WO2015167444A1 - Combustion chamber for an internal combustion engine and an internal combustion engine - Google Patents

Combustion chamber for an internal combustion engine and an internal combustion engine Download PDF

Info

Publication number
WO2015167444A1
WO2015167444A1 PCT/US2014/035773 US2014035773W WO2015167444A1 WO 2015167444 A1 WO2015167444 A1 WO 2015167444A1 US 2014035773 W US2014035773 W US 2014035773W WO 2015167444 A1 WO2015167444 A1 WO 2015167444A1
Authority
WO
WIPO (PCT)
Prior art keywords
piston
combustion engine
set forth
internal combustion
combustion chamber
Prior art date
Application number
PCT/US2014/035773
Other languages
French (fr)
Inventor
Richard S. BRANDT, III
Original Assignee
Volvo Truck Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Volvo Truck Corporation filed Critical Volvo Truck Corporation
Priority to US15/303,000 priority Critical patent/US10415456B2/en
Priority to EP14890716.5A priority patent/EP3140527B1/en
Priority to PCT/US2014/035773 priority patent/WO2015167444A1/en
Publication of WO2015167444A1 publication Critical patent/WO2015167444A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0624Swirl flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/066Details related to the fuel injector or the fuel spray the injector being located substantially off-set from the cylinder centre axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0663Details related to the fuel injector or the fuel spray having multiple injectors per combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0666Details related to the fuel injector or the fuel spray having a single fuel spray jet per injector nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0678Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets
    • F02B23/0687Multiple bowls in the piston, e.g. one bowl per fuel spray jet
    • 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
    • F02B25/02Engines characterised by using fresh charge for scavenging cylinders using unidirectional scavenging
    • F02B25/08Engines with oppositely-moving reciprocating working pistons
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • aspects of the presen t in vention relate generally to internal combustion engines and, more particularly, to combustion chambers for internal combustion engines.
  • Opposed piston engines include a cylinder with a pair of pistons that move toward each other toward top dead center positions to compress gas in the cylinder and near which fuel is injected through a side wall of the cyiinder.
  • U .S . Patent App. 1182012/0285418 observes that such engines require different arrangements for effective mixing of fuel, and air. Providing for effective mixing of fuel in air in conventional engine cy linders is, of course, also importan
  • a combustion chamber for an internal combustion engine comprises a cylinder wall defining a cylinder, a fuel injector disposed in a first opening in the cylinder wall, and a pisto head disposed in the cylinder, a piston bowl at least partially defined by a wall having a generally spiral shape being provided in a top of the piston head.
  • an engine comprising such a combustion chamber is provided.
  • FIG. I is a top, partially cross-sectional view of an internal combustion engine according to an aspect of the present invention.
  • FIG. 2 is a perspecti ve view of piston heads of an internal combustion engine according to an aspect of the present invention
  • FIGS. 3A-3B are top perspective and top views of a piston head of an internal
  • FIG. 3C is a cross- sectional view taken at section 3C-3C of FIG. 3B;
  • FIGS. 4A-4B are top views of a piston head of an internal combustion engine according to another aspect of the present invention, with FIG. 4B showing orientations of fuel injectors relative to the piston head;
  • FIGS. 5A-5B are side, partially cross-sectional views of an internal combustion engine according to another aspect of the present invention.
  • FIG. 6A is a top view of a piston in an internal combustion engine according to an aspect of the present invention, showing an orientation of inlet ports in a cylinder relative to an tipper piston of an opposed piston, engine;
  • FIG. 6B is a top view of a piston in an internal combustion engine according to an aspect of the present invention showing an orientation of outlet ports relative to a lower piston of an opposed piston engine; and
  • FIG , 7 A is a top view of a piston head according to another aspect of the present
  • FIG. 7B is a perspective view of piston heads of the tvpe shown in FIG. 7 A
  • FIG. 7C is a cross-sectional view taken at section 7C-7C of the piston head of FIG. 7 A.
  • FIG. I An internal combustio engine 2 i according to an aspect of the presen invention is seen in FIG. I and comprises a combustion chamber 23 comprising a cylinder wa l 25 defining a cylinder 27,
  • the cylinder wall 25 is ordinarily part of a cviinder liner or an engine block.
  • a fuel injector 29 is disposed in a first opening 3 1 in the cylinder wall 25
  • a piston head 33 is movably disposed in the cylinder 25 and is linked to a crankshaft (not shown in FIGS. I or 2) by a connecting rod (sometimes referred to as a conrod or pushrod) (not shown in FIGS. I or 2).
  • FIG. 2 shows piston heads 33 and 33 U of an opposed piston arrangement, with the upper piston head 33U tilted to permit illustration of fuel jets FJ injected by fuel injectors 29.
  • a piston bowl 35 that is at least partially defined by a wall 37 having a generally spiral shape is provided i a top 39 of the piston head 33.
  • the spiral may be a specific form of spiral, such as a logarithmic spiral, an Archimedean spiral, a hyperbolic spiral, etc., except where otherwise indicated, a
  • “spiral” will be understood to be a curve that, gets progressively closer to a central point as it revolves around the point.
  • References to the "top” of the pisto head 33 are intended to refe to the part of the piston head that, with the c viinder wail 25 defines the combustion chamber 23.
  • the piston head may be oriented in an engine so that the "top” of the piston head is in fact vertically below the rest of the pi ston head (suc as i s seen in the upper piston head in the opposed piston arrangement shown in FIGS. 2, 5A and 5B), horizontally even with the rest of the piston head (suc as when the cylinder 27 extends horizontally), or
  • the upper piston head 33U has a bowl 35U with a geometry that is a mirror image of the bowl. 35 of the lower piston head 33.
  • References herein to the piston head 33 or the bowl 35 of the piston head will be understood to apply equally to the upper piston head 33U and bowl 35U, the onl differences being that the geometry of the bowls are reversed on the two piston heads.
  • the volume of the pisto bow! 35 depends upon a compression ratio that is desired to be obtained by the piston head 33 and cylinder 27.
  • a depth of the spiral shaped wall 37 increases toward a center portion 41 of the pisto bowl 35. In the embodiment shown in FIGS.
  • the pisto bowl 35 is further defined by a ramp 43 that is defined on one edge by the spiral shaped wall 37 and on another edge by the center portion 41 of the piston bowl and that descends from the top surface 53 of the piston head 33 to the center portion at a distance below the top surface.
  • the fuel injector 29 can be oriented relative to piston bowl 35 so that a centra! axis AJ of an injected fuel jet FJ is generally parallel with the ramp 43 which can facilitate causing the mixture to "tumble" in the sense that, after proceeding downwardly into the bow! 35, it then moves upwardly again, as wei!
  • the fuel injector may, alternatively, be oriented so that the central axis of the injected fuel jet is generally perpendicular to a central axis AC of the cylinder as illustrated.
  • the outer end 45' of the spiral shaped wall 37 * may extend to the peripheral edge 47' of the top 39' of the piston head. 33' and the bowl may have no ramp. As seen in FIGS. 5A-58, in such an
  • the fuel injectors can be (but is not necessarily) oriented so thai the central, axis of the injected fuel jet Pi is generally perpendicular to a central axis AC of the cylinder.
  • the fuel injectors can, alternatively, be disposed at an angle to the perpendicular, which can further facilitate mixing of gas and fuel by causing the .mixture to "tumble" in. the sense that, after proceeding downwardly into the bowl 35 ', it then moves upwardly again, as well as to "swirl” by moving circumferential iy around the bowl.
