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WO2001088341A1 - Moteur a combustion interne possedant un rotor articule - Google Patents

Moteur a combustion interne possedant un rotor articule Download PDF

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Publication number
WO2001088341A1
WO2001088341A1 PCT/AU2001/000544 AU0100544W WO0188341A1 WO 2001088341 A1 WO2001088341 A1 WO 2001088341A1 AU 0100544 W AU0100544 W AU 0100544W WO 0188341 A1 WO0188341 A1 WO 0188341A1
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
combustion engine
internal combustion
engine described
segments
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.)
Ceased
Application number
PCT/AU2001/000544
Other languages
English (en)
Inventor
Peter Szorenyi
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
Priority claimed from AU24071/00A external-priority patent/AU2407100A/en
Priority claimed from AU34071/00A external-priority patent/AU726791B1/en
Application filed by Individual filed Critical Individual
Priority to JP2001584712A priority Critical patent/JP3676303B2/ja
Priority to EP01929123A priority patent/EP1285149A4/fr
Priority to US10/149,913 priority patent/US6718938B2/en
Priority to CA002425487A priority patent/CA2425487C/fr
Priority to AU2001256006A priority patent/AU2001256006A1/en
Priority to KR1020027015139A priority patent/KR100854573B1/ko
Publication of WO2001088341A1 publication Critical patent/WO2001088341A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
    • F01C1/44—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/22—Rotary-piston machines or engines of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005—Wankel engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four

Definitions

  • This invention is in the field of rotary internal combustion engines utilising a flexible, hinged rotor assembly.
  • the rotor assembly is confined by a coaxial housing whose internal profile is derived from an exact mathematical relationship.
  • the engine utilises a synchronised power transfer system whereby the rotor directly bears on the crankshaft.
  • Documents containing related art include US Patent Nos. 3,139,722; 3,369,529; 3,872,852; 3,918,415; 4,181,481; GB Patent Nos. 1,289,479; 1,521,960; DE 2,321,763; CA 2,192,714 and EP0571637.
  • the cited patents relate to internal combustion engine designs based on rigid (eg. Wankel) and flexible rotor assemblies contained in a coaxial housing.
  • This invention discloses the exact mathematical definition of the housing profile, required to accommodate a four-segment flexible, or hinged, rotor assembly at any rotational angle.
  • the novel mathematical relationship is applicable to the design and manufacture of said rotor assembly housings.
  • the specification for a synchronised, direct power transfer system is also described. Such a power transfer system harmonises the rotation of the hinged rotor assembly with the rotation of the crankshaft.
  • This invention concerns the design of an Otto cycle (four-stroke) rotary internal combustion engine employing the concept of a deformable four-segment hinged rotor assembly.
  • the underlying principle consists of accommodating the four-segment equilateral hinged rotor in a coaxial confinement housing such that the four vertices of this rotating equilateral parallelogram coincide with the confining curve (rotor housing internal contour) at any angle of rotation.
  • the basic concept is illustrated in Figure 1.
  • the four-segment rotor assembly 1 deforms and continuously adapts to the rotor housing 2 contour.
  • the hinged equilateral parallelogram rotates, it changes from a square to a rhombus and then back to a square, and so on.
  • the volume enclosed between the rotor housing flat-plate side covers 3, rotor housing 2 and each individual rotor segment face 4, cyclically varies from a minimum to a maximum.
  • the successive expansion and contraction of the enclosed volumes enables the device to perform the Otto cycle internal combustion engine functions of intake, compression, expansion and exhaust.
  • the rotor housing curve or internal profile is defined by a novel mathematical relationship and is described in detail in the text.
  • the curve will be known as Szorenyi's curve, named after the inventor who is believed to be the first to recognise this mathematical relationship.
  • the characteristics of the rotor housing curve depend on the ratio n of rotor housing minor to major internal diameters (adopting ellipse terminology). In the case of a one-to-one correspondence of these diameters, the curve is a circle with no practical motor application in that there is no cyclic volume change generated by rotation of the rotor. As the ratio of minor to major diameters n decreases, the curve assumes more of an elliptical shape and, for the three-dimensional case, the ratio of maximum enclosed volume to minimum enclosed volume increases.
  • n becomes a shape resembling two conjoint circles, or a dividing cell.
  • n there is considerable variation in the curve's characteristics, as illustrated in Figures 2 to 7. Below a minor to major diameter ratio of approximately 0.625, the curve begins to exhibit central intrusions along the minor axis.
  • Such "pinched" housing configurations provide larger intake/expansion chamber volumes and would be particularly suited for diesel applications where compression ratios exceeding 20: 1 may be required.
  • the engine employs a unique system of synchronised, direct power take-off whereby the rotor directly bears on the crankshaft.
  • the synchronised, direct power transfer system harmonises the rotation of the hinged rotor assembly with the rotation of the crankshaft.
  • Implementation of the arrangement comprises a single-piece crankshaft whose rotation is synchronised with the rotor assembly apices. Power transfer is effected by the rotor segments directly and constantly bearing on crankshaft crankpins. The crankshaft is only in sliding contact with rotor segments and is thus decoupled in the axial direction.
  • the principle of enclosed volume variation described herein is also applicable to pumps, compressors, hydraulic motors and other mechanisms where a working chamber volume cyclic change from a maximum to a minimum is utilised.
  • a two-stroke engine variant is also feasible, provided that each of the intake/compression and expansion/exhaust phases is completed in a quarter (90 degrees) rotation of the four-segment hinged rotor assembly.
  • each of the intake/compression and expansion/exhaust phases is completed in a half (180 degrees) rotation of the four-segment rotor assembly.
  • Szorenyi's curve is generated by the trajectory of the base extremities (points A and B) of an isosceles right-angle translating and simultaneously rotating triangle.
  • Figure 8 to scale, provides a graphical representation of the general construction method.
  • Szorenyi's curve is defined as the locus of all points A' and B' generated by the translating and rotating triangle ABC with the following constraints satisfied:
  • the base length c of the isosceles right-angle generating triangle ABC equals one side of the equilateral parallelogram (or the length of one of the four identical rotor segments) that is continuously accommodated within the confines of the rotor housing having a Szorenyi's curve profile);
  • Szorenyi's curve is additionally characterised by the property that line OA is perpendicular to line OB and, similarly, every line OA' is perpendicular to its corresponding pair, line OB'.
  • Szorenyi's curves are fully characterised by only two parameters; namely the minor and major diameters (or minor and major radii).
  • Computer code embodying the above mathematical relationships defining Szorenyi's curve, is applied to generate exact housing profiles for any user-defined minor to major rotor housing diameter ratio.
  • the hinge pin diameter has to be finite and non-zero.
  • the curve requires modification by expanding it outwards along the normal to Szorenyi's curve at every point by an amount equal to the radius of a finite hinge pin 7.
  • the resultant curve is known as the "Modified Szorenyi's Curve" which forms the basis of practical embodiments. The concept is illustrated in Figures 11, 12, 13 and 14.
  • the engine is ideally suited for directly driving the propellers of aircraft, obviating the need for a reduction gearbox. Direct coupling of the engine to a motor vehicle's drive train may also be feasible.
  • the balanced nature of the rotating gear does not require a flywheel.
  • the engine is expected to be highly responsive providing rapid acceleration.
  • pressurised oil lubrication or a sump There are few moving parts and the engine does not require pressurised oil lubrication or a sump.
  • the crankshaft can be externally supported by sealed roller/ball bearings or carbon/graphite journal bearings. The self-lubricating nature of these bearings makes pressurised lubrication and a sump redundant.
  • Advanced materials such as oil impregnated sintered iron, carbon, graphite, adaptable metal reinforced carbon composites and ceramics may be used to provide self-lubricating solutions.
  • DLC Diamond Like Carbon
  • gas seals are similar to those used in Wankel type rotary engines. These may not require additional lubrication if self-lubricating materials are used. However, if necessary, seal lubrication can be derived from the charge mixture containing a small fraction of lubricating oil.
  • the hinged rotor engine requires no valves or associated valve train and "D" shaped apposite intake ports could be cut into each of the two rotor flat-plate side covers.
  • the peripheral exhaust port located in the rotor housing could have a circular or oval cross section.
  • a peripheral intake port could be employed instead of the side cover intake port(s).
  • the hinged rotor engine's "valve" timing allows some intake/exhaust overlap for scavenging efficiency. There needs to be no unintentional overlap of intake and exhaust ports, direct fuel injection, supercharging and turbo boost may all be employed. The rapid expansion of combustion products would reduce the production of nitrous oxides, lowering undesirable emissions.
  • the engine could run on a variety of fuels, including natural gas and hydrogen.
  • the ignition system is conventional and initiates combustion through a single spark plug.
  • High compression ratios permitting Diesel operation are achievable through varying the rotor segment face radius of curvature and/or shape.
  • Hemispherical cavities may be machined into rotor segment faces to increase intake capacity and provide a combustion chamber shape closer to the spherical ideal.
  • Cooling of the rotor housing may be effected through cooling fins cast or machined into the housing.
  • the stator may be liquid cooled.
  • the rotor assembly is cooled by the charge and additional cooling may be provided by cooling fins machined into the inner surfaces of the rotor segments and by the natural or forced circulation of cooling air through the central core of the engine. Forced circulation of cooling air may be achieved through fan blades attached to the crankshaft or rotor segments. Cooling air entry into and exit from the engine's central core may be controlled through openings cut into the two flat-plate side covers and ducts.
  • Lightweight materials can be employed in construction including aluminium alloys, and ceramic materials to minimise engine weight and achieve high power-to-weight ratios. These engine characteristics would conserve construction materials and energy, as well as reduce fuel consumption in practical installations. Perceived applications for smaller, directly air- cooled engines are light aircraft, UAVs, hybrid road vehicles, portable generating sets, lawnmowers, hand-held machinery and motorcycles. More powerful, and probably liquid cooled, engines could propel larger vehicles. A number of engine units could be joined to a common crankshaft for even greater power output and degree of redundancy.
  • crankshaft having two perpendicular fixed arms that accommodate four equispaced, circularly disposed crankpins.
  • each of the four crankpins remains in constant sliding contact with the convex cylindrical internal contour of the two adjacent rotor segments.
  • the judicious choice of crankpin and rotor materials and/or coatings would obviate the need for lubrication.
  • the sliding friction between crankpins and rotor segments may be substituted with rolling friction. In such a configuration rollers mounted on the four equispaced, circularly disposed crankpins would remain in constant contact with the internal contour of the two adjacent rotor segments.
  • Swivelling roller segments mounted on the four equispaced, circularly disposed crankpins may also have gear teeth, meshing with corresponding gear teeth cut in the internal contour of the two adjacent rotor segments.
  • the crankpins need not be solid but may be hollow to save weight. Additionally, as crankpin contact with the rotor segment is limited to a small arc, the crankpin need not be a complete solid or hollow cylinder, but may be a segment thereof, or an individual crankpin may be replaced by two smaller diameter crankpins.
  • crankarm attachment points to rotor segments is critical and must coincide with the longitudinal axes of the cylindrical lobes of rotor segments. This method of attaching the rotor segments to the crankshaft is illustrated in Figures 15 and 16. The four pairs of identical crankarms 9 would be alternately attached to the top and bottom halves of the four equispaced, circularly disposed crankpins.
  • Plan view schematics of the preferred implementation of the engine are at Figures 17 and 18.
  • Engine rotation is clockwise, as shown by the arrows.
  • the figures also indicate the positioning of the peripheral inlet port 10, peripheral exhaust port 11 and spark plug hole 12 in the rotor housing 2.
  • Power transfer is directly obtained through rotor segment convex cylindrical inner profiles 13 bearing on the crankpins 6, with which they are in constant sliding contact.
  • Rotor segment outer faces 14 are convex to produce the desired compression ratio of maximum to minimum working chamber volumes required for operation in the internal combustion engine mode.
  • Rotor segment inner surfaces have convex cylindrical contours 13 for the direct transfer of motive power by being in continuous contact with the crankpins 6 attached to the crankshaft 8.
  • a computer application program is used to calculate the required convex cylindrical rotor segment contours for any combinations of rotor housing and rotor assembly dimensions, crank and crankpin radii.
  • a typical rotor segment is shown in Figure 19.
  • each adjacent pair of rotor segments are joined with an "anchor block" 15; front and rear views shown in Figure 20.
  • the figure also illustrates the way each anchor block holds the tips of adjacent rotor segments 16 in a pivoting labyrinth arrangement, providing a gas-tight seal. This method of attachment permits articulated movement of one rotor segment relative to the other, and relative to the anchor block.
  • the four anchor blocks are essential components of the hinged rotor assembly in linking the four rotor segments and also providing receptacles for gas seals. Seals
  • Each anchor block incorporates a radially outward facing axial apex seal/seal spring slot 17 and top and bottom corner seal/seal spring cavities 18.
  • Each complete rotor segment comprises the rotor segment body 19 and firmly attached top and bottom closure plates 20. These integral closure plates lock-in the anchor blocks and contain grooves for the side seals and side seal springs. The corresponding disposition of conventional apex 21, side 22 and corner 23 seals in the anchor block/rotor segment assembly is shown in the exploded view of Figure 21.
  • crankshaft rotation is synchronised with the rotation of the rotor assembly apices (hinges). If power transfer were effected by linking the crankshaft to the midpoints (P) of rotor segments (which are always on the inscribed circle of radius c/2), rotation of the crankshaft would become irregular. This irregularity results from the non-uniform rotation/translation of the rotor segment midpoints around the inscribed circle in relation to the constant rotation of the rotor assembly apices.
  • Double-concave, open-face bearing blocks may be inserted between the convex cylindrical rotor segment inner profiles and crankpins to increase contact surface area and reduce loading.
  • These bearing blocks may be made from a self-lubricating material (such as carbon- graphite) and may consist of scarf-jointed segments to compensate for wear. The concept is illustrated in Figure 22.
  • crankshaft Being in sliding contact only, the crankshaft is axially decoupled from the rotor assembly. Therefore, the rotor assembly is not subjected to any lateral (axial) load.
  • Simple thrust washers mounted on the crankshaft shoulders may be employed to bear any axial load acting on that component, for instance load that may result from the clutch being depressed in automotive applications.
  • a system of track rollers 25 and associated tracks 26 is employed.
  • Two track rollers, one on either side, are mounted on each rotor segment as shown in Figure 24.
  • the roller shafts are inserted in corresponding axial holes in the rotor segment bodies.
  • the position and diameter of track rollers are optimised to ensure that the corresponding track profile has a gradually changing convex curvature and that the rotational speed of track rollers is not excessive.
  • Track plates are internally attached to each of the two flat-plate side covers 3, illustrated in Figure 25.
  • the tracks are not identical; the second track profile is obtained by rotating the first one through 180°, either about the x-axis or the y-axis.
  • the symmetric relationship between guide tracks is shown in Figure 26.
  • Pinion gears that mesh with corresponding gear teeth cut into the circumferences of tracks may be substituted for track rollers and smooth tracks.
  • the track rollers also provide lateral (or axial) positioning for the rotor assembly, relative to the rotor housing and flat-plate side covers. This function is achieved by permitting the rims 27 of the track rollers 25, attached to the rotor segments, to ride on the extended base platform 28 of the track 26.
  • flanged rollers 29 may be used riding on the inner profile edge 30 of the track 26.
  • Plan views of the engine are in Figures 29 and 30, showing the assembled parts, including track rollers and associated tracks.
  • Figure 31 a perspective of major engine components is provided in Figure 31.
  • the flat-plate side covers and attached tracks are removed for clarity.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

Moteur à combustion interne rotatif comprenant un ensemble rotor articulé possédant quatre segments et logeant dans un carter coaxial, de façon à se déformer et à s'adapter en continu au profil intérieur du carter pendant sa rotation. Ce profil intérieur du carter du rotor non circulaire fermé consiste en une courbe définie par un nouveau rapport mathématique. Cette courbe est le locus de la totalité des points générés par les extrémités de base A et B d'un triangle isocèle effectuant une translation à angle droit et une rotation simultanée avec les contraintes suivantes: le centre P de la base AB (de longueur c) du triangle doit toujours être situé sur un cercle inscrit de rayon c/2 et centre au niveau du point O; le sommet C du triangle doit toujours être situé sur un des quatre lobes de la courbe de forme r = cos(2υ), où l'angle υ est l'angle entre la ligne OA et l'axe (y) vertical positif et également la ligne OB et l'axe (x) horizontal positif.
PCT/AU2001/000544 2000-05-12 2001-05-11 Moteur a combustion interne possedant un rotor articule Ceased WO2001088341A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2001584712A JP3676303B2 (ja) 2000-05-12 2001-05-11 ヒンジ結合ロータ型内燃エンジン
EP01929123A EP1285149A4 (fr) 2000-05-12 2001-05-11 Moteur a combustion interne possedant un rotor articule
US10/149,913 US6718938B2 (en) 2000-05-12 2001-05-11 Hinged rotor internal combustion engine
CA002425487A CA2425487C (fr) 2000-05-12 2001-05-11 Moteur a combustion interne possedant un rotor articule
AU2001256006A AU2001256006A1 (en) 2000-05-12 2001-05-11 Hinged rotor internal combustion engine
KR1020027015139A KR100854573B1 (ko) 2000-05-12 2001-05-11 힌지식 로터 내연 기관

