of the short gas transfer ports 42 as the piston approaches BDC.
- the annular well 23 does not extend fully around the lower cylinder section, where it is not aligned with the long transfer port inlet apertures, as can be seen in the sectioned view of the right hand cylinder in Figure 2.
- the pistons of an engine for which the gas transfer port system of the invention is suited are provided with a shorter skirt 56 diametrically opposite the exhaust skirt 25.
- This inlet port skirt 56 extends downward from the piston 20 and is substantially coextensive with the area of the outlet aperture of the inlet port 50, as can best be seen in Figure 2.
- the rapidly compressing gas between the underside of the piston and the fixed separator plate 18 could transmit a destructive pressure wave up the inlet port to the relatively fragile leaf of the pivot valve 16 in its closed position. This pressure wave is trapped behind the inlet port skirt 56.
Landscapes
- 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)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Compressor (AREA)
Abstract
Description
Claims
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013126883/06A RU2559217C2 (en) | 2010-11-12 | 2011-11-11 | Two-stroke engine intake and exhaust channels configuration |
MX2013005193A MX339633B (en) | 2010-11-12 | 2011-11-11 | Two stroke engine porting arrangement. |
EP11840243.7A EP2638267A4 (en) | 2010-11-12 | 2011-11-11 | Two stroke engine porting arrangement |
CN201180064849.XA CN103380278B (en) | 2010-11-12 | 2011-11-11 | Two stroke engine port device |
JP2013538005A JP5874733B2 (en) | 2010-11-12 | 2011-11-11 | Two-stroke engine porting configuration |
CA2817637A CA2817637C (en) | 2010-11-12 | 2011-11-11 | Two stroke engine porting arrangement |
BR112013011843A BR112013011843A2 (en) | 2010-11-12 | 2011-11-11 | arrangement carrying two stroke engine |
US13/884,273 US9334789B2 (en) | 2010-11-12 | 2011-11-11 | Two stroke engine porting arrangement |
KR1020137014434A KR101747755B1 (en) | 2010-11-12 | 2011-11-11 | Two stroke engine porting arrangement |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2010241402A AU2010241402B1 (en) | 2010-11-12 | 2010-11-12 | Two-Stroke Engine Porting Arrangement |
AU2010241402 | 2010-11-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2012061894A1 true WO2012061894A1 (en) | 2012-05-18 |
Family
ID=45442319
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AU2011/001456 WO2012061894A1 (en) | 2010-11-12 | 2011-11-11 | Two stroke engine porting arrangement |
Country Status (11)
Country | Link |
---|---|
US (1) | US9334789B2 (en) |
EP (1) | EP2638267A4 (en) |
JP (1) | JP5874733B2 (en) |
KR (1) | KR101747755B1 (en) |
CN (1) | CN103380278B (en) |
AU (1) | AU2010241402B1 (en) |
BR (1) | BR112013011843A2 (en) |
CA (1) | CA2817637C (en) |
MX (1) | MX339633B (en) |
RU (1) | RU2559217C2 (en) |
WO (1) | WO2012061894A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8505504B2 (en) * | 2009-04-09 | 2013-08-13 | Louis A. Green | Two-stroke engine and related methods |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US948336A (en) | 1908-09-08 | 1910-02-08 | Edward Moore | Internal-combustion engine. |
AU2009238281B1 (en) | 2009-11-16 | 2010-10-28 | CITS Engineering Pty Limited | Improvements in two-stroke engines |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
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US1785909A (en) * | 1928-12-05 | 1930-12-23 | Berr E Post | Explosive engine |
US2010170A (en) * | 1932-10-31 | 1935-08-06 | Edward A Winfield | Internal combustion engine |
JPS5840649B2 (en) * | 1972-08-22 | 1983-09-07 | パ−フオ−マンス インダストリイズ インコ−ポレ−テツド | benzouchi |
