WO1988000281A1 - Multi-phase combustion system for piston internal combustion engines - Google Patents
Multi-phase combustion system for piston internal combustion engines Download PDFInfo
- Publication number
- WO1988000281A1 WO1988000281A1 PCT/AU1987/000209 AU8700209W WO8800281A1 WO 1988000281 A1 WO1988000281 A1 WO 1988000281A1 AU 8700209 W AU8700209 W AU 8700209W WO 8800281 A1 WO8800281 A1 WO 8800281A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- cylinder
- piston
- openings
- improvement according
- ports
- 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/02—Engines characterised by precombustion chambers the chamber being periodically isolated from its 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
- F02B21/00—Engines characterised by air-storage chambers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the invention concerns means by which a multi-phase combustion process may be achieved in piston internal combustion engines.
- combustion occurs in a multi-phase manner. Following the first phase, the establishment of a self-sustaining body of flame adjacent to the spark plug, a flame front propagates rapidly throughout the combustion chamber in what may be termed the primary combustion event. Very little piston movement occurs during this process. As the piston descends, further combustion occurs of areas of lean mixture, of quench products scoured by turbulence away from the combustion chamber walls and of mixture trapped in narrow parts of the combustion chamber. This process may be termed the secondary combustion event.
- the present invention has for its object the provision of an arrangement in an internal combustion engine which will achieve a prolonging of the secondary combustion event without the disadvantages of the method described in the foregoing paragraph.
- the present invention provides an internal, combustion engine having at least one cylinder in a cylinder' block with a piston reciprocable therein and a cylinder head closing an upper end of the or each of said cylinders, the improvement comprising the provision of at least one recess in a wall of the or each of the said cylinders adjacent said cylinder head forming a chamber adapted to- receive combustible charge materials from the cylinder: a jacent thereto through a restricted access opening: ox: ⁇ p-enings.
- the upper part of the cylinder block of a piston engine is made such that an annular recess of rectangular cross-sectional shape is provided at the top of the or each of the cylinder bores.
- Accommodated within the said annular recess and imprisoned by the cylinder head may be provided one or more rings incorporating at l.east one and preferably an annular space forming said chamber communicating with the cylinder through a plurality of ports, said ports being positioned such that they are covered by the piston as it approaches top dead centre.
- the inner face of the said ring or rings may be honed to make than a smooth contiguous extension of the engine upper cylinder bore.
- the cylinder bore area between the said discharge ports is such that adequate bearing surface is provided for the piston rings.
- a recess 1 is provided in cylinder block 5 at the top of cylinder bore 2, in said annular recess being acco odated ring 3 imprisoned by cylinder head 4. Said ring is fitted into cylinder block 5 in an interference fit to provide good heat transfer properties, and its inner surface 10 is honed to make it a smooth contiguous extension of the engine upper cylinder bore 2.
- Ring 3 incorporates annular space 6 communicating with cylinder 8 through a plurality of ports 7.
- Said ports are positioned such that they are covered by piston 9 during the final part of its upward travel. Said ports are made to direct their discharge radially into the cylinder or, in alternative embodiments, are angled such that their collective discharge produces a v rtex' within the cylinder or is directed upward or downward.
- annular space 6 is positioned high up in a single ring 3, permitting discharge ports 7 to take the form of narrow channels in the upper surface of the said ring, said channels being closed by the lower surface of cylinder head 4.
- annular space 6 is made more or less toroidal with ports 7 positioned more or less tangential to its upper edge.
- the said annular space is made with other cross-sectional shapes.
- one or more additional rings 3 are provided in the upper cylinder bore, each incorporating an annular space 6 and ports 7.
- the bore and stroke dimensions of the engine are made to suit the desired duty characteristics of the engine and the number and volume of the said annular spaces.
- the dimensions of ports 7 are altered to permit combustion to occur within the said annular space or spaces or to ensure that quenching effects prevent combustion from occurring therein.
- ports 7 are deleted from the cylinder bore thrust face, or are made smaller with wider bearing surfaces between them.
- mixture is forced through ports 7 into annular space 6 and is trapped by piston 9 closing off the said ports during its final upward travel.
- the said ports are uncovered releasing the compressed mixture to prolong the secondary combustion event.
- combustion extends to annular space 6, resulting in jets of combustion products entering cylinder 8, said combustion products serving to prolong- the secondary combustion event.
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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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
In a reciprocating piston engine a peripheral cavity (6) surrounds each engine cylinder (8) adjacent a cyclinder head (4) of the engine. A plurality of ports (7) provide communication between the cavity (6) and the cylinder (8), the ports (7) being opened and closed by passage of the piston (9) whereby a portion of the charge is received and sealed in the cavity (6) during the engine compression stroke. Following ignition, the power stroke takes place in two stages; a primary combustion stage while the ports (7) are covered by the piston (9) followed by a secondary combustion stage when the ports (7) have been uncovered by the descending piston (9) to re-establish communication between the cylinder (8) and the cavity (6).
Description
MULTI-PHASE COMBUSTION SYSTEM FOR PISTON INTERNAL COMBUSTION ENGINES
The invention concerns means by which a multi-phase combustion process may be achieved in piston internal combustion engines.
In the spark ignited internal combustion engine, combustion occurs in a multi-phase manner. Following the first phase, the establishment of a self-sustaining body of flame adjacent to the spark plug, a flame front propagates rapidly throughout the combustion chamber in what may be termed the primary combustion event. Very little piston movement occurs during this process. As the piston descends, further combustion occurs of areas of lean mixture, of quench products scoured by turbulence away from the combustion chamber walls and of mixture trapped in narrow parts of the combustion chamber. This process may be termed the secondary combustion event.
Methods have been devised to retard the combustion events in a manner calculated to make their duration more consistent with piston movement. One such method involves the fixing of a false crown to the piston, the diameter of the said .false crown being smaller than the cylinder bore in a way which provides a narrow annular opening around its periphery. During the compression stroke, mixture is forced through the said narrow annular opening into the area beneath the said false crown, being released during the firing stroke. This release of mixture has the effect of prolonging the secondary combustion event and improving engine torque and fuel economy.
The shortcomings of this arrangement are complexity of manufacture, the problem of cooling the false piston crown during high power operation, and the increased parasitic losses resulting from the increased reciprocating mass .
The present invention has for its object the provision of an arrangement in an internal combustion engine
which will achieve a prolonging of the secondary combustion event without the disadvantages of the method described in the foregoing paragraph.
Accordingly the present invention provides an internal, combustion engine having at least one cylinder in a cylinder' block with a piston reciprocable therein and a cylinder head closing an upper end of the or each of said cylinders, the improvement comprising the provision of at least one recess in a wall of the or each of the said cylinders adjacent said cylinder head forming a chamber adapted to- receive combustible charge materials from the cylinder: a jacent thereto through a restricted access opening: ox: σp-enings.
According to a preferred arrangement, the upper part of the cylinder block of a piston engine is made such that an annular recess of rectangular cross-sectional shape is provided at the top of the or each of the cylinder bores.
Accommodated within the said annular recess and imprisoned by the cylinder head may be provided one or more rings incorporating at l.east one and preferably an annular space forming said chamber communicating with the cylinder through a plurality of ports, said ports being positioned such that they are covered by the piston as it approaches top dead centre. The inner face of the said ring or rings may be honed to make than a smooth contiguous extension of the engine upper cylinder bore. The cylinder bore area between the said discharge ports is such that adequate bearing surface is provided for the piston rings.
The present invention will be more readily understood by reference to the following description of preferred embodiments given in relation to the accompanying drawing which depicts a transverse sectional view of an engine cylinder block embodying the invention.
With reference to the drawing, a recess 1 is provided in cylinder block 5 at the top of cylinder bore 2, in said annular recess being acco odated ring 3 imprisoned
by cylinder head 4. Said ring is fitted into cylinder block 5 in an interference fit to provide good heat transfer properties, and its inner surface 10 is honed to make it a smooth contiguous extension of the engine upper cylinder bore 2. Ring 3 incorporates annular space 6 communicating with cylinder 8 through a plurality of ports 7.
Said ports are positioned such that they are covered by piston 9 during the final part of its upward travel. Said ports are made to direct their discharge radially into the cylinder or, in alternative embodiments, are angled such that their collective discharge produces a v rtex' within the cylinder or is directed upward or downward.
In another embodiment, annular space 6 is positioned high up in a single ring 3, permitting discharge ports 7 to take the form of narrow channels in the upper surface of the said ring, said channels being closed by the lower surface of cylinder head 4. In the preferred embodiment, annular space 6 is made more or less toroidal with ports 7 positioned more or less tangential to its upper edge. In other embodiments, the said annular space is made with other cross-sectional shapes. In a further embodiment, one or more additional rings 3 are provided in the upper cylinder bore, each incorporating an annular space 6 and ports 7.
The bore and stroke dimensions of the engine are made to suit the desired duty characteristics of the engine and the number and volume of the said annular spaces. Depending upon the size and desired duty characteristics of the engine, the dimensions of ports 7 are altered to permit combustion to occur within the said annular space or spaces or to ensure that quenching effects prevent combustion from occurring therein.
In engines producing high torque, ports 7 are deleted from the cylinder bore thrust face, or are made smaller with wider bearing surfaces between them.
In operation, during the compression stroke, mixture is forced through ports 7 into annular space 6 and is trapped by piston 9 closing off the said ports during its final upward travel. During the firing stroke and after completion of the primary combustion event, the said ports are uncovered releasing the compressed mixture to prolong the secondary combustion event. In an alternative embodiment, as piston 9 uncovers ports 7, combustion extends to annular space 6, resulting in jets of combustion products entering cylinder 8, said combustion products serving to prolong- the secondary combustion event.
Claims
1. In an internal combustion engine having at least one cylinder in a cylinder block with a piston reciprocable therein and a cylinder head closing an upper end of the or each of said cylinders, an improvement comprising the provision of at least one recess in a wall of the or each of the said cylinders adjacent said cylinder head forming a chamber or chambers adapted to receive combustible charge materials from the cylinder adjacent thereto through a restricted access opening or openings, said access opening or openings being opened or closed by passage of the piston within the cylinder.
2. The improvement according to claim 1 wherein a single said chamber is provided in the form of a peripheral cavity surrounding each said cylinder with a plurality of access openings leading to said cylinder from said peripheral cavity.
3. The improvement according to claim 2 wherein said peripheral cavity is toroidal in configuration.
4. The improvement according to claim 2 wherein said peripheral cavity is arranged as an annular groove opening onto a parting face between said cylinder block and said cylinder head.
5. The improvement according to claim 4 wherein said openings are formed by circu ferentially located recesses opening onto said parting face and extending between each said cylinder and its associated said peripheral cavity.
6. The improvement according to any one of claims 1 to 5 wherein said chambers and said access opening or openings are formed in an annular insert arranged in a corresponding annular recess in the cylinder wall adjacent said cylinder head.
7. The improvement according to any one of claims 1 to 6 wherein said access opening or openings is/are shaped and configured to create vortex flow conditions within the adjacent cylinder.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU681986 | 1986-07-09 | ||
AUPH6819 | 1986-07-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1988000281A1 true WO1988000281A1 (en) | 1988-01-14 |
Family
ID=3697410
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AU1987/000209 WO1988000281A1 (en) | 1986-07-09 | 1987-07-09 | Multi-phase combustion system for piston internal combustion engines |
Country Status (1)
Country | Link |
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WO (1) | WO1988000281A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0486963A1 (en) * | 1990-11-22 | 1992-05-27 | Hugo Kueckenwaitz | Combustion engine with a plurality of combustion chambers |
WO2011097253A1 (en) * | 2010-02-03 | 2011-08-11 | Total Energy Renewable Power Systems, Llc | Modifying an internal combustion engine for radical ignition combustion |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU1152923A (en) * | 1923-03-15 | 1923-07-24 | Orville Trudeau Maxisiillian | Internal combustion engines |
US1937655A (en) * | 1931-02-14 | 1933-12-05 | Lanova Ag | Diesel engine |
US1944352A (en) * | 1930-12-01 | 1934-01-23 | Lanova Ag | Injection engine |
US4070998A (en) * | 1975-10-24 | 1978-01-31 | Grow Harlow B | Compression ignition control pressure heat engine |
-
1987
- 1987-07-09 WO PCT/AU1987/000209 patent/WO1988000281A1/en unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU1152923A (en) * | 1923-03-15 | 1923-07-24 | Orville Trudeau Maxisiillian | Internal combustion engines |
US1944352A (en) * | 1930-12-01 | 1934-01-23 | Lanova Ag | Injection engine |
US1937655A (en) * | 1931-02-14 | 1933-12-05 | Lanova Ag | Diesel engine |
US4070998A (en) * | 1975-10-24 | 1978-01-31 | Grow Harlow B | Compression ignition control pressure heat engine |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0486963A1 (en) * | 1990-11-22 | 1992-05-27 | Hugo Kueckenwaitz | Combustion engine with a plurality of combustion chambers |
WO2011097253A1 (en) * | 2010-02-03 | 2011-08-11 | Total Energy Renewable Power Systems, Llc | Modifying an internal combustion engine for radical ignition combustion |
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