WO2003008781A1 - Moteur a pistons rotatifs - Google Patents

Moteur a pistons rotatifs Download PDF

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Publication number
WO2003008781A1
WO2003008781A1 PCT/US2002/019112 US0219112W WO03008781A1 WO 2003008781 A1 WO2003008781 A1 WO 2003008781A1 US 0219112 W US0219112 W US 0219112W WO 03008781 A1 WO03008781 A1 WO 03008781A1
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WIPO (PCT)
Prior art keywords
gear
type
gears
piston
sakita
Prior art date
Application number
PCT/US2002/019112
Other languages
English (en)
Inventor
Masami Sakita
Original Assignee
Masami Sakita
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 US09/910,545 external-priority patent/US6457451B1/en
Application filed by Masami Sakita filed Critical Masami Sakita
Publication of WO2003008781A1 publication Critical patent/WO2003008781A1/fr

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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
    • F01C1/02—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F01C1/063—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them
    • F01C1/077—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them having toothed-gearing type drive
    • 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
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines

Definitions

  • This invention relates generally to rotary piston engines and in particular to rotary piston engines that include first- and second-piston assemblies that are interconnected for alternate variable-speed rotation whereby pistons of the slower piston assembly comprise trailing pistons during the power and intake phases of the engine operating cycle.
  • the present invention is an extension of the work presented in U.S. Patent 5,381 ,766 by the present inventor, Sakita.
  • the present inventor described a rotary engine equipped with a gear mechanism that enables intermittent rotation of pistons, namely, the stopping of the trailing pistons while the leading pistons are rotating at maximum speed.
  • the gear mechanism provides said engine with the smallest overall working chamber and the thinnest piston to produce a specified output.
  • some applications including the aforementioned spark plug adoption or adoption in diesel engines in which robust structures are required, may require thicker pistons than are possible in engines with intermittent rotation of pistons.
  • engines with intermittent operation may not necessarily be the most efficient; this is because the nonstopping piston of the intermittent operation engine rotates faster than the faster piston in the nonintermittent rotation engine, and may cause higher mechanical loss.
  • the present inventor felt the need to devise a gear set that allows rotation of the pistons for any designed speed profiles.
  • gear teeth may be used if gear teeth are not attached in the vicinity of the teardrop-shaped gear's apex and the corresponding sections of the heart-shaped gear; not attaching gear teeth at a portion of the heart- and teardrop-shaped gears, however, would require the gears to be twice as thick. This is another area for improvement the present invention addresses.
  • Another improvement focused on in the present invention is the adoption of technologies that are known to further improve engine output and energy efficiency with no or little additional power requirements, such as the use of different compression ratios for compression and expansion (U.S. Patent Number 5,433,179 - Wittry) and the use of an air nozzle for scavenging exhaust air (NACA Report No.469, Increasing the Air Charge and Scavenging the Clearance Volume of a Compression-Ignition Engine, J.S. Spanogle, C. W. Hicks, and H. H. Foster, Langley Field, VA, June 1933).
  • An object of this invention is the provision of a working chamber that is equipped with a means to allow easy access to spark plugs installed inside the piston assembly.
  • An object of this invention is the provision of interconnecting piston assemblies to enable variable-speed operation of the pistons as specified by the engine designer.
  • An object of this invention is the provision of a pair of gears that remain engaged at all times while rotating with specified rotational speed profiles.
  • An object of this invention is the provision of a working chamber such that the compression ratio computed as the maximum volume of the compression subchamber over the minimum volume of the compression subchamber is in an acceptable range for a given engine type but will be higher if the compression ratio is computed as the maximum volume of the combustion subchamber over the minimum volume of the combustion subchamber, wherein the minimum volume of the compression subchamber equals the minimum volume of combustion subchamber.
  • An object of this invention is the provision of a working chamber equipped with an exhaust port wider than the piston width to permit ending of the expansion phase before the piston reaches the end of the combustion phase.
  • An object of this invention is the provision of an air nozzle that is installed at the mouth of the exhaust port to scavenge the exhaust air that remains within the exhaust subchamber at the end of the cycle.
  • An object of this invention is the provision of a pair of gears that are equipped with teeth specially designed for gears with variable rotational speeds.
  • the present invention includes an engine with working chamber within which the first and second piston assemblies rotate about a rotational axis.
  • Each piston assembly includes a hollow piston hub to which one or more pairs of diametrically opposed pistons are attached.