  • the spiral shape of the walls 37 and 37' facilitates creati on of a circumferential swirling effect in the cylinder 27 and 27' that facilitates mixing of the injected fuel with incoming air and later with scavenging of exhaust gas. While dimensions will vary depending upon factors such as the size of the piston head 33 and cylinder 27, for a fuel jet FJ thai is typically about 50 mm in length, the length of the wails 37 and 37' will ordinarily be between about 20 and 100 mm, more preferably between about 30 and 60 mm. In the illustrated embodiments, the circumferential swirling effect will be in the clockwise direction, however, it will be appreciated that the effect could alternatively be in the counter-clockwise direction
  • the center portion 41 of the piston bowl 35 is ordinarily substantially circular in shape. This is true, as well, for the embodiment of the piston bowl 35 ' shown in FIGS. 4A-4B, as illustrated by the dotted line representing the circular central portion 41 ⁇ however, the circula ' shape is more apparent in FIGS. 3A-3B.
  • the spiral shaped wall 37 typically increases in depth from the outer end 45 of the spiral shaped wall toward an inner end 49 of the spiral shaped wall at the center portion 41.
  • substantially circular is defined herein as meaning approximating circular, but not necessarily exactly circular, as the precise boundaries of the substantially circular- central portions may not be capable of precise definition as different surfaces merge into each other, or (as in the piston heads 33' shown in. FIGS. 4A.-4B) the shapes do not As seen in FIG. 3C (cross-section of piston head), the center portion 4! of the piston bowl 35 can be substantially flat or. as shown in phantom, concave. Altering the depth and total volume of the piston bowl 35 alters the compression ratio that is desired to be obtained by the piston bead 33 and cylinder 27.
  • the bowl 35 of the pisto head 33 is at least partially defined by a second wall 5 i having a generally spiral shape.
  • the first spiral shaped wall 37 and the second spiral shaped wall 51 are ordinarily rotationally symmetrical about the central axis AC of the cylinder 27.
  • a top surface 53 of the top 39 of the piston head 33 is substantially flat, and the piston bowl 35 and tlie first and second spiral shaped walls 37 and 5 i are recessed relative to the top surface.
  • First and second recesses 55 and 57 defining outer ends 45 and 59 of the first and second spiral shaped walls 7 and 51 , respecti vely, can be disposed inwardly from an outer peripheral edge 47 of the top 39 of the piston head 33.
  • a. second fuel injector 61 can also be provided i a second opening 63 in the cylinder wall 25.
  • the first and second fuel injectors 29 and 61 ca be oriented relative to the piston bowl 35 so that central axes AJ of injected fuel jets FJ from the first and second fuel injectors are generally aligned with centers of the first and second recesses 55 and 57, Ordinarily, a center portion 41 of the piston bowl 35 is substantiall circular in shape, and the first and second fuel injectors 29 and 61 are oriented relative to the piston bowl so that central axes.
  • AJ of injected fuel jets FJ from the first and second fuel injectors are offset relative to the central axis of the piston 33 so that they are tangent to the circle, or nearly tangent thereto, as illustrated in FIG. I.
  • the injectors 29 and 61 are illustrated as being disposed at
  • a periphery 47 Of the top 39 * of the piston head is recessed at an outer end 45' of die spiral shaped wall 37', i.e., the spiral shaped wall extends all the way to the periphery of the top of the piston head to define a recess 69'.
  • the fuel injectors 29' and 6 are oriented relative to piston bowl 35' so that a central axis A J of an injected fuel jet FJ is generally aligned with a center of the recess 69'.
  • the piston head 33' is ordinarily used with another upper piston head 331 ⁇ in an opposed piston engine 2 .
  • the piston head 33' and the upper pisto head 33 LP will be mirror images of each other, except that one is rotated 180 degrees around a central, axis of the cylinder to the other.
  • references to the piston head 33' will be understood to appl equall to the piston head 331J ⁇ except where otherwise indicated.
  • an opposed piston engine 21 using the piston heads 33 shown in FIGS. 1-3C can hav the same basic constructions as the opposed piston engine 21 ' shown in FIGS. 5A-5B.
  • the center portion 4 of the resulting piston bowl 35' is more clearly substantially circular in shape.
  • the central axis AJ of the injected fuel jet. FJ is offset from the central axis of the piston so that ft i tange t to, or nearly tangent to, the resulting circle at the center portion 41. ',.
  • the circle 41 ' defined by the spiral shaped wall 37' of the piston head 33' may be offset from the circle defined by the spiral shaped wall of the upper piston head 33U'.
  • the spiral shaped walls 37' of the piston heads 33' and 33 U' can be rather high, which can be helpful to avoid spraying fuel on the cylinder wall or liner.
  • a second fuel injector 61 ' can be disposed in a second opening 63' in the cylinder wall 25', and a second piston head 33' can be disposed in the cylinder 27'.
  • the second piston head 33' can have a second piston bowl 35' at least partially defined by a second wall 51' having a generally spiral shape in a top 39' of the second piston head.
  • the top 39' of the first piston head 33 ' faces the top of the second piston head.
  • the piston heads 33' can be replaced by the piston heads 33 shown in, e.g., FIGS. I -3C.
  • At least one inlet port 71 * ordinarily a plurality of inlet ports can be pro vided in the cylinder wall 25' below a top dead center (TDQ and above a bottom dead center (BDC) of the first or "upper" piston head 33' and at least one Outlet port 73 (and ordinarily a plurality of outlet, ports) can be provided in the cylinder wall below a TDC and above a BDC of the second or "lower” piston head 33' .
  • references to "above” and “below” when referring to TDC or BDC relate to the positions of the pistons in the cylinder, where IDC will always be considered to be above BDC, regardless of the orientation of the cylinder or the direction of movement of the piston head toward TDC or BDC.
  • the center portions 1 of the first and second piston bowls 35 can be substantially circul ar in shape, and a central axis AI of the at least one inlet port 71 can be offset relative to the central axis AC of the cylinder 27 and substantially tangent to the center portions of the first and second piston bowls.
  • the piston head 33 seen in FIG. 6A would be the lower piston head
  • a central axis AO of the at least one outlet port.73 can also be offset relative to the central axis AC of the cylinder 27 and substantially tangent to the center portions 41 of the first and second piston bowls 35. in the embodiment of the engine 21 ' seen in FIGS.
  • the piston head 33 seen in FIG, 6B would also be the lower piston head.
  • the inlet ports 7 and outlet ports 73' of the cylinders 27' shown in F IGS. 5A-5B will ordinarily also be oriented in the .manner shown in. FIGS. 6A and 6B.
  • inlet ducts 75 * and outlet ducts 77' can extend around the cylinder 27' and lead to each, of a plurality of inlet ports 7 ⁇ and outlet ports 73 ' , respectively.
  • the first and second spiral shaped walls 137 and 151 can increase in depth from the outer ends 145 and 159 of the first and second spiral shaped walls toward inner ends 149 and 165 of the first and second spiral shaped walls at a substantially circular center portion 141 of the piston bowl 135.
  • the inner ends 149 and 165 of the first and second spiral shaped walls 137 and 151 can merge into an S-shaped partition 167 between two concave portions 141a and 141 b of the center portion of the piston bowl.
  • the concave portions 141a and 141b form a ' ia and yang" geometry when viewed along the central axis of the piston head.
  • the concave portions 141a and 141 b are generally teardrop shaped in that they increase from a minimal depth at the outer end of the spiral shaped walls to a largest depth close to the inner end of the spiral shaped walls and then back to a zero depth over a relatively short distance.
  • this geometry further facilitates mixing of fuel and air by causing the gas and foe! to "tumble" in the sense that, after proceeding downwardly into the bowl 135, it is then caused to move upwardly again, as well, as to "swirl” by moving circumferentially around the bowl.

Landscapes

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

Abstract

An engine includes a combustion chamber including a cylinder wall defining a cylinder, a fuel injector disposed in a first opening in the cylinder wall and a piston head disposed in the cyiinder. A piston bowl at least partially defined by a wall having a generally spiral shape is provided in a top of the piston head.

Description

COMBUSTION CHAMBER FOR AN INTERNAL COMBUSTION ENGINE AND AN INTERN AL COMBUSTION ENGINE
BACKGROUND AND SUMMARY
Aspects of the presen t in vention relate generally to internal combustion engines and, more particularly, to combustion chambers for internal combustion engines.
Opposed piston engines include a cylinder with a pair of pistons that move toward each other toward top dead center positions to compress gas in the cylinder and near which fuel is injected through a side wall of the cyiinder. LIS, Patent App, US2012/0285418 and L S, Patent App. US2013/0036999, which are incorporated by reference, describe the general structure and operation of an opposed piston engine. U .S . Patent App. 1182012/0285418 observes that such engines require different arrangements for effective mixing of fuel, and air. Providing for effective mixing of fuel in air in conventional engine cy linders is, of course, also importan
It is desirable to provide an arrangement for effectively mixing fuel and air in an engine cylinder, particularly for an opposed piston engine cylinder.
According to an aspec t of the present invention, a combustion chamber for an internal combustion engine comprises a cylinder wall defining a cylinder, a fuel injector disposed in a first opening in the cylinder wall, and a pisto head disposed in the cylinder, a piston bowl at least partially defined by a wall having a generally spiral shape being provided in a top of the piston head.
According to another aspect of the invention, an engine comprising such a combustion chamber is provided. BRIEF DESCRIPTION OF THE D AWINGS
The features and advantages of the present invention are well understood by reading the following detailed description in conjunction with the drawings in which like numerals indicate similar elements and in which:
FIG. I is a top, partially cross-sectional view of an internal combustion engine according to an aspect of the present invention;
FIG. 2 is a perspecti ve view of piston heads of an internal combustion engine according to an aspect of the present invention;
FIGS. 3A-3B are top perspective and top views of a piston head of an internal
combustion engine according to an aspect of the present invention, and FIG. 3C is a cross- sectional view taken at section 3C-3C of FIG. 3B;
FIGS. 4A-4B are top views of a piston head of an internal combustion engine according to another aspect of the present invention, with FIG. 4B showing orientations of fuel injectors relative to the piston head;
FIGS. 5A-5B are side, partially cross-sectional views of an internal combustion engine according to another aspect of the present invention;
FIG. 6A is a top view of a piston in an internal combustion engine according to an aspect of the present invention, showing an orientation of inlet ports in a cylinder relative to an tipper piston of an opposed piston, engine;
FIG. 6B is a top view of a piston in an internal combustion engine according to an aspect of the present invention showing an orientation of outlet ports relative to a lower piston of an opposed piston engine; and FIG , 7 A is a top view of a piston head according to another aspect of the present
invention, FIG. 7B is a perspective view of piston heads of the tvpe shown in FIG. 7 A, and FIG . 7C is a cross-sectional view taken at section 7C-7C of the piston head of FIG. 7 A.
DETAILED DESCRIPTION
An internal combustio engine 2 i according to an aspect of the presen invention is seen in FIG. I and comprises a combustion chamber 23 comprising a cylinder wa l 25 defining a cylinder 27, The cylinder wall 25 is ordinarily part of a cviinder liner or an engine block. As seen in FIGS. 1 and 2, a fuel injector 29 is disposed in a first opening 3 1 in the cylinder wall 25, A piston head 33 is movably disposed in the cylinder 25 and is linked to a crankshaft (not shown in FIGS. I or 2) by a connecting rod (sometimes referred to as a conrod or pushrod) (not shown in FIGS. I or 2). FIG. 2 shows piston heads 33 and 33 U of an opposed piston arrangement, with the upper piston head 33U tilted to permit illustration of fuel jets FJ injected by fuel injectors 29.
As seen, for example, in the piston head 33 shown in FIGS. 3A-3C, a piston bowl 35 that is at least partially defined by a wall 37 having a generally spiral shape is provided i a top 39 of the piston head 33. While the spiral may be a specific form of spiral, such as a logarithmic spiral, an Archimedean spiral, a hyperbolic spiral, etc., except where otherwise indicated, a
"spiral" will be understood to be a curve that, gets progressively closer to a central point as it revolves around the point. References to the "top" of the pisto head 33 are intended to refe to the part of the piston head that, with the c viinder wail 25 defines the combustion chamber 23. It will be apprec iated that the piston head may be oriented in an engine so that the "top" of the piston head is in fact vertically below the rest of the pi ston head (suc as i s seen in the upper piston head in the opposed piston arrangement shown in FIGS. 2, 5A and 5B), horizontally even with the rest of the piston head (suc as when the cylinder 27 extends horizontally), or
somewhere in between above, below, and horizontally even with,
hi the embodiment shown in FIG. 2, it will be seen that the upper piston head 33U has a bowl 35U with a geometry that is a mirror image of the bowl. 35 of the lower piston head 33. References herein to the piston head 33 or the bowl 35 of the piston head will be understood to apply equally to the upper piston head 33U and bowl 35U, the onl differences being that the geometry of the bowls are reversed on the two piston heads. The volume of the pisto bow! 35 depends upon a compression ratio that is desired to be obtained by the piston head 33 and cylinder 27. A depth of the spiral shaped wall 37 increases toward a center portion 41 of the pisto bowl 35. In the embodiment shown in FIGS. 3A-3C, the pisto bowl 35 is further defined by a ramp 43 that is defined on one edge by the spiral shaped wall 37 and on another edge by the center portion 41 of the piston bowl and that descends from the top surface 53 of the piston head 33 to the center portion at a distance below the top surface. The fuel injector 29 can be oriented relative to piston bowl 35 so that a centra! axis AJ of an injected fuel jet FJ is generally parallel with the ramp 43 which can facilitate causing the mixture to "tumble" in the sense that, after proceeding downwardly into the bow! 35, it then moves upwardly again, as wei! as to "swirl" by moving circuniferentially around the bowl The fuel injector may, alternatively, be oriented so that the central axis of the injected fuel jet is generally perpendicular to a central axis AC of the cylinder as illustrated.