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
AU24071/00A AU2407100A (en) 1999-01-07 2000-01-06 Fabrication of particulate tapes by electrophoretic deposition
AU34071/00A AU726791B1 (en) 2000-05-12 2000-05-12 Hinged rotor internal combustion engine
AU34071/00 2000-05-12

Publications (1)

Publication Number Publication Date
WO2001088341A1 true WO2001088341A1 (fr) 2001-11-22

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Family Applications (1)

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PCT/AU2001/000544 Ceased WO2001088341A1 (fr) 2000-05-12 2001-05-11 Moteur a combustion interne possedant un rotor articule

Country Status (1)

Country Link
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1484474A1 (fr) * 2003-06-03 2004-12-08 Giovanni Donato Moteur endothermique à pistons rotatifs
WO2008107547A1 (fr) * 2007-01-19 2008-09-12 Philippe Kuzdzal Moteur rotatif a losange deformable
WO2010031927A1 (fr) 2008-09-22 2010-03-25 Vincent Genissieux Machine rotative a losange deformable multifonctions
FR2950926A1 (fr) * 2009-10-05 2011-04-08 Pk Enr Moteur a pistons rotatifs
US8951028B2 (en) 2008-11-12 2015-02-10 Vincent Genissieux Rotary machine of the deformable rhombus type comprising an improved transmission mechanism

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3369529A (en) * 1966-09-29 1968-02-20 Alfred Jordan Rotary internal combustion engine
DE2321763A1 (de) * 1973-04-30 1974-11-14 Bach Rotationskolbenmaschine
US3918415A (en) * 1972-09-19 1975-11-11 Ishida Industry Company Limite Rotary internal combustion engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3369529A (en) * 1966-09-29 1968-02-20 Alfred Jordan Rotary internal combustion engine
US3918415A (en) * 1972-09-19 1975-11-11 Ishida Industry Company Limite Rotary internal combustion engine
DE2321763A1 (de) * 1973-04-30 1974-11-14 Bach Rotationskolbenmaschine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1285149A4 *

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1484474A1 (fr) * 2003-06-03 2004-12-08 Giovanni Donato Moteur endothermique à pistons rotatifs
WO2008107547A1 (fr) * 2007-01-19 2008-09-12 Philippe Kuzdzal Moteur rotatif a losange deformable
WO2010031927A1 (fr) 2008-09-22 2010-03-25 Vincent Genissieux Machine rotative a losange deformable multifonctions
EP3045656A1 (fr) 2008-09-22 2016-07-20 Vincent Genissieux Machine rotative a losange deformable multifonctions
US9523276B2 (en) 2008-09-22 2016-12-20 Vincent Genissieux Multifunction rotary machine with deformable rhomb
US8951028B2 (en) 2008-11-12 2015-02-10 Vincent Genissieux Rotary machine of the deformable rhombus type comprising an improved transmission mechanism
FR2950926A1 (fr) * 2009-10-05 2011-04-08 Pk Enr Moteur a pistons rotatifs
WO2011042648A2 (fr) 2009-10-05 2011-04-14 Pk-Enr Moteur à pistons rotatifs
WO2011042648A3 (fr) * 2009-10-05 2012-04-05 Pk-Enr Moteur à pistons rotatifs

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