  • the pairs of pistons divide the working chamber into a plurality of subchambers in which a single pair of diametrically opposed pistons per piston assembly provides four subchambers in the working chamber, and two pairs of diametrically opposed pistons per piston assembly provide eight subchambers in the working chamber.
  • a spark plug having electrodes with spark gaps is installed within the piston assembly such that the electrodes communicate with a subchamber through a hole bored at the center of the piston surface.
  • a spark plug maintenance hole is bored on the side of the engine housing for accessing the spark plug from outside.
  • the first and second piston assemblies are connected to the first and second input shafts, respectively, of the differential means for rotation in the same direction. With one complete revolution of the piston assemblies, four engine operating cycles are completed for a four-piston engine and eight operating cycles are completed for an eight-piston engine, with each operating cycle comprising the power, exhaust, intake, and compression phases.
  • the interconnection between the first and second piston assemblies results in rotation of each piston such that as the leading piston increases its rotational speech the trailing piston decreases its rotational speed, and as the leading piston decreases its rotational speed, the trailing piston increases its rotational speed.
  • the engine's working chamber includes a compression subchamber that is smaller than the combustion subchamber.
  • the intake port, exhaust port, and piston widths are adjusted so that the compression ratio computed as the maximum volume over the minimum volume of the compression subchamber will be within the normally acceptable range for a given engine type, but the compression ratio computed as the maximum volume over the minimum volume of the combustion subchamber is generally higher than the normal compression ratio.
  • the present invention includes differential means having first and second input shafts and an output shaft, together with first and second noncircular gear sets.
  • Each of the first and second gear sets includes two types of intermeshing noncircular gears we call Sakita type 1 and type 2 gears (or type 1 and type 2 gears).
  • the extension of the differential output becomes the output shaft, which is connected through a circular gear set to an idler shaft to which type 2 gears are affixed.
  • the type 1 gears of the first and second gear sets are connected to the first and second differential input shafts, respectively.
  • the type 1 gears rotate with widely varying speeds, while the type 2 gears rotate at the same rate as the output shaft of the engine.
  • the differential assures that the sum of the rotational speeds of the type 1 gears equals twice the rotational speed of the type 2 gears.
  • each of the first and second gear sets includes gears which we call the Wildhaber-Sakita type 1 and type 2 gears (or to avoid confusion, simply the type 3 and type 4 gears, respectively).
  • the extension of the differential output becomes the output shaft, which is connected through a circular gear set to an idler shaft to which type 4 gears are affixed.
  • the type 3 gears of the first and second gear sets are connected to the first and second differential input shafts, respectively.
  • the type 3 gears rotate with widely varying speeds, while the type 4 gears rotate at twice the rate of the output shaft of the engine.
  • the differential assures that the sum of the rotational speeds of the type 3 gears equals the rotational speed of the type 4 gears.
  • Fig. 1 is an exploded isometric view of a rotary piston engine embodying the present invention
  • Fig. 2 is a cross-sectional view of the working chamber with a detailed view of the ball bearings
  • Fig. 3 is an enlarged sectional view taken along line A-A of Fig. 2;
  • Fig. 4 is a skeletal view of piston assemblies with emphasis on sealing rings, a view taken from B of Fig. 2;
  • Fig. 5 is a schematic illustration showing separation of functions within the working chamber of a four-piston engine
  • Fig. 6 is a schematic illustration showing separation of functions within the working chamber of an eight-piston engine
  • Fig. 7 is a diagram showing the rotational speed profile of type 1 and type 2 gears
  • Fig. 8 is a schematic diagram of type 1 and type 2 gears with no gear teeth shown;
  • Fig. 9 is a diagram of geometries of the type 1 and type 2 gears with no gear teeth shown;
  • Fig. 10 is a detailed view of gear geometries near the rotational axis of the type 2 gear
  • Fig. 12 is a diagram showing a type 1 and type 2 gear set
  • Fig. 13 is a diagram showing the process of arranging gear teeth of type 1 and type 2 gears
  • Fig. 14 is an enlarged view of curves involved in the type 1 and type 2 gears' teeth, with a detailed view of a selected area;
  • Fig. 15 is an enlarged view showing the meshing of type 1 and type 2 gears
  • Fig. 16 is an enlarged view showing the meshing of modified type 1 and type 2 gears
  • Fig. 17 is a diagram showing the front view of an alternative type 1 and type 2 gear set
  • Fig. 18 a diagram showing the side view of said alternative type 1 and type 2 gear set
  • Fig. 19 is a diagram of type 1 and type 2 gears with no gear teeth shown;
  • Fig. 20 is a diagram showing the rotational speed profile of type 1 and type 2 gears
  • Fig. 21 is a diagram showing the relationship between piston positions and type 1 and type 2 gear positions
  • Fig. 22 is an exploded isometric view of a rotary piston engine's working chamber in an alternative embodiment of the present invention.