As seen in another embodiment of the piston bowl 35" shown in FIGS. 4A-4B, the outer end 45' of the spiral shaped wall 37* may extend to the peripheral edge 47' of the top 39' of the piston head. 33' and the bowl may have no ramp. As seen in FIGS. 5A-58, in such an
embodiment, the fuel injectors can be (but is not necessarily) oriented so thai the central, axis of the injected fuel jet Pi is generally perpendicular to a central axis AC of the cylinder. The fuel injectors can, alternatively, be disposed at an angle to the perpendicular, which can further facilitate mixing of gas and fuel by causing the .mixture to "tumble" in. the sense that, after proceeding downwardly into the bowl 35 ', it then moves upwardly again, as well as to "swirl" by moving circumferential iy around the bowl.
The spiral shape of the walls 37 and 37' facilitates creati on of a circumferential swirling effect in the cylinder 27 and 27' that facilitates mixing of the injected fuel with incoming air and later with scavenging of exhaust gas. While dimensions will vary depending upon factors such as the size of the piston head 33 and cylinder 27, for a fuel jet FJ thai is typically about 50 mm in length, the length of the wails 37 and 37' will ordinarily be between about 20 and 100 mm, more preferably between about 30 and 60 mm. In the illustrated embodiments, the circumferential swirling effect will be in the clockwise direction, however, it will be appreciated that the effect could alternatively be in the counter-clockwise direction
As seen in the embodiment shown in FIGS. 3A-3B, the center portion 41 of the piston bowl 35 is ordinarily substantially circular in shape. This is true, as well, for the embodiment of the piston bowl 35 ' shown in FIGS. 4A-4B, as illustrated by the dotted line representing the circular central portion 41 \ however, the circula 'shape is more apparent in FIGS. 3A-3B. The spiral shaped wall 37 typically increases in depth from the outer end 45 of the spiral shaped wall toward an inner end 49 of the spiral shaped wall at the center portion 41. "Substantially" circular is defined herein as meaning approximating circular, but not necessarily exactly circular, as the precise boundaries of the substantially circular- central portions may not be capable of precise definition as different surfaces merge into each other, or (as in the piston heads 33' shown in. FIGS. 4A.-4B) the shapes do not As seen in FIG. 3C (cross-section of piston head), the center portion 4! of the piston bowl 35 can be substantially flat or. as shown in phantom, concave. Altering the depth and total volume of the piston bowl 35 alters the compression ratio that is desired to be obtained by the piston bead 33 and cylinder 27.
In the embodiment shown in FIGS. 3A-3C, the bowl 35 of the pisto head 33 is at least partially defined by a second wall 5 i having a generally spiral shape. The first spiral shaped wall 37 and the second spiral shaped wall 51 are ordinarily rotationally symmetrical about the central axis AC of the cylinder 27. hi the embodiment shown in FIGS. 3A-3C, a top surface 53 of the top 39 of the piston head 33 is substantially flat, and the piston bowl 35 and tlie first and second spiral shaped walls 37 and 5 i are recessed relative to the top surface. First and second recesses 55 and 57 defining outer ends 45 and 59 of the first and second spiral shaped walls 7 and 51 , respecti vely, can be disposed inwardly from an outer peripheral edge 47 of the top 39 of the piston head 33.
As seen, for example, in FIGS. 1 and 2, a. second fuel injector 61 can also be provided i a second opening 63 in the cylinder wall 25. The first and second fuel injectors 29 and 61 ca be oriented relative to the piston bowl 35 so that central axes AJ of injected fuel jets FJ from the first and second fuel injectors are generally aligned with centers of the first and second recesses 55 and 57, Ordinarily, a center portion 41 of the piston bowl 35 is substantiall circular in shape, and the first and second fuel injectors 29 and 61 are oriented relative to the piston bowl so that central axes. AJ of injected fuel jets FJ from the first and second fuel injectors are offset relative to the central axis of the piston 33 so that they are tangent to the circle, or nearly tangent thereto, as illustrated in FIG. I. The injectors 29 and 61 are illustrated as being disposed at
approximately 180 degrees around the circumference of the cylinder 25 from each other, however, it is possible that the injectors could disposed at different angular relationships. Additionally, although two injectors are shown in the illustrated embodiments, it will be appreciated that one or more than two injectors may be provided, in different embodiments. in the embodiment of the piston head 33' shown in FIGS. 4A-4B, a periphery 47 Of the top 39* of the piston head is recessed at an outer end 45' of die spiral shaped wall 37', i.e., the spiral shaped wall extends all the way to the periphery of the top of the piston head to define a recess 69'. As seen in FiG, 4B, the fuel injectors 29' and 6 are oriented relative to piston bowl 35' so that a central axis A J of an injected fuel jet FJ is generally aligned with a center of the recess 69'. As seen, for example, in FIGS. 5A and 5B, the piston head 33' is ordinarily used with another upper piston head 331Γ in an opposed piston engine 2 . The piston head 33' and the upper pisto head 33 LP will be mirror images of each other, except that one is rotated 180 degrees around a central, axis of the cylinder to the other. As before, references to the piston head 33' will be understood to appl equall to the piston head 331J\ except where otherwise indicated. It will be appreciated that an opposed piston engine 21 using the piston heads 33 shown in FIGS. 1-3C can hav the same basic constructions as the opposed piston engine 21 ' shown in FIGS. 5A-5B. Particularly when the two piston heads 33' and 33U' approach top dead center (T'DC) and the spiral shaped walls 37' of the two piston heads are at their closest to the tops of the other one of the piston heads, the center portion 4 of the resulting piston bowl 35' is more clearly substantially circular in shape. As seen in FIG, 4B, the central axis AJ of the injected fuel jet. FJ is offset from the central axis of the piston so that ft i tange t to, or nearly tangent to, the resulting circle at the center portion 41. ',. The circle 41 ' defined by the spiral shaped wall 37' of the piston head 33' may be offset from the circle defined by the spiral shaped wall of the upper piston head 33U'. By not including a ramp, the spiral shaped walls 37' of the piston heads 33' and 33 U' can be rather high, which can be helpful to avoid spraying fuel on the cylinder wall or liner.
