US3923032A - Chambered piston for an internal combustion engine - Google Patents

Chambered piston for an internal combustion engine Download PDF

Info

Publication number
US3923032A
US3923032A US462642A US46264274A US3923032A US 3923032 A US3923032 A US 3923032A US 462642 A US462642 A US 462642A US 46264274 A US46264274 A US 46264274A US 3923032 A US3923032 A US 3923032A
Authority
US
United States
Prior art keywords
piston
chamber
nozzle
combustion chamber
wedge
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
US462642A
Inventor
Karl E Studenroth
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US462642A priority Critical patent/US3923032A/en
Application granted granted Critical
Publication of US3923032A publication Critical patent/US3923032A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0636—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space having a substantially flat and horizontal bottom
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0603—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston at least part of the interior volume or the wall of the combustion space being made of material different from the surrounding piston part, e.g. combustion space formed within a ceramic part fixed to a metal piston head
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0633—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space being almost completely enclosed in the piston, i.e. having a small inlet in comparison to its volume
    • 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/0015—Multi-part pistons
    • F02F3/0023—Multi-part pistons the parts being bolted or screwed together
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/26—Pistons  having combustion chamber in piston head
    • 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
    • F02B1/00—Engines characterised by fuel-air mixture compression
    • F02B1/02—Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04—Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into 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
    • F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618—Other 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
    • F02B23/0621—Squish flow
    • 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
    • F02B3/00—Engines characterised by air compression and subsequent fuel addition
    • F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