JPS5455208A (en) * | 1977-10-11 | 1979-05-02 | Toyota Motor Corp | Activehot atmosphere combustion for two-cycle internal combustion engine |
SU1280155A1 (en) * | 1980-04-07 | 1986-12-30 | Институт проблем надежности и долговечности машин АН БССР | Two-stroke internal combustion engine |
EP0263117A1 (en) * | 1986-02-17 | 1988-04-13 | URQUHART, Robert | Supercharged two-stroke engine |
MX9200702A (en) * | 1991-02-21 | 1992-10-01 | Orbital Eng Pty | INTERNAL COMBUSTION ENGINE, RECIPROMOTIVE INTERNAL COMBUSTION, RECIPROCAL MOTION, TWO-STROKE CYCLE, MULTIPLE CYLINDERS, TWO-STROKE CYCLE, MULTIPLE CYLINDERS. YOU. |
DE4311620A1 (en) * | 1993-04-08 | 1994-10-13 | Frank Schmidt | Two-stroke engine |
DE19641703C1 (en) * | 1996-10-10 | 1998-01-22 | Daimler Benz Ag | Two-stroke engine |
GB9810057D0 (en) * | 1998-05-11 | 1998-07-08 | Ricardo Consulting Eng | Crankcase scavenged two-stroke engines |
JP2000034924A (en) * | 1998-07-17 | 2000-02-02 | Kioritz Corp | 2-cycle internal combustion engine |
US6223705B1 (en) * | 1998-07-17 | 2001-05-01 | Kioritz Corporation | Two-stroke internal combustion engine |
JP2002276377A (en) * | 2001-03-21 | 2002-09-25 | Kioritz Corp | Two-cycle internal combustion engine |
FR2838478B1 (en) * | 2002-04-15 | 2004-05-28 | D L B | 2-STROKE THERMAL ENGINE WITH REDUCED POLLUTION AND 4-STROKE WITH SCAN AND VOLUMETRIC SUPPLY |
US20090013980A1 (en) * | 2005-07-05 | 2009-01-15 | Ken Takachi | Two cycle engine |
WO2009117775A1 (en) * | 2008-03-26 | 2009-10-01 | Basil Van Rooyen | High secondary compression ratio anp pressube lubricated two- stroke engine |
RU2398117C1 (en) * | 2008-12-01 | 2010-08-27 | Государственное образовательное учреждение высшего профессионального образования Самарский государственный аэрокосмический университет им. академика С.П. Королева | Two-stroke ice |
-
2010
- 2010-11-12 AU AU2010241402A patent/AU2010241402B1/en not_active Ceased
-
2011
- 2011-11-11 CN CN201180064849.XA patent/CN103380278B/en active Active
- 2011-11-11 CA CA2817637A patent/CA2817637C/en not_active Expired - Fee Related
- 2011-11-11 EP EP11840243.7A patent/EP2638267A4/en not_active Withdrawn
- 2011-11-11 WO PCT/AU2011/001456 patent/WO2012061894A1/en active Application Filing
- 2011-11-11 US US13/884,273 patent/US9334789B2/en active Active
- 2011-11-11 RU RU2013126883/06A patent/RU2559217C2/en not_active IP Right Cessation
- 2011-11-11 MX MX2013005193A patent/MX339633B/en active IP Right Grant
- 2011-11-11 JP JP2013538005A patent/JP5874733B2/en active Active
- 2011-11-11 BR BR112013011843A patent/BR112013011843A2/en not_active IP Right Cessation
- 2011-11-11 KR KR1020137014434A patent/KR101747755B1/en active IP Right Grant
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US948336A (en) | 1908-09-08 | 1910-02-08 | Edward Moore | Internal-combustion engine. |
AU2009238281B1 (en) | 2009-11-16 | 2010-10-28 | CITS Engineering Pty Limited | Improvements in two-stroke engines |
Non-Patent Citations (1)
Title |
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Publication number | Publication date |
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RU2013126883A (en) | 2014-12-20 |
BR112013011843A2 (en) | 2016-08-16 |
CN103380278A (en) | 2013-10-30 |
US9334789B2 (en) | 2016-05-10 |
CA2817637C (en) | 2016-12-20 |
JP5874733B2 (en) | 2016-03-02 |
KR101747755B1 (en) | 2017-06-27 |
EP2638267A4 (en) | 2015-12-09 |
RU2559217C2 (en) | 2015-08-10 |
JP2014500428A (en) | 2014-01-09 |
CA2817637A1 (en) | 2012-05-18 |
EP2638267A1 (en) | 2013-09-18 |
MX339633B (en) | 2016-06-02 |
MX2013005193A (en) | 2013-09-26 |
CN103380278B (en) | 2016-09-14 |
US20130228158A1 (en) | 2013-09-05 |
KR20140001932A (en) | 2014-01-07 |
AU2010241402B1 (en) | 2011-11-24 |
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