Referring, for purposes of discussion, to FIGS. 5A-5B, a second fuel injector 61 ' can be disposed in a second opening 63' in the cylinder wall 25', and a second piston head 33' can be disposed in the cylinder 27'. The second piston head 33' can have a second piston bowl 35' at least partially defined by a second wall 51' having a generally spiral shape in a top 39' of the second piston head. The top 39' of the first piston head 33 ' faces the top of the second piston head. It will be appreciated that the piston heads 33' can be replaced by the piston heads 33 shown in, e.g., FIGS. I -3C.
As see in FIG. 5A (in phantom) and FIG. SB, at least one inlet port 71* ordinarily a plurality of inlet ports) can be pro vided in the cylinder wall 25' below a top dead center (TDQ and above a bottom dead center (BDC) of the first or "upper" piston head 33' and at least one Outlet port 73 (and ordinarily a plurality of outlet, ports) can be provided in the cylinder wall below a TDC and above a BDC of the second or "lower" piston head 33' . References to "above" and "below" when referring to TDC or BDC relate to the positions of the pistons in the cylinder, where IDC will always be considered to be above BDC, regardless of the orientation of the cylinder or the direction of movement of the piston head toward TDC or BDC. References to "upper" or "lower" when referring to the two piston heads 33' are onl with reference to their positions in the embodiment illustrated, and ft will be appreciated that the cylinder 27' can be oriented differently than shown with the inlet ports vertically above the outlet ports, such as where the inlet and outlet ports are horizontally even with each other, the inlet potts are all vertically below the outlet ports, or something in between with some inlet ports being above some outlet ports and some outlet ports being above some inlet ports. As seen in FIG. 6A, which shows a piston head 33 as in FIGS. 1 -3C, the center portions 1 of the first and second piston bowls 35 can be substantially circul ar in shape, and a central axis AI of the at least one inlet port 71 can be offset relative to the central axis AC of the cylinder 27 and substantially tangent to the center portions of the first and second piston bowls. In the embodiment of the engine 21 * seen in FIGS. 5A and 5B, the piston head 33 seen in FIG. 6A would be the lower piston head, As see in FIG. 6B, a central axis AO of the at least one outlet port.73 can also be offset relative to the central axis AC of the cylinder 27 and substantially tangent to the center portions 41 of the first and second piston bowls 35. in the embodiment of the engine 21 ' seen in FIGS. 5A and 5B, the piston head 33 seen in FIG, 6B would also be the lower piston head. The inlet ports 7 and outlet ports 73' of the cylinders 27' shown in F IGS. 5A-5B will ordinarily also be oriented in the .manner shown in. FIGS. 6A and 6B. The
orientation of the inlet ports 71 and outlet ports 73 i the manner shown in FIGS. 6 A and 6B, together with the spiral shape of the walls 37 (and 37' for the piston 33 ' of FIGS. 4A-5B) facilitates creation of a circumferential swirling effect in the cylinder 27 that facilitates mixing of the injected fuel with incoming air and later with scavenging of exhaust gas. It will be appreciated that, instead only one of the central axes ΑΪ or AO of the inlet potts 71 or the outlet ports 73, or none, might, instead be substantially tangent to the center portions 4i ' of the first and second piston bowls 35, As seen in FIG. 5A, inlet ducts 75* and outlet ducts 77' (shown as transparent, features) can extend around the cylinder 27' and lead to each, of a plurality of inlet ports 7Γ and outlet ports 73', respectively.
In a further embodiment shown in FIGS. 7A-7C, the first and second spiral shaped walls 137 and 151 can increase in depth from the outer ends 145 and 159 of the first and second spiral shaped walls toward inner ends 149 and 165 of the first and second spiral shaped walls at a substantially circular center portion 141 of the piston bowl 135. The inner ends 149 and 165 of the first and second spiral shaped walls 137 and 151 can merge into an S-shaped partition 167 between two concave portions 141a and 141 b of the center portion of the piston bowl. The concave portions 141a and 141b form a ' ia and yang" geometry when viewed along the central axis of the piston head. The concave portions 141a and 141 b are generally teardrop shaped in that they increase from a minimal depth at the outer end of the spiral shaped walls to a largest depth close to the inner end of the spiral shaped walls and then back to a zero depth over a relatively short distance. As seen b the arrows reflecting the flow of gas in the concave portions 141 and 141 b, this geometry further facilitates mixing of fuel and air by causing the gas and foe! to "tumble" in the sense that, after proceeding downwardly into the bowl 135, it is then caused to move upwardly again, as well, as to "swirl" by moving circumferentially around the bowl.
In the present application, the use of terms such as "including" is open-ended and is intended to have the same meaning as terms such as "comprising" and not preclude the presence of other structure, material, or acts. Similarly, though the use of terms such as "can" or "may" is intended to be open-ended and to reflect that structure, material, or acts are not necessary, the failure to use such terms is not intended to reflect that structure, material, or acts are essentia!. To the extent that structure, material, or acts are presently considered to be essential, they are identified as such.
While this invention has been illustrated and described in accordance with a preferred embodiment, it is recognized that variations and changes may be made therein without departing from the invention as set forth in the claims.

Claims

WHAT IS CLAIMED IS:
1. A combustion chamber for an internal combustion, engine, comprising;
a cylinder wall defining a cylinder;
a fuel injector disposed in a first opening in the cylinder wall;
a piston head disposed in the cylinder, a piston bow! at least partially defined by a wall having a generally spiral shape being provided in a top of the piston head.
2. The combustion chamber for an internal combustion engine as set forth in claim I, wherein a depth of the spiral shaped wail increases toward a center portion of the piston bowl,
3. The combustion chamber for a internal combustion engine as set forth in claim 2, wherein the piston bowl is further defined by a ramp defined on one edge by the spiral shaped wall and on another edge by the center portion of the piston bowl.
4. The combustion chamber for an internal combustion engine as set forth in claim 3» wherein the fuel injector is oriented reiative to piston bowl so thai a central axis of an injected fuel jet is generally perpendicula to a central axis of the piston.
5. The combustion chamber for a internal combustion engine as set forth i claim 1 , wherein a center portion of the piston bowl is substantially circular in shape.
I I
6. The combustion chamber for an internal combustion engine as set forth in claim 5, wherein the spiral shaped waii increases in depth from the outer end of the spiral shaped wai l toward an inner end of the spiral shaped wall at the center portion.
7. The combustion chamber for an internal combustion engine as set forth in ciaim 5, wherein the center portion of the piston bowl is substantially flat.
8. The combustion chamber for an internal combustion engine as set forth in claim 5, wherein the center portion of the piston bowl is concave,
9. The combustion chamber for a internal combustion engine as set forth in. claim 1 , wherein the piston bowl is at least partially defined by a second wall having a generally spiral shape.
.10. The combustio cimmber for an internal combustion engine as set forth i claim 9, wherein the first spiral shaped wail and the second spiral shaped wall are rotationally symmetrical.
1 . The combustion chamber for an internal combustion engine as set forth in claim 9, wherein a top surface of the top of the piston head is substantially flat, and the pisto bowl and the first and second spiral shaped walls are recessed relative to the top surface.
12. The combustion chamber for an internal combustion engine as set forth in claim 1 1 , wherein fi rst and second recesses defining outer ends of the first and second spiral shaped walls are disposed i nwardly from an outer peripheral edge of the top of the piston head .
13. The combustion chamber for an internal combustion engine as set forth in claim 12, comprising a second fuel injector, wherein the first and second fuel injectors are oriented relative to the piston bo wl so that central axes of injected fuel jets from the fi rst and second fuel injectors are generally al igned with centers of the first and second recesses.
14. The combustion chamber for an internal, combustion engine as set forth in claim 9, wherein a center portion of the piston bowl is substantially circular in shape, the combustion chamber comprising a second fuel injector, wherein the first and second fuel injectors are oriented relative to the piston bow! so that central axes of injected fuel jets from the first and second fuel injectors are tangent to the circle.
15. The combustio chamber for an internal combustion engine as set forth in claim 9, wherein the first and second spiral shaped walls increase i depth from the outer ends of the first and second spiral shaped wails toward an inner end of the first and second spiral shaped walls at a substantially circular center portion of the piston bowl.
16. The combustion chamber for an internal combustion engine as set forth in claim 1 , wherein the irmer ends of the .first and second spiral shaped wall s m erge into an S-shaped partition between two concave portions of the center portion of the piston bowl.
17. The combustion chamber for an internal combustion engine as set forth in claim 1 , wherein the spiral shaped wall is between 20 - 100 mm in length.
18, The combustion chamber for an interna! combustion engine as set forth in claim I, wherein a periphery of the top of the piston head is recessed at an outer end of the spiral shaped wail
1 , The combustion chamber for an internal combustion engine as set forth in claim 18, wherein the fuel injector is oriented relative to piston bowl so that a central axis of a injected fuel jet is generally aligned with a center of the recess.
20. The combustion chamber for an internal combustion engine as set forth in claim 1 , wherein a center portion of the pi ston bowl is substantially circular in shape and the central axis of the injected fuel jet is tan gen t to the circle ,
21 , The combustion chamber for an internal combustion engine as set forth in claim 1 ,
comprising a second fuel injector disposed in second opening in the cylinder wall, and a. second piston head disposed in the cylinder, a second piston bowl, at least partially defined by a second wall having a general ly spiral shape being provided in a top of the second piston head, the top of the fi rst piston head facing the top of the second piston head,
22. The combustion chamber for an internal combustion engine as set forth in claim 2.1 , wherein the second piston head is a mirror image of the first piston head.
23. The combustion chamber for an internal combustion engine as set forth in claim 21 , comprising at least one inlet port in the cylinder wall below a top dead center and above a bottom dead center of the first piston head and at least one outlet port in the cylinder wail below a top dead center and above a. bottom dead center of the second piston head.
24. The combustion chamber for an internal combustion engine as set forth in claim 23, wherein center portions of the first and second piston bowls are substantially circular in shape, and- a central axis of the at least one inlet port is offset relative to the central axis of the cylinder and substantially tangent to the center portions of the first and second pisto bowls.
25. The combustion chamber for an internal combustion engine as set forth in claim 24, wherein a central axis of the at least one outlet port is offset relative to the central axis of the cylinder and substantial ly tangent to the center portions of the first and second piston bowls.
26, The combustion chamber for an internal combustion engine as set forth in claim 23, wherei center portions of the first and second piston bowls ar substantially circular in shape, and a central axis of the at least one outlet port is offset rel ative to the cen tral ax is of the cylinder and substantially tangent to the center portions of the first and second piston bowls.
27, An infernal combustion engine comprising a combustion chamber as set. forth in claim ί .
PCT/US2014/035773 2014-04-29 2014-04-29 Combustion chamber for an internal combustion engine and an internal combustion engine WO2015167444A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US15/303,000 US10415456B2 (en) 2014-04-29 2014-04-29 Combustion chamber for an internal combustion engine and an internal combustion engine
EP14890716.5A EP3140527B1 (en) 2014-04-29 2014-04-29 Combustion chamber for an internal combustion engine and an internal combustion engine
PCT/US2014/035773 WO2015167444A1 (en) 2014-04-29 2014-04-29 Combustion chamber for an internal combustion engine and an internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2014/035773 WO2015167444A1 (en) 2014-04-29 2014-04-29 Combustion chamber for an internal combustion engine and an internal combustion engine

Publications (1)

Publication Number Publication Date
WO2015167444A1 true WO2015167444A1 (en) 2015-11-05

Family

ID=54359003

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2014/035773 WO2015167444A1 (en) 2014-04-29 2014-04-29 Combustion chamber for an internal combustion engine and an internal combustion engine

Country Status (3)

Country Link
US (1) US10415456B2 (en)
EP (1) EP3140527B1 (en)
WO (1) WO2015167444A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3176403A1 (en) * 2015-12-02 2017-06-07 Caterpillar Energy Solutions GmbH Piston for a gaseous fuel internal combustion engine
JP2018513936A (en) * 2015-03-31 2018-05-31 アカーテース パワー,インク. Asymmetrically shaped combustion chamber of opposed piston engine

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9995203B2 (en) * 2016-10-27 2018-06-12 Caterpillar Inc. Piston design for flow re-direction
CN111033009B (en) * 2017-09-07 2023-09-05 阿凯提兹动力公司 Piston assembly with opposed injection regions for opposed piston engine
US10876495B2 (en) * 2018-10-11 2020-12-29 Caterpillar Inc. Piston design for splitting jets into streams
US11555469B2 (en) * 2020-06-29 2023-01-17 Cummins Inc. Piston bowls
US11959436B2 (en) * 2022-09-20 2024-04-16 Tenneco Inc. Piston including spiral features to increase in-cylinder swirl

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2231392A (en) * 1939-01-26 1941-02-11 John J Mccarthy Internal combustion engine
US2766738A (en) * 1953-07-24 1956-10-16 Daimler Benz Ag Internal combustion engine
US20110271932A1 (en) * 2010-04-27 2011-11-10 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US20120073541A1 (en) * 2010-08-16 2012-03-29 Achates Power, Inc. Fuel injection spray patterns for opposed-piston engines

Family Cites Families (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE102658C1 (en) *
US1856328A (en) * 1926-11-24 1932-05-03 Louis O French Internal combustion engine
US2269084A (en) * 1941-05-03 1942-01-06 John J Mccarthy Internal combustion engine
US2504036A (en) * 1945-08-24 1950-04-11 Morrison Alfred Charles Combustion chamber for internal-combustion engines
US2600440A (en) * 1950-05-17 1952-06-17 Donald H Smith Piston construction for internal-combustion engines
US2851019A (en) * 1956-06-29 1958-09-09 Gen Motors Corp Combustion chamber for internal combustion engine
DE1451636A1 (en) * 1963-09-21 1969-07-10 Daimler Benz Ag Diesel engine, especially four-stroke engine for motor vehicles
GB1293855A (en) * 1969-05-24 1972-10-25 Daimler Benz Ag Four-stroke internal combustion engines
JPS5949407B2 (en) * 1976-11-15 1984-12-03 トヨタ自動車株式会社 Combustion chamber of internal combustion engine
JPS57171026A (en) 1981-04-16 1982-10-21 Nippon Soken Inc Direct injection type diesel engine
US4467752A (en) * 1982-06-21 1984-08-28 Motortech, Inc. Internal combustion engine
JPS6314836U (en) * 1986-07-14 1988-01-30
DE3629437A1 (en) * 1986-08-29 1988-03-03 Elsbett L FUEL INJECTION FOR PISTON COMBUSTION ENGINE WITH SEVERAL INJECTORS
JPS63113113A (en) * 1986-10-31 1988-05-18 Matsukichi Haruyama Piston structure of internal combustion engine
US5103784A (en) * 1990-02-07 1992-04-14 The Univeristy Of British Columbia Squish jet combustion chamber
US5065715A (en) * 1990-02-07 1991-11-19 The University Of British Columbia Squish jet combustion chamber
JPH084535A (en) * 1994-06-17 1996-01-09 Kubota Corp Piston of direct injection type diesel engine
US6003487A (en) * 1995-08-05 1999-12-21 Merritt; Dan Internal combustion engine
AT2432U1 (en) * 1997-10-16 1998-10-27 Avl List Gmbh INTERNAL COMBUSTION ENGINE
JP3767125B2 (en) * 1997-10-21 2006-04-19 日産自動車株式会社 Piston for in-cylinder internal combustion engine
US6182619B1 (en) * 1998-12-24 2001-02-06 General Atomics Aeronautical Systems, Inc. Two-stroke diesel engine
AUPQ092199A0 (en) * 1999-06-14 1999-07-01 Aardvark Pty. Ltd. Internal combustion engine
JP4149621B2 (en) * 1999-09-03 2008-09-10 邦彦 奥平 Opposed piston type 2-cycle uniflow type engine
DE19957461A1 (en) * 1999-11-29 2001-06-07 Adolf Filmann Swirl channels for combustion chambers in IC engines extend from cylinder edge to combustion chamber with tangential entry into combustion chamber aperture
US6418885B1 (en) * 2000-03-17 2002-07-16 Marius A. Paul Total energy general optimized engine cycle
US6609490B2 (en) 2001-11-15 2003-08-26 John Flinchbaugh Piston head for a spark ignition engine
US7360511B2 (en) * 2004-06-10 2008-04-22 Achates Power, Inc. Opposed piston engine
JP4100401B2 (en) * 2005-02-24 2008-06-11 トヨタ自動車株式会社 Internal combustion engine
US8561581B2 (en) * 2009-08-04 2013-10-22 Jack R. Taylor Two-stroke uniflow turbo-compound internal combustion engine
US20110067671A1 (en) * 2009-09-01 2011-03-24 Laimboeck Franz J Non-soot emitting fuel combustion chamber
US20110114070A1 (en) * 2009-11-18 2011-05-19 Achates Power, Inc. Apparatus and method for controlling swirl in a ported, two-stroke, internal combustion engine
DE202009017699U1 (en) * 2009-11-18 2010-09-23 Daude, Otto, Dr.-Ing. MBA Tangentially aligned on the cylinder circumference injection nozzles for internal combustion engines with gas exchange control
US20110186017A1 (en) * 2010-02-03 2011-08-04 Achates Power, Inc. Single-crankshaft, opposed-piston engine constructions
US9512779B2 (en) * 2010-04-27 2016-12-06 Achates Power, Inc. Swirl-conserving combustion chamber construction for opposed-piston engines
US10180115B2 (en) * 2010-04-27 2019-01-15 Achates Power, Inc. Piston crown bowls defining combustion chamber constructions in opposed-piston engines
EP2712394B1 (en) * 2011-05-18 2016-12-14 Achates Power, Inc. Combustion chamber construction for opposed-piston engines
GB2493061A (en) * 2011-07-15 2013-01-23 Ecomotors Internat Inc Opposed piston engine with toroidal combustion chamber
GB2493260A (en) * 2011-07-26 2013-01-30 Ecomotors Internat Inc Opposed piston engine with tumble flow in shaped combustion chamber
US20130036999A1 (en) 2011-08-08 2013-02-14 Ecomotors International, Inc. High-Squish Combustion Chamber With Side Injection
GB2496479A (en) * 2011-11-11 2013-05-15 Ecomotors Internat Inc Intake System for an Opposed-Piston Engine
DE102012111776A1 (en) * 2011-12-09 2013-06-13 Ecomotors International, Inc. Opposed piston engine with annular combustion chamber with side injection

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2231392A (en) * 1939-01-26 1941-02-11 John J Mccarthy Internal combustion engine
US2766738A (en) * 1953-07-24 1956-10-16 Daimler Benz Ag Internal combustion engine
US20110271932A1 (en) * 2010-04-27 2011-11-10 Achates Power, Inc. Combustion chamber constructions for opposed-piston engines
US20120073541A1 (en) * 2010-08-16 2012-03-29 Achates Power, Inc. Fuel injection spray patterns for opposed-piston engines

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3140527A4 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018513936A (en) * 2015-03-31 2018-05-31 アカーテース パワー,インク. Asymmetrically shaped combustion chamber of opposed piston engine
EP3176403A1 (en) * 2015-12-02 2017-06-07 Caterpillar Energy Solutions GmbH Piston for a gaseous fuel internal combustion engine

Also Published As

Publication number Publication date
US10415456B2 (en) 2019-09-17
EP3140527A4 (en) 2017-12-27
EP3140527A1 (en) 2017-03-15
EP3140527B1 (en) 2020-11-18
US20170067391A1 (en) 2017-03-09

Similar Documents

Publication Publication Date Title
EP3140527A1 (en) Combustion chamber for an internal combustion engine and an internal combustion engine
US9482145B2 (en) Toroidal combustion chamber with side injection
US8997710B2 (en) Fuel injector support constructions for direct injection opposed-piston engines
US9211797B2 (en) Combustion chamber construction with dual mixing regions for opposed-piston engines
US20160017839A1 (en) Piston Engine with Non-Circular Combustion Chamber
JP6069306B2 (en) Internal combustion engine
US10309294B2 (en) Engine
US10161371B2 (en) Opposed piston three nozzle piston bowl design
JP2014515454A (en) Internal combustion engine
US10422272B2 (en) Compact ported cylinder construction for an opposed-piston engine
JP2002502932A (en) Internal combustion engine
US10760526B2 (en) Piston for internal combustion engine
CN108260358B (en) Engine piston with grooved top land
EP3176402A1 (en) Piston for a gaseous fuel internal combustion engine
US20220416514A1 (en) Spark plug for internal combustion engine
JP2019120185A (en) Structure of cylinder peripheral wall surface
JP2021080899A (en) Internal combustion engine
US10280831B2 (en) Engine
JPH108968A (en) Piston for internal combustion engine
JP2020191161A (en) Internal combustion engine and spark plug
EP3379050B1 (en) Internal combustion engine
WO2013101832A1 (en) Piston and combustion chamber
JPH0112925B2 (en)
RU2020138705A (en) Two-stroke internal combustion engine
GB2557266A (en) Piston bowl

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 14890716

Country of ref document: EP

Kind code of ref document: A1

DPE1 Request for preliminary examination filed after expiration of 19th month from priority date (pct application filed from 20040101)
WWE Wipo information: entry into national phase

Ref document number: 15303000

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

REEP Request for entry into the european phase

Ref document number: 2014890716

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2014890716

Country of ref document: EP