  • a piston for an internal combustion engine is provided with an interior chamber of relatively large crosssectional area clg about 30 percent of the piston area, and a nozzle of relatively smaller throat area, e.g., about 3 to 5 percent of the piston area, opening into the combustion chamber of the engine.
  • a nozzle of relatively smaller throat area e.g., about 3 to 5 percent of the piston area
  • the chamber in the piston of the present invention has a unique shape, somewhat like a bottle, with an interior of relatively large cross-sectional area and a neck or nozzle portion with an opening or throat of relatively small cross-sectional area.
  • the piston chamber preferably has a flat wall at the end opposite the nozzle opening, the flat wall being normal to the direction of travel of the piston. From the flat wall, the piston chamber tapers and/or curves convergingly toward the smaller nozzle opening.
  • the nozzle portion itself, first converges toward a minimum diameter throat and then diverges to open onto the outer surface or crown of the piston.
  • the piston may be made of two members which are secured together.
  • the air in case of a fuel-injection engine, and/or fuel-air mixture, in case of a spark ignition engine, is concentrated in the chamber of the piston during the comprssion stroke.
  • the expanding gases first act on the flat wall of the piston chamber opposite the nozzle opening and then expand out the nozzle to act on the outer surface or crown of the piston in a conventional manner to drive the piston so that the expanding gases do additional work and produce additional power.
  • FIG. I is a cross-sectional view of one embodiment of a chambered piston of the present invention for a reciprocating engine
  • FIG. 2 is a cross-sectional view of a second embodiment of a chambered piston of the present invention for a reciprocating enging;
  • FIG. 3 is a cross-sectional view of a third embodiment of a chambered piston of the present invention for a rotary engine
  • FIG. 4 is an elevational view taken in the direction of the arrows 44 in FIG. 3 with a portion broken away;
  • FIG. 5 is a plan view taken in the direction of the arrows 5-5 in FIG. 4.
  • FIG. I illustrates a chambered piston according to the present invention which is suitable for use in an internal combustion engine having engine walls which in conjunction with the chambered piston 10 form a combustion chamber II.
  • the engine is of the reciprocating type and has a wall I2 defining a cylinder which is closed at one end by a cylinder head I4.
  • the piston 10 is cylindrical and is received in the cylinder I2 for reciprocation therein.
  • the piston I0 is connected to a crankshaft (not shown) through the medium ofa connecting rod 16, as is conventional.
  • the piston would carry piston rings (not shown) for sealing engagement with the walls of the cylinder I2.
  • the chambered piston 10 of the present invention may also be suitable for fuel injection or compression ignition engines, in this instance the chambered piston 10 is illustrated with a spark ignition engine having a spark plug I8 located centrally in the cylinder head 14.
  • the chambered piston 10 is formed of two members, namely, a crown member having a crown or surface 22 exposed to the combustion chamber 11 and a body member 24 which is adapted to be connected to the connecting rod 16 by a wrist pin 26.
  • the crown member 20 may be fastened or secured to the body member 24 by various means so that the crown member reciprocates with the body member. As shown in FIG. 1, the crown member 20 may be secured to the body member 24 by a plurality of bolts 28 which fit in openings 29 in the body member and engage threaded openings 30 in the crown memher.
  • the chambered piston 10 has formed therein a piston chamber 40.
  • the piston chamber is symetrical about the axis of the cylinder I2 and includes an interior portion 42 and a neck or nozzle portion 50.
  • the interior portion 42 includes a wall 44 opposite the nozzle, which is preferably essentially flat and normal to the direction of piston movement.
  • the side walls of the chamber 40 converge from the flat wall 44 toward the nozzle and are defined by an inwardly tapering conical wall 46 which joins an inwardly curved arcuate wall 48.
  • the cross-section area of the interior portion 42 is quite lar e,
  • he interior portion 42 of the piston chamber 40 is connected to the combustion chamber I1 through the nozzle portion 50 which comprises an inner converging portion 52, a minimum area opening or throat 54, and a diverging portion 56 which exists through the crown 22 of the piston 10 into the combustion chamber I l.
  • the size of the combustion chamber 11 and of the piston chamber 40 will vary with the size and compression ratio of the engine, and the volume of the piston chamber 40 must be taken into consideration in order to achieve the desired compression ratio for the engine.
  • the clearance between the cylinder head I4 and the crown 22 of the piston 10 should be held to a minimum.
  • the piston chamber should have as large a cross-sectional area in the interior portion as possible, e.g..
  • the piston chamber should also be sized so that the piston has adequate wall thickness for structural strength.
  • the area of the throat of the nozzle portion should be relatively small, e.g., 3 to 5 percent of the piston area.
  • the ratio of the largest cross-sectional area of the piston chamber, such as that of the flat wall 44, to that of the nozzle or throat is in the range of 5:l to 1.
  • the other dimensions of the piston chamber should be such as to give the engine the desired compression ratio.
  • the spark plug 18 (or the fuel injector) centrally located on the axis of the cylinder so that the nozzle portion 50 which is also centrally located along the piston axis receives the tip of the spark plug 18 (or fuel injector) when the piston I0 is in the position shown in dotted lines in FIG. 1.
  • the gases After leaving the piston chamber, the gases increase the pressure in the combustion chamber, and the gases in the combustion chamber act on the crown 22 of the piston in a conventional manner.
  • the exhaust port Near the bottom on the power stroke, the exhaust port (not shown) is opened, and the piston moves upward on the exhaust stroke to drive the spent gases from the cylinder preparatory to receiving a new charge for the next cycle.
  • the chambered piston of the present invention is also driven by the high pressure gases first acting on the flat wall 44 and being discharged out the nozzle into the combustion chamber.
  • FIG. 2 A second embodiment of chambered piston of the present invention is shown in FIG. 2.
  • the piston 60 is similar to the piston 10 previously described except for the features mentioned below.
  • the piston 60 is mounted for reciprocation in an engine having a cylinder wall 62 and a cylinder head 64.
  • the engine instead of having a centrally located spark plug, the engine has a spark plug 66 offset to one side of the cylinder.
  • the chambered piston 60 has a chamber 68 generally similar to the chamber 40, having an interior portion 70 and a neck or nozzle portion 72 which are generally similar to portions 42 and 50, respectively, of the piston I0.
  • the chambered piston 60 has an offset ignition opening 74 communicating between the interior por tion 70 of the chamber 68 and the combustion chamber adjacent the spark plug 66. As is shown in FIG. 2, the ignition opening 74 is inclined toward chamber 68 and is enlarged somewhat at its outer end 76 to receive the tip of the spark plug 66.
  • the spark plug 66 ignites the gases in the opening 74 which in turn ignites the gases in the interior 70.
  • the operation of the chambered piston 60 is otherwise the same as that of the chambered piston 10 and will not be described.
  • FIGS. 3-5 A third embodiment of the chambered piston 80 of the present invention is illustrated in FIGS. 3-5.
  • the chambered piston 80 is a rotor for a variable volume rotary engine.
  • the rotor rotates on an axis in the direction of the arrow 81 within the confines of a stator wall 82 (shown in dotted lines) and cooperates with another similar piston 84 shown in dotted lines.
  • the wall 82 and the pistons 80 and 84 define a variable volume combustion chamber 83.
  • the rotor or piston 80 comprises two diamentrically opposed wedges 86 which are integral with a central tubular hub 88 located between the wedges.
  • the hub is internally splined for cooperation with an engine drive shaft (not shown).
  • the wedges 86 are provided with sealing slots 124 in the peripheral surfaces thereof for reception of sealing rings (not shown) which are adapted to engage the wall 82 to seal the rotor to the wall. As shown in FIG. 4, the wedges 86 are elongated in the direction of the axis of rotation, and are at least twice the length of the hub 88.
  • a chamber 92 is provided in the interior of each of the wedges 86. Like the previously described chambers 40 and 60, the chamber 92 has a neck or nozzle portion 94 and an interior portion 96. Again, the nozzle portion 94 opens through a surface 98 of the piston 80 into the combustion chamber 83. Preferably, the nozzle portion has a minimum cross-sectional area of 3 to 5 percent of the piston area and the interior portion has a cross-sectional area of about 30 percent of the piston area, the piston area being taken as dimensions a X b (FIGS. 3 and 4).
  • each of the wedges 86 is in two pieces, having a plate 100 which closes one end of the chamber 92.
  • the plate I00 has a flat inner wall or surface 102 that extends normal to the direction of travel of the rotor.
  • the plate I00 is secured to the wedge 86 by fastening means or screws 104 which fit in openings 105 in the plate 100 and engage in threaded openings 106 provided in the wedge 86.
  • the interior portion 96 of the chamber 92 in the form of an elongated slot I07 (FIG. 4) having parallel walls and curve wall segments 112 at its ends.
  • the nozzle portion 94 also is elongated and formed by an intersecting slot 114 having curved end segments II6.
  • the slots I07 and 114 are at an angle to each other so that the nozzle portion 94 has an inner converging section 118, a minimum throat section I20, and a diverging section 122 existing to the combustion chamber.
  • the operation of the piston 80 is somewhat similar to that of the pistons 40 and 60 previously described.
  • air or a fuel-air mixture is drawn into the combustion chamber 83.
  • the compression stroke the air or fuel-air mixture is compressed into chamber 92.
  • the pistons 80 and 84 rotate, and when the slot 134 of the piston 80 is adjacent the spark plug 130, the spark plug is fired.
  • the mixture in the chamber 92 ignites and raise the pressure in the chamber.
  • the high pressure gases in the chamber 92 first act on the surface 102 of the chamber 92 and then are discharged out the nozzle portion 94 to provide a rocket or jet type reaction driving the piston.
  • the discharged gases then raise the pressure in the combustion chamber and act on the surface 98 of the piston 80 to further drive the piston, as is conventional.
  • the exhaust port of the engine is opened, and the pistons 80 and 94 cooperate to drive the gases from the combustion chamber to ready it for the next cycle.
  • a rotary engine or reciprocating engine having a chambered piston of the present invention additional power is produced during the power stroke by the gases acting against the wall of the piston chamber and being discharged out the nozzle. This additional power augments the power produced by the gases discharged to the combustion chamber which act on the outer surface of the piston:
  • the use of the chambered piston of the present invention in an engine improves combustion, reduces octane requirement and improves fuel economy.
  • each piston member includes a hub and a pair of elongated wedge-shaped members disposed on oppo site sides of said hub and extending parallel to the axis of rotation of said hub, said wedge-shaped members being at least twice as long as said hub and being mounted at their inner ends on said hub, each of said wedge-shaped members having a pair of substantially radially extending faces and one of said piston chambers formed therein, said piston chamber being elongated and extending in a direction parallel to the axis of rotation of said hub, each of said wedge-shaped members having an elongated slot intersecting its associated chamber and extending substantially perpendicularly through one radial face of said wedge-shaped member to form said nozzle, the cross-sectional area of said chamber in a plane including said axis of rotation being at least five times larger than the cross-sectional area of said slot in a plane including said axis of rotation, and a radi
  • a rotating piston for a rotary internal combustion engine comprising a hub and a pair of elongated wedgeshaped members disposed on opposite sides of said hub and extending parallel to the axis of rotation of said hub, said wedge-shaped members having a pair of generally radial faces, being mounted on their inner ends to said hub and at least twice the length of said hub, said piston cooperating with a similar second piston and the engine walls to define a pair of variable volume wedgeshaped combustion chambers between the wedge-shaped members, each of said wedge-shaped members having a piston chamber formed therein extending in a direction parallel to the axis of rotation, a elongated slot intersecting said chamber and extending generally perpendicularly through one of said radial faces to form a nozzle exiting onto one of the combustion chambers, the cross-sectional area of said piston chamber in a plane including the axis of rotation being at least five times larger than the cross-sectional area of said slot in a plane including the axis of rotation, and a generally radial passage intersecting said

Landscapes

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

Abstract

A piston for an internal combustion engine is provided with an interior chamber of relatively large cross-sectional area, e.g., about 30 percent of the piston area, and a nozzle of relatively smaller throat area, e.g., about 3 to 5 percent of the piston area, opening into the combustion chamber of the engine. Upon ignition, gases in the chamber in the piston act on a wall of said chamber opposite the nozzle and then expand through the nozzle into the combustion chamber to act also on the crown of the piston.

Description

United States Patent n 1 Studenroth 1 1 Dec. 2, 1975 1 1 CHAMBERED PISTON FOR AN INTERNAL COMBUSTION ENGINE I761 Inventor: Karl E. Studenroth, 1609 Euclid Ave Chicago Heights, 111 60411 221 Filed: Apr. 22. mm
2n App1.N0.:462,642
[52] US. Cl. H 123/193 P; 123/32 B;123/191S [51] Int. Cl. F02F 3/00; F02F 3/26 [581 Field of Search H 123/32 C, 32 D, 32 K, 32 ST, 123/32 SP, DIG. 4 75 B, 191 S, 191 SP 193 CP.193 P, 8.47, 32 B I561 References Cited FOREIGN PATENTS OR APPLICATIONS 639,889 7/1928 France 123/32 8 852,936 10/1970 Canada w A 4 w 60/3962 2.023.279 11/1971 Germany .7 123/847 1.316.039 12/1962 France 123/847 Primary Examiner-Charles J. Myhre Assirrunl liraminer-william C. Anderson Almrney Agent, or FirmGary. Jeuttner, Pigott 8:
Cullinan l 57] ABSTRACT A piston for an internal combustion engine is provided with an interior chamber of relatively large crosssectional area clg about 30 percent of the piston area, and a nozzle of relatively smaller throat area, e.g., about 3 to 5 percent of the piston area, opening into the combustion chamber of the engine. Upon ignition gases in the chamber in the piston act on a wall of said chamber opposite the nozzle and then expand through the nozzle into the combustion chamber to act also on the crown of the piston.
9 Claims, 5 Drawing Figures U.S. Patent Dec. 2, 1975 3,927,032
jaw;
CHAMBERED PISTON FOR AN INTERNAL COMBUSTION ENGINE BACKGROUND OF THE INVENTION Heretofore, internal combustion engines have been provided with chambers of various designs forming parts of the combustion chambers of the engines. Such chambers were located either in the cylinder heads or in the pistons. Typically, the chambers in the pistons were generally saucer-like or cup shaped recesses, having the largest cross-sectional area thereof open directly to the combustion chamber. Such chambers were used mainly in the pistons of diesel engines to concentrate the air prior to receiving the injected fuel. Such chambered pistons were infrequently used in spark ignition engines. Because of the shape of the chamber, the prior art chambered piston did not appreciably produce more power than a conventional flat top" piston.
SUMMARY OF THE INVENTION The chamber in the piston of the present invention has a unique shape, somewhat like a bottle, with an interior of relatively large cross-sectional area and a neck or nozzle portion with an opening or throat of relatively small cross-sectional area. The piston chamber preferably has a flat wall at the end opposite the nozzle opening, the flat wall being normal to the direction of travel of the piston. From the flat wall, the piston chamber tapers and/or curves convergingly toward the smaller nozzle opening. The nozzle portion, itself, first converges toward a minimum diameter throat and then diverges to open onto the outer surface or crown of the piston. To facilitate formation of the chamber inside the piston, the piston may be made of two members which are secured together.
In operation, the air, in case of a fuel-injection engine, and/or fuel-air mixture, in case of a spark ignition engine, is concentrated in the chamber of the piston during the comprssion stroke. Upon ignition, either by compression or spark, the expanding gases first act on the flat wall of the piston chamber opposite the nozzle opening and then expand out the nozzle to act on the outer surface or crown of the piston in a conventional manner to drive the piston so that the expanding gases do additional work and produce additional power.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. I is a cross-sectional view of one embodiment of a chambered piston of the present invention for a reciprocating engine;
FIG. 2 is a cross-sectional view of a second embodiment of a chambered piston of the present invention for a reciprocating enging;
FIG. 3 is a cross-sectional view of a third embodiment of a chambered piston of the present invention for a rotary engine;
FIG. 4 is an elevational view taken in the direction of the arrows 44 in FIG. 3 with a portion broken away; and
FIG. 5 is a plan view taken in the direction of the arrows 5-5 in FIG. 4.
DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. I illustrates a chambered piston according to the present invention which is suitable for use in an internal combustion engine having engine walls which in conjunction with the chambered piston 10 form a combustion chamber II. In this instance the engine is of the reciprocating type and has a wall I2 defining a cylinder which is closed at one end by a cylinder head I4. The piston 10 is cylindrical and is received in the cylinder I2 for reciprocation therein. The piston I0 is connected to a crankshaft (not shown) through the medium ofa connecting rod 16, as is conventional. Also as is conventional, the piston would carry piston rings (not shown) for sealing engagement with the walls of the cylinder I2. While the chambered piston 10 of the present invention may also be suitable for fuel injection or compression ignition engines, in this instance the chambered piston 10 is illustrated with a spark ignition engine having a spark plug I8 located centrally in the cylinder head 14.
While the chambered piston of the present invention could have been formed in one piece, in this instance, to facilitate manufacturing, the chambered piston 10 is formed of two members, namely, a crown member having a crown or surface 22 exposed to the combustion chamber 11 and a body member 24 which is adapted to be connected to the connecting rod 16 by a wrist pin 26. The crown member 20 may be fastened or secured to the body member 24 by various means so that the crown member reciprocates with the body member. As shown in FIG. 1, the crown member 20 may be secured to the body member 24 by a plurality of bolts 28 which fit in openings 29 in the body member and engage threaded openings 30 in the crown memher.
The chambered piston 10 has formed therein a piston chamber 40. In this instance, the piston chamber is symetrical about the axis of the cylinder I2 and includes an interior portion 42 and a neck or nozzle portion 50. The interior portion 42 includes a wall 44 opposite the nozzle, which is preferably essentially flat and normal to the direction of piston movement. The side walls of the chamber 40 converge from the flat wall 44 toward the nozzle and are defined by an inwardly tapering conical wall 46 which joins an inwardly curved arcuate wall 48. As is apparent from FIG. I, the cross-section area of the interior portion 42 is quite lar e,
"l he interior portion 42 of the piston chamber 40 is connected to the combustion chamber I1 through the nozzle portion 50 which comprises an inner converging portion 52, a minimum area opening or throat 54, and a diverging portion 56 which exists through the crown 22 of the piston 10 into the combustion chamber I l.
The size of the combustion chamber 11 and of the piston chamber 40 will vary with the size and compression ratio of the engine, and the volume of the piston chamber 40 must be taken into consideration in order to achieve the desired compression ratio for the engine. In order to concentrate as much air and/or fueI-airmixture in the piston chamber 40, to permit the largest size piston chamber for a given compression ratio, and to have the spark plug 18 extend into the piston chamber as far as possible, the clearance between the cylinder head I4 and the crown 22 of the piston 10 should be held to a minimum. Preferably, the piston chamber should have as large a cross-sectional area in the interior portion as possible, e.g.. 30 percent of the piston area, based on a piston area of 11 (Diameter of Piston) /4 and neglecting the area of the nozzle. The piston chamber should also be sized so that the piston has adequate wall thickness for structural strength. The area of the throat of the nozzle portion should be relatively small, e.g., 3 to 5 percent of the piston area. Preferably, the ratio of the largest cross-sectional area of the piston chamber, such as that of the flat wall 44, to that of the nozzle or throat is in the range of 5:l to 1. The other dimensions of the piston chamber should be such as to give the engine the desired compression ratio.
With the chambered piston 10 of the present invention, it is preferable to have the spark plug 18 (or the fuel injector) centrally located on the axis of the cylinder so that the nozzle portion 50 which is also centrally located along the piston axis receives the tip of the spark plug 18 (or fuel injector) when the piston I0 is in the position shown in dotted lines in FIG. 1.
In operation in a four cycle engine, as the chambered piston 10 moves downward on the intake stroke, a fresh charge or air or fuel-air mixture is drawn into the cylinder through an intake port (not shown). On the compression stroke, the piston moves upward to substantially the cylinder head 14 so that almost all the air or fuel-air mixture is forced into the piston chamber 40. Near the end of the compression stroke, the spark plug 18 is fired (or the fuel injected) to ignite the fuel-air mixture in the piston chamber 40. The burning gases expand and raise the pressure in the piston chamber 40. The high pressure gases act against the flat end wall 44 of the piston chamber and are discharged through the nozzle 50 with a rocket or jet type action which causes an opposite reaction tending to drive the piston downward on its power stroke. After leaving the piston chamber, the gases increase the pressure in the combustion chamber, and the gases in the combustion chamber act on the crown 22 of the piston in a conventional manner. Near the bottom on the power stroke, the exhaust port (not shown) is opened, and the piston moves upward on the exhaust stroke to drive the spent gases from the cylinder preparatory to receiving a new charge for the next cycle.
Unlike a conventional piston which is driven solely by high pressure gases in the combustion chamber, the chambered piston of the present invention is also driven by the high pressure gases first acting on the flat wall 44 and being discharged out the nozzle into the combustion chamber.
A second embodiment of chambered piston of the present invention is shown in FIG. 2. In this embodi ment, the piston 60 is similar to the piston 10 previously described except for the features mentioned below. As illustrated in FIG. 2, the piston 60 is mounted for reciprocation in an engine having a cylinder wall 62 and a cylinder head 64. In this instance, instead of having a centrally located spark plug, the engine has a spark plug 66 offset to one side of the cylinder.
The chambered piston 60 has a chamber 68 generally similar to the chamber 40, having an interior portion 70 and a neck or nozzle portion 72 which are generally similar to portions 42 and 50, respectively, of the piston I0. To accommodate the offset location of the spark plug 66, the chambered piston 60 has an offset ignition opening 74 communicating between the interior por tion 70 of the chamber 68 and the combustion chamber adjacent the spark plug 66. As is shown in FIG. 2, the ignition opening 74 is inclined toward chamber 68 and is enlarged somewhat at its outer end 76 to receive the tip of the spark plug 66. Upon firing, the spark plug 66 ignites the gases in the opening 74 which in turn ignites the gases in the interior 70. The operation of the chambered piston 60 is otherwise the same as that of the chambered piston 10 and will not be described.
A third embodiment of the chambered piston 80 of the present invention is illustrated in FIGS. 3-5. Unlike the chambered pistons 40 and 60, the chambered piston 80 is a rotor for a variable volume rotary engine. The rotor rotates on an axis in the direction of the arrow 81 within the confines of a stator wall 82 (shown in dotted lines) and cooperates with another similar piston 84 shown in dotted lines. The wall 82 and the pistons 80 and 84 define a variable volume combustion chamber 83. As is shown in FIG. 3, the rotor or piston 80 comprises two diamentrically opposed wedges 86 which are integral with a central tubular hub 88 located between the wedges. The hub is internally splined for cooperation with an engine drive shaft (not shown). The wedges 86 are provided with sealing slots 124 in the peripheral surfaces thereof for reception of sealing rings (not shown) which are adapted to engage the wall 82 to seal the rotor to the wall. As shown in FIG. 4, the wedges 86 are elongated in the direction of the axis of rotation, and are at least twice the length of the hub 88.
A chamber 92 is provided in the interior of each of the wedges 86. Like the previously described chambers 40 and 60, the chamber 92 has a neck or nozzle portion 94 and an interior portion 96. Again, the nozzle portion 94 opens through a surface 98 of the piston 80 into the combustion chamber 83. Preferably, the nozzle portion has a minimum cross-sectional area of 3 to 5 percent of the piston area and the interior portion has a cross-sectional area of about 30 percent of the piston area, the piston area being taken as dimensions a X b (FIGS. 3 and 4).
To facilitate formation of the piston chamber 92, each of the wedges 86 is in two pieces, having a plate 100 which closes one end of the chamber 92. As shown in FIGS. 3 and 4, the plate I00 has a flat inner wall or surface 102 that extends normal to the direction of travel of the rotor. The plate I00 is secured to the wedge 86 by fastening means or screws 104 which fit in openings 105 in the plate 100 and engage in threaded openings 106 provided in the wedge 86.
In this instance the interior portion 96 of the chamber 92 in the form of an elongated slot I07 (FIG. 4) having parallel walls and curve wall segments 112 at its ends. The nozzle portion 94 also is elongated and formed by an intersecting slot 114 having curved end segments II6. The slots I07 and 114 are at an angle to each other so that the nozzle portion 94 has an inner converging section 118, a minimum throat section I20, and a diverging section 122 existing to the combustion chamber.
In order to ignite the charge in the chamber 92 a spark plug, indicated in dotted lines by the reference numeral 130, is provided. The interior of the chamber 92 communicates with the spark plug I30 through a generally radial passage I32 in the wedge 86. The outer end of the passage I32 intersects a groove or slot 134 located on the arcuate outer surface of the wedge 86. As is shown in FIGS. 3 and 5, the slot I34 is of suffi' cient length so that the plug I30 may ignite the charge in the chamber 92 even though the plug is not exactly over the end of the radial opening 132.
The operation of the piston 80 is somewhat similar to that of the pistons 40 and 60 previously described. On the intake stroke of the engine air or a fuel-air mixture is drawn into the combustion chamber 83. On the compression stroke, the air or fuel-air mixture is compressed into chamber 92. The pistons 80 and 84 rotate, and when the slot 134 of the piston 80 is adjacent the spark plug 130, the spark plug is fired. The mixture in the chamber 92 ignites and raise the pressure in the chamber. The high pressure gases in the chamber 92 first act on the surface 102 of the chamber 92 and then are discharged out the nozzle portion 94 to provide a rocket or jet type reaction driving the piston. The discharged gases then raise the pressure in the combustion chamber and act on the surface 98 of the piston 80 to further drive the piston, as is conventional. After a certain time the exhaust port of the engine is opened, and the pistons 80 and 94 cooperate to drive the gases from the combustion chamber to ready it for the next cycle.
ln a rotary engine or reciprocating engine having a chambered piston of the present invention additional power is produced during the power stroke by the gases acting against the wall of the piston chamber and being discharged out the nozzle. This additional power augments the power produced by the gases discharged to the combustion chamber which act on the outer surface of the piston: The use of the chambered piston of the present invention in an engine improves combustion, reduces octane requirement and improves fuel economy.
While only several embodiments of the chambered piston of the present invention has been described it shall be understood that variations, modifications and equivalent structures shall come within the scope of the appended claims.
I claim:
1. In a piston for a four cycle spark ignition internal combustion engine having a spark plug, the piston cooperating with the engine walls to define a combustion chamber of variable volume, the improvement comprising a piston member with a fixed piston area and having a piston chamber formed within said piston member, said piston chamber having a nozzle of an area of generally five or less percent of the piston area exiting through an outer surface of the piston member into said combustion chamber, said piston chamber having an interior of a cross-sectional area at least five times larger than the cross-sectional area of said nozzle, said piston chamber containing substantially all of a combustible mixture introduced into the combustion chamber of the engine and being in communication with said spark plug near the completion of the compression cycle, whereby upon ignition of the combustible mixture in said piston chamber by said spark plug, the gases generated by combustion are discharged from said piston chamber out said nozzle to drive said piston member by jet reaction and after being discharged into said combustion chamber act on said outer surface of said piston to further drive said piston member.
2. The piston member of claim 1, wherein said nozzle of said piston chamber and said spark plug at the end of the compression cycle are aligned with one another, whereby said nozzle of said piston chamber receives said spark plug at the end of the compression cycle.
3. The piston member of claim 1, wherein said nozzle and said spark plug are misaligned, said piston member having a second opening therein aligned with said spark 6 plug to communicate the interior of said piston chamber with said spark plug at the end of the compression cycle.
4. The piston member of claim 1, wherein said piston chamber has a flat surface opposite said nozzle and converges from the margins of said flat surface toward said nozzle, said nozzle first converging and then diverging to exit into the combustion chamber.
5. The piston member of claim 1, wherein said piston member is in the form of a rotor for a rotary engine and includes an elongated wedge member in which said piston chamber is formed.
6. The piston member of claim 1, wherein a pair of said piston members comprises a rotor for a rotary engine, each piston member includes a hub and a pair of elongated wedge-shaped members disposed on oppo site sides of said hub and extending parallel to the axis of rotation of said hub, said wedge-shaped members being at least twice as long as said hub and being mounted at their inner ends on said hub, each of said wedge-shaped members having a pair of substantially radially extending faces and one of said piston chambers formed therein, said piston chamber being elongated and extending in a direction parallel to the axis of rotation of said hub, each of said wedge-shaped members having an elongated slot intersecting its associated chamber and extending substantially perpendicularly through one radial face of said wedge-shaped member to form said nozzle, the cross-sectional area of said chamber in a plane including said axis of rotation being at least five times larger than the cross-sectional area of said slot in a plane including said axis of rotation, and a radial passage extending from said chamber to the outer periphery of said wedge-shaped member for establishing communication between said piston chamber and said spark plug in the vicinity of the end of the compression cycle for the respective wedge-shaped member.
7. A process of operating a four cycle spark ignition internal combustion engine having a spark plug and a piston cooperating with other portions of the engine to define a variable volume combustion chamber, said piston having a piston chamber therein, said piston chamber having an interior portion and a nozzle portion exiting through an outer surface of the piston into the combustion chamber, the cross-sectional area of said interior portion being at least five times larger than the cross-sectional area of the nozzle portion, and the cross-sectional area of said nozzle portion being five or less percent of the piston area, comprising the steps of:
a. charging said combustion chamber with a combustible mixture,
b. compressing substantially all of said combustible mixture into said piston chamber,
c. igniting the combustible mixture in said piston chamber with said spark plug to increase the pressure in the piston chamber above that in the combustion chamber,
d. discharging the high pressure gases formed by combustion of said combustible mixture from said piston chamber through said nozzle portion into said combustion chamber to produce a jet type reaction driving the piston,
e. raising the pressure in the combustion chamber with the discharged gases from the piston chamber, the gases in the combustion chamber acting on the outer surface of the piston to further drive the piston, and
7 f. exhausting the gases from the piston chamber and combustion chamber,
whereby said piston is driven both by jet reaction of the gases discharged through the nozzle and by the discharged gases increasing the pressure in the combustion chamber and acting on the outer piston surface.
8. A rotating piston for a rotary internal combustion engine comprising a hub and a pair of elongated wedgeshaped members disposed on opposite sides of said hub and extending parallel to the axis of rotation of said hub, said wedge-shaped members having a pair of generally radial faces, being mounted on their inner ends to said hub and at least twice the length of said hub, said piston cooperating with a similar second piston and the engine walls to define a pair of variable volume wedgeshaped combustion chambers between the wedge-shaped members, each of said wedge-shaped members having a piston chamber formed therein extending in a direction parallel to the axis of rotation, a elongated slot intersecting said chamber and extending generally perpendicularly through one of said radial faces to form a nozzle exiting onto one of the combustion chambers, the cross-sectional area of said piston chamber in a plane including the axis of rotation being at least five times larger than the cross-sectional area of said slot in a plane including the axis of rotation, and a generally radial passage intersecting said piston chamber and extending to the outer periphery of said wedgeshaped member for communicating said piston chamber with a spark plug or fuel injector of the engine, whereby a combustible mixture may be burned in said piston chamber to raise the pressure in the piston chamber above that in the combustion chamber, the gases generated by combustion being discharged out the nozzle to the associated combustion chamber to first drive the piston with jet type reaction and then acting on the outer radial face of said piston to further drive the piston.
9. A process of operating a rotary internal combustion engine having a pair of wedge-shaped pistons cooperating with each other and other portions of the engine to define a wedge-shaped variable volume combustion chamber, one of said pistons having a chamber therein, said piston chamber having an interior portion and a nozzle portion exiting through an outer surface of the piston into the combustion chamber, the cross-sectional area of said interior portion being at least five time larger than the cross-sectional area of the nozzle portion, comprising the steps of:
a. charging said wedge-shaped combustion chamber with air or fuel-air mixture,
b. compressing substantially all of said air or fuel-air mixture between said wedge-shaped pistons and into said piston chamber,
c. igniting the fuel-air mixture to increase the pressure in the piston chamber above that of the combustion chamber,
(1. discharging the high pressure gases formed through said nozzle portion into said wedge-shaped combustion chamber to produce a jet type reaction driving said one piston away from the other piston,
e. raising the pressure in the combustion chamber with the discharged gases from the piston chamber, the gases in the combustion chamber acting on the outer surface of said one piston to further drive said one piston away from the other piston, and
f. moving the other piston toward said one piston to exhaust the gases from the combustion chamber, whereby said one piston is driven both by the jet reaction of the gases discharged from the nozzle and by the discharged gases increasing the pressure in the combustion chamber and acting on the outer surface of said one piston.

Claims (9)

1. In a piston for a four cycle spark ignition internal combustion engine having a spark plug, the piston cooperating with the engine walls to define a combustion chamber of variable volume, the improvement comprising a piston member with a fixed piston area and having a piston chamber formed within said piston member, said piston chamber having a nozzle of an area of generally five or less percent of the piston area exiting through an outer surface of the piston member into said combustion chamber, said piston chamber having an interior of a crosssectional area at least five times larger than the crosssectional area of said nozzle, said piston chamber containing substantially all of a combustible mixture introduced into the combustion chamber of the engine and being in communication with said spark plug near the completion of the compression cycle, whereby upon ignition of the combustible mixture in said piston chamber by said spark plug, the gases generated by combustion are discharged from said piston chamber out said nozzle to drive said piston member by jet reaction and after being discharged into said combustion chamber act on said outer surface of said piston to further drive said piston member.
2. The piston member of claim 1, wherein said nozzle of said piston chamber and said spark plug at the end of the compression cycle are aligned with one another, whereby said nozzle of said piston chamber receives said spark plug at the end of the compression cycle.
3. The piston member of claim 1, wherein said nozzle and said spark plug are misaligned, said piston member having a second opening therein aligned with said spark plug to communicate the interior of said piston chamber with said spark plug at the end of the compression cycle.
4. The piston member of claim 1, wherein said piston chamber has a flat surface opposite said nozzle and converges from the margins of said flat surface toward said nozzle, said nozzle first converging and then diverging to exit into the combustion chamber.
5. The piston member of claim 1, wherein said piston member is in the form of a rotor for a rotary engine and includes an elongated wedge member in which said piston chamber is formed.
6. The piston member of claim 1, wherein a pair of said piston members comprises a rotor for a rotary engine, each piston member includes a hub and a pair of elongated wedge-shaped members disposed on opposite sides of said hub and extending parallel to the axis of rotation of said hub, said wedge-shaped members being at least twice as long as said hub and being mounted at their inner ends on said hub, each of said wedge-shaped members having a pair of substantially radially extending faces and one of said piston chambers formed therein, said piston chamber being elongated and extending in a direction parallel to the axis of rotation of said hub, each of said wedge-shaped members having an elongated slot intersecting its associated chamber and extending substantially perpendicularly through one radial face of said wedge-shaped member to form said nozzle, the cross-sectional area of said chamber in a plane including said axis of rotation being at least five times larger than the cross-sectional area of said slot in a plane including said axis of rotation, and a radial passage extending from said chamber to the outer periphery of said wedge-shaped member for establishing communication between said piston chamber and said spark plug in the vicinity of the end of the compression cycle for the respective wedge-shaped member.
7. A process of operating a four cyclE spark ignition internal combustion engine having a spark plug and a piston cooperating with other portions of the engine to define a variable volume combustion chamber, said piston having a piston chamber therein, said piston chamber having an interior portion and a nozzle portion exiting through an outer surface of the piston into the combustion chamber, the cross-sectional area of said interior portion being at least five times larger than the cross-sectional area of the nozzle portion, and the cross-sectional area of said nozzle portion being five or less percent of the piston area, comprising the steps of: a. charging said combustion chamber with a combustible mixture, b. compressing substantially all of said combustible mixture into said piston chamber, c. igniting the combustible mixture in said piston chamber with said spark plug to increase the pressure in the piston chamber above that in the combustion chamber, d. discharging the high pressure gases formed by combustion of said combustible mixture from said piston chamber through said nozzle portion into said combustion chamber to produce a jet type reaction driving the piston, e. raising the pressure in the combustion chamber with the discharged gases from the piston chamber, the gases in the combustion chamber acting on the outer surface of the piston to further drive the piston, and f. exhausting the gases from the piston chamber and combustion chamber, whereby said piston is driven both by jet reaction of the gases discharged through the nozzle and by the discharged gases increasing the pressure in the combustion chamber and acting on the outer piston surface.
8. A rotating piston for a rotary internal combustion engine comprising a hub and a pair of elongated wedge-shaped members disposed on opposite sides of said hub and extending parallel to the axis of rotation of said hub, said wedge-shaped members having a pair of generally radial faces, being mounted on their inner ends to said hub and at least twice the length of said hub, said piston cooperating with a similar second piston and the engine walls to define a pair of variable volume wedgeshaped combustion chambers between the wedge-shaped members, each of said wedge-shaped members having a piston chamber formed therein extending in a direction parallel to the axis of rotation, a elongated slot intersecting said chamber and extending generally perpendicularly through one of said radial faces to form a nozzle exiting onto one of the combustion chambers, the cross-sectional area of said piston chamber in a plane including the axis of rotation being at least five times larger than the cross-sectional area of said slot in a plane including the axis of rotation, and a generally radial passage intersecting said piston chamber and extending to the outer periphery of said wedge-shaped member for communicating said piston chamber with a spark plug or fuel injector of the engine, whereby a combustible mixture may be burned in said piston chamber to raise the pressure in the piston chamber above that in the combustion chamber, the gases generated by combustion being discharged out the nozzle to the associated combustion chamber to first drive the piston with jet type reaction and then acting on the outer radial face of said piston to further drive the piston.
9. A process of operating a rotary internal combustion engine having a pair of wedge-shaped pistons cooperating with each other and other portions of the engine to define a wedge-shaped variable volume combustion chamber, one of said pistons having a chamber therein, said piston chamber having an interior portion and a nozzle portion exiting through an outer surface of the piston into the combustion chamber, the cross-sectional area of said interior portion being at least five time larger than the cross-sectional area of the nozzle portion, comprising the steps of: a. charging said wedge-shaped combustion chamber with air or fuel-air mixture, b. compressing subStantially all of said air or fuel-air mixture between said wedge-shaped pistons and into said piston chamber, c. igniting the fuel-air mixture to increase the pressure in the piston chamber above that of the combustion chamber, d. discharging the high pressure gases formed through said nozzle portion into said wedge-shaped combustion chamber to produce a jet type reaction driving said one piston away from the other piston, e. raising the pressure in the combustion chamber with the discharged gases from the piston chamber, the gases in the combustion chamber acting on the outer surface of said one piston to further drive said one piston away from the other piston, and f. moving the other piston toward said one piston to exhaust the gases from the combustion chamber, whereby said one piston is driven both by the jet reaction of the gases discharged from the nozzle and by the discharged gases increasing the pressure in the combustion chamber and acting on the outer surface of said one piston.
US462642A 1974-04-22 1974-04-22 Chambered piston for an internal combustion engine Expired - Lifetime US3923032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US462642A US3923032A (en) 1974-04-22 1974-04-22 Chambered piston for an internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US462642A US3923032A (en) 1974-04-22 1974-04-22 Chambered piston for an internal combustion engine

Publications (1)

Publication Number Publication Date
US3923032A true US3923032A (en) 1975-12-02

Family

ID=23837207

Family Applications (1)

Application Number Title Priority Date Filing Date
US462642A Expired - Lifetime US3923032A (en) 1974-04-22 1974-04-22 Chambered piston for an internal combustion engine

Country Status (1)

Country Link
US (1) US3923032A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4127094A (en) * 1973-02-12 1978-11-28 Barry Leonard D Engine
WO1980000862A1 (en) * 1978-10-25 1980-05-01 R Blaser Energy conversion cycle for internal combustion engine and apparatus for carrying out the cycle
US4236490A (en) * 1977-01-14 1980-12-02 A. C. Engines, Inc. Internal combustion engine
US4515114A (en) * 1983-08-15 1985-05-07 Nguyen Dang Two part piston assembly
US5042441A (en) * 1989-10-03 1991-08-27 Paul Marius A Low emission combustion system for internal combustion engines
US5052356A (en) * 1976-10-19 1991-10-01 Sonex Research, Inc. Method for control of pressure in internal combustion engines
EP0454031A1 (en) * 1990-04-23 1991-10-30 Isuzu Motors Limited Construction of a combustion chamber for an internal combustion engine
US5117788A (en) * 1976-10-19 1992-06-02 Sonex Research, Inc. Apparatus for control of pressure in internal combustion engines
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
DE4406127A1 (en) * 1994-02-25 1995-01-26 Daimler Benz Ag Piston for an internal combustion engine
WO2006058525A1 (en) * 2004-11-30 2006-06-08 Mahle International Gmbh Two-part piston for a combustion engine
US20090194065A1 (en) * 2006-05-09 2009-08-06 Okamura Yugen Kaisha Rotary Piston Type Internal Combustion Engine
US20100050981A1 (en) * 2008-09-04 2010-03-04 Ivas Richard T Rotary internal combustion engine
US20140261289A1 (en) * 2013-03-15 2014-09-18 Randy Koch Rotary Internal Combustion Engine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR639889A (en) * 1927-04-12 1928-07-02 Ceskomoravska Kolben Combustion chamber piston for internal combustion engines
FR1316039A (en) * 1962-01-30 1963-01-25 Rotary engine, especially internal combustion
CA852936A (en) * 1970-10-06 W. Sherwood John Rotary gas turbine engine
DE2023279A1 (en) * 1970-05-13 1971-11-25 Wolff, Bruno, 7031 Aidlingen Rotary piston engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA852936A (en) * 1970-10-06 W. Sherwood John Rotary gas turbine engine
FR639889A (en) * 1927-04-12 1928-07-02 Ceskomoravska Kolben Combustion chamber piston for internal combustion engines
FR1316039A (en) * 1962-01-30 1963-01-25 Rotary engine, especially internal combustion
DE2023279A1 (en) * 1970-05-13 1971-11-25 Wolff, Bruno, 7031 Aidlingen Rotary piston engine

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4127094A (en) * 1973-02-12 1978-11-28 Barry Leonard D Engine
US5052356A (en) * 1976-10-19 1991-10-01 Sonex Research, Inc. Method for control of pressure in internal combustion engines
US5117788A (en) * 1976-10-19 1992-06-02 Sonex Research, Inc. Apparatus for control of pressure in internal combustion engines
US4236490A (en) * 1977-01-14 1980-12-02 A. C. Engines, Inc. Internal combustion engine
WO1980000862A1 (en) * 1978-10-25 1980-05-01 R Blaser Energy conversion cycle for internal combustion engine and apparatus for carrying out the cycle
US4465033A (en) * 1978-10-25 1984-08-14 Blaser Richard Florencio Energy conversion cycle for internal combustion engine and apparatus for carrying out the cycle
US4515114A (en) * 1983-08-15 1985-05-07 Nguyen Dang Two part piston assembly
US5042441A (en) * 1989-10-03 1991-08-27 Paul Marius A Low emission combustion system for internal combustion engines
EP0454031A1 (en) * 1990-04-23 1991-10-30 Isuzu Motors Limited Construction of a combustion chamber for an internal combustion engine
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
DE4406127A1 (en) * 1994-02-25 1995-01-26 Daimler Benz Ag Piston for an internal combustion engine
WO2006058525A1 (en) * 2004-11-30 2006-06-08 Mahle International Gmbh Two-part piston for a combustion engine
US20080121102A1 (en) * 2004-11-30 2008-05-29 Rainer Scharp Two-Part Piston For a Combustion Engine
US20090194065A1 (en) * 2006-05-09 2009-08-06 Okamura Yugen Kaisha Rotary Piston Type Internal Combustion Engine
US7793635B2 (en) * 2006-05-09 2010-09-14 Okamura Yugen Kaisha Rotary piston type internal combustion engine
US20100050981A1 (en) * 2008-09-04 2010-03-04 Ivas Richard T Rotary internal combustion engine
US20140261289A1 (en) * 2013-03-15 2014-09-18 Randy Koch Rotary Internal Combustion Engine
US9291095B2 (en) * 2013-03-15 2016-03-22 Randy Koch Rotary internal combustion engine
US9828907B2 (en) 2013-03-15 2017-11-28 Randy Koch Rotary internal combustion engine

Similar Documents

Publication Publication Date Title
US3923032A (en) Chambered piston for an internal combustion engine
US4090479A (en) I.C. engine having improved air or air-fuel induction system
JP3016485B2 (en) Reciprocating 2-cycle internal combustion engine without crank
US4038948A (en) Rotary internal combustion engine
US4086878A (en) Combustion process for externally controlled reciprocating piston internal combustion engine operating with hydrogen injection
US4149498A (en) Internal combustion engine
US5275134A (en) Two stroke internal combustion engine having an intake piston adjacent each power piston
US4362132A (en) Two-cycle engine
US5372107A (en) Rotary engine
US2269948A (en) Internal combustion engine
US2688320A (en) Piston and cylinder construction for internal-combustion engines
US4686941A (en) Turbulence generator for two-stroke spark-assisted diesel engines
US4164915A (en) Conversion of gasoline to diesel engine
US4516536A (en) Three cycle internal combustion engine
JPS592766B2 (en) Structural improvements in two-stroke opposed piston engines operated by layered charge
US5908012A (en) Combustion control device for an engine
US4457273A (en) Conical piston and cylinder head in internal combustion engine
US4913111A (en) Turbulence generator for two-stroker spark-assisted diesel engines
US4175501A (en) Internal combustion engine with an auxiliary combustion chamber
US2033155A (en) Process of mixing and burning fuel
KR20010041930A (en) High power density, diesel engine
US2685869A (en) Internal-combustion engine
US3842812A (en) Four-cycle internal combustion engine without a camshaft
GB2108581A (en) Fuel injection stratified charge internal combustion engine
US4434752A (en) Internal combustion engine