  • Fig. 23 is a cross-sectional view of an alternative design of the engine's working chamber
  • Fig. 24 is a schematic diagram of type 3 and type 4 gears
  • Fig. 25 is a diagram showing the rotational speed profile of type 3 and type 4 gears
  • Fig. 26 is a schematic diagram of type 3 and type 4 gears with no gear teeth shown similar to that of Fig. 24, but shown the gears at different positions;
  • Fig. 27 is a diagram of geometries of the type 3 and type 4 gears with no gear teeth shown
  • Figs. 29A through 29D show, using mathematical notations and commonly used Greek letters for some variables and constants, Equations (1) through (24) described in this Specification.
  • FIG. 1 of the drawings wherein an engine 20 is shown to include a stationary cylindrical housing 22 having a bore that is closed at opposite ends by engine's housing walls 24 and 26 attached thereto as by bolts or other suitable means, not shown, containing a toroidal working chamber inside.
  • the engine's working chamber formed by piston assemblies 30, 32 and stationary outer cover 59 is divided into first and second pairs of diametrically opposed subchambers by pistons included in first and second piston assemblies 30 and 32.
  • the piston assemblies 30 and 32 are rotatable about a common axis 40 and, in operation, rotate in the same direction as indicated by arrows 42.
  • Piston assembly 30 includes a pair of diametrically opposed pistons 30A and 30B attached to piston hub 30C
  • piston assembly 32 includes a pair of diametrically opposed pistons 32A and 32B attached to piston hub 32C.
  • Pistons 30A and 30B are affixed to the outer piston shaft 36 through piston hub 30C.
  • the inner piston shaft 38 is rotatably mounted in the tubular shaft 36.
  • Pistons 32A and 32B of second piston assembly 32 are attached to inner piston shaft 38 through piston hub 32C at diametrically opposed positions.
  • the working chamber is divided into two pairs of diametrically opposed subchambers by four pistons 30A, 30B, 32A, and 32B in a four-piston engine as shown in Fig. 1.
  • Each piston assembly alternately rotates with a faster and slower speed such that trailing pistons rotate at a slower speed than leading pistons during the power and intake phases of engine operation, and periodically variable volume subchambers are provided between adjacent pistons.
  • the engine housing 22 has an opening for an exhaust port 54, and an opening for an intake port 56.
  • Engine's working chamber is also shown in Figs. 2 and 3 of the drawings.
  • FIG. 2 of the drawings wherein are shown the engine housing 22 comprising an outer cover 59 and housing walls 24 and 26, within which piston assemblies 30 and 32 are located. Openings for port 27 in the engine housing walls are provided, through which air or another type of gas used for cooling is brought into the hollow piston assemblies 30 and 32.
  • the cooling gas is sent from the outer end of the piston assemblies 30 and 32 to the outer cover 59 through openings 30E and 32E and then back to the air or gas pump, which is equipped with an air/gas cooling mechanism, not shown, from port 21 of the outer cover 59.
  • a spark plug 14 is housed in a casing 12 inside piston 32A with no openings at one end, one opening 11 on a side, near the end of the casing facing a near-side subchamber in Fig. 2, and another opening at the other end of casing 12 facing wall 26.
  • a spark plug maintenance hole 32D is included on wall 26 of the engine housing for access to spark plug 14 carried by pistons 32A and 32B for removal and replacement of the spark plug. Spark plug 14 communicates with a subchamber through opening 11.
  • a power terminal case 19 made of a nonconductive material is installed within the piston assembly 32 to function as a socket to the spark plug 14.
  • the power terminal case 19 has two electric terminals 16 made of conductive material from which the spark plug 14 takes electricity.
  • spark plug 14 gets electricity from terminals 16.
  • a seal 18 secures the spark plug 14 in its place and seals off the casing 12 from the outer atmosphere.
  • a spark plug is provided for each of the subchambers into which the working chamber is divided by the pistons.
  • a spark plug 14 and its peripheral parts that are housed in piston 32B are shown in Fig. 2 in dotted line.
  • spark plug 14 embedded in pistons 30A and 30B are accessible through a spark plug maintenance hole 30D in housing wall 24.
  • Means to support horizontal forces, such as ball bearing 25, which comprising a main bearing ball 25A, smaller bearing balls 25B and support rings as shown in Fig. 2A, are placed between piston assemblies 30 and 32, between piston assembly 30 and wall 24, and between piston assembly 32 and wall 26.
  • Conventional ball bearings 25C are placed between piston assembly 30 and outer cover 59 and between piston assembly 32 and outer cover 59.
  • FIG. 3 of the drawings wherein the toroidal working chamber's outer cover 59 comprising an upper half 59A and a lower half 59B, attached by means such as bolts 59C, is shown.
  • the outer cover 59 has an exhaust port 54, the width of which is generally the same as the piston width, but it may be cut wider than the piston width in the direction of piston travel if needed for better breathing or for preventing the gas pressure in the exhaust subchamber from becoming lower than the outside atmospheric pressure.
  • the outer cover 59 is also equipped with an intake port 56, which is generally cut wider than the piston width and also the exhaust port in the direction of piston travel.
  • the maximum volume of the compression subchamber is generally smaller than the maximum volume of the combustion subchamber, and the piston width is adjusted so that the compression ratio computed as the maximum volume of the compression subchamber over the minimum volume of the compression subchamber is in an acceptable range for a given engine type. Consequently, the compression ratio computed as the maximum volume of the combustion subchamber over the minimum volume of the combustion subchamber may be higher than the normally acceptable range.
  • the exhaust port is provided with an air nozzle 79 at its mouth to spray fresh air into the exhaust subchamber for scavenging the remaining exhaust air inside the subchamber. Referring to Fig.
  • sealing of subchambers to prevent the flow of gases therebetween is provided by any suitable means, including for example, semicircular piston rings 50 along the outer convex surfaces of pistons 30A and 30B and semicircular piston rings 52 along the outer convex surfaces of pistons 32A and 32B.
  • Circular seal means 47 (not shown in Fig. 4, but shown in Fig. 2) is placed along the crevice between piston assembly 32 and outer cover 59, and circular seal means 48 is placed along the crevice between piston assembly 30 and outer cover 59 for sealing engagement between each of the piston assemblies and the outer cover.
  • a circular seal means 46 is placed along the crevices between the piston assemblies for sealing engagement between the two piston assemblies.
  • the working chamber is divided into four subchambers.
  • the power phase of engine operation occurs during the angular movement of the leading piston is within segment arrow 62;
  • the exhaust phase of the engine occurs during the angular movement of the trailing piston is within segment 62;
  • the intake phase occurs during the angular movement of the leading piston is within segment 64;
  • the compression phase occurs during the angular movement of the trailing piston is within segment 64. If one of the pistons is within segment 62, we say that the piston assembly is in the active phase, and if one of the pistons is within segment 60, we say that the piston assembly is in the nonactive phase.
  • piston assembly 30 that includes pistons 30A and 30B has just finished the nonactive phase and is just about to start the active phase
  • piston assembly 32 that includes pistons 32A and 32B has just finished the active phase and is just about to start the nonactive phase.
  • the exhaust port 54 and intake port 56, and a fuel injection nozzle 58 which is connected to the source of fuel, injects fuel into the compression subchamber following intake of air through intake port 56 are also shown in Fig. 5.
  • the working chamber is divided into eight subchambers.
  • the power phase of engine operation occurs during the angular movement of the leading piston is within segment arrow 62-A; the exhaust phase of the engine occurs during the angular movement of the trailing piston is within segment 62-A; the intake phase occurs during the angular movement of the leading piston is within segment 64-A; and the compression phase occurs during the angular movement of the trailing piston is within segment 64-A. If one of the pistons is within segment 64-A, we say that the piston assembly is in the active phase, and if one of the pistons is within segment 60-A, we say that the piston assembly is in the nonactive phase. Fig.
  • piston assembly 30-A that includes pistons 30A-A and 30B-A has just finished the nonactive phase and is just about to start the active phase
  • piston assembly 32-A that includes pistons 32A- A and 32B-A has just finished the active phase and is just about to start the nonactive phase.
  • Exhaust ports 54-A and intake ports 56-A, and fuel injection nozzles 58-A which are connected to the source of fuel, inject fuel into the compression subchambers following intake of air through intake ports 56-A are also shown in Fig. 6.
  • Connecting means identified generally by reference numeral 66, for operatively connecting the first and second piston assemblies 30 and 32 to an engine output shaft 86 and for providing the piston assemblies with variable speed rotation, now will be described with reference to Fig. 1.
  • connecting means 66 includes circular gear sets 70 and 72, noncircular gear sets 74 and 76, differential means 78, and circular gear set 80. Suffixes A and B are used to identify the separate gears of the gear pairs.
  • Gear 70A of gear set 70 is connected to piston assembly 30 through outer piston shaft 36
  • gear 72A of gear set 72 is connected to the other piston assembly 32 through inner piston shaft 38.
  • circular gear pairs 70 and 72 are provided with a 1 :2 gear ratio whereby gears 70B and 72B undergo two complete revolutions for each complete revolution of piston shafts 36 and 38, respectively.
  • gear ratio of gear pairs 70 and 72 is 1 :4, whereby gears 70B and 72B undergo four complete revolutions for each complete revolution of piston shafts 36 and 38, respectively.
  • the rest of the gear and shaft arrangement in connecting means 66 for an eight-piston engine is identical to that of a four-piston engine.
  • Circular gears 70B and 72B are affixed to tubular shafts 82 and 84, respectively, which are rotatably mounted on spider shaft 86 of differential 78.
  • Spider shaft 86 which for purposes of description also is defined as the differential output, is supported by suitable bearings, not shown, for rotation about axis 88, which extends parallel to piston shaft axis 40.
  • Spider shaft 86 is also the engine output shaft, which is connected through a circular gear set 80 to an idler shaft 68 to which gears 74B and 76B are affixed.
  • Affixed to tubular shaft 82 are gear 74A of noncircular gear set 74 and end gear 78A of differential 78 for simultaneous rotation thereof with gear 70B.
  • tubular shaft 84 has affixed thereto gear 76A of noncircular gear set 76 and end gear 78B of differential 78 for simultaneous rotation thereof with gear 72B.
  • shafts 82 and 84 to which differential end gears 78A and 78B are affixed are defined as differential inputs.
  • Differential 78 may be of any conventional type such as the illustrated bevel gear differential which, in addition to end, or sun, gears 78A and 78B, includes spider, or planet, gears 78C and 78D rotatably mounted on spider cross shaft 78E. Spider gears 78C and 78D mesh with end gears 78A and 78B.
  • noncircular gear sets 74 and 76 are of the same design.
  • connecting means that does not include differential 78 and uses shaft 68 as the output shaft is possible.
  • WO rotational speed of spider shaft 86 and gear 80A
  • W1 rotational speed of sun gear 78A
  • W2 rotational speed of sun gear 78B.
  • gears 78A and 78B are connected to gears 74A and 76A, respectively, and gear 80B that meshes with 80A at the ratio of 1 :1 is connected to gears 74B and 76B, the relationship given in (1) holds for
  • WO rotational speed of gears 74B and 76B
  • W1 rotational speed of gear 74A
  • W2 rotational speed of gear 76A.
  • Operation of the connecting means 66 will best be understood with reference to Figs. 7 and 8 of the drawings.
  • the speed profile of type 1 gears shows the way the speed of type 1 gears 74A and 76A vary as they rotate relative to the rotational angle of type 2 gears 74B and 76B, wherein type 2 gears 74B and 76B keep a constant rotational speed WO.
  • the horizontal axis (Q) indicates the rotational angle of type 2 gears 74B and 76B in radian
  • the vertical axis (W) indicates the rotational speed of type 1 gears 74A and 76A and type 2 gears 74B and 76B.
  • the rotational speed of type 1 gear 74A is represented by 74A-S
  • that of type 2 gear 74B is represented by 74B -S
  • that of type 2 gear 76B by 76B-S.
  • the positions of type 1 and type 2 gears corresponding to the gear operation at time point T in Fig. 7 are given in Fig. 8.
  • rotational angle of type 2 gears 74B and 76B measured from the end of circular segments 104 and 102, respectively, is Q (99).
  • type 1 gear 74A is at 101Y, the end of circular segment 101 (Fig. 8), ready to increase its rotational speed, and typel gear 76A is at 100Y, the end of circular segment 100 (Fig. 8), ready to decrease its rotational speed. While type 2 gears 74B and 76B each travels Q (99), type 1 gear 74A travels Qy1 (97) and type 1 gear 76A travels Qy2 (98) as shown in Fig. 8. In Fig. 7, type 1 gear 74A is at 101Y, the end of circular segment 101 (Fig. 8), ready to increase its rotational speed, and typel gear 76A is at 100Y, the end of circular segment 100 (Fig. 8), ready to decrease its rotational speed. While type 2 gears 74B and 76B each travels Q (99), type 1 gear 74A travels Qy1 (97) and type 1 gear 76A travels Qy2 (98) as shown in Fig. 8. In Fig.
  • Type 1 gear 74A rotates at maximum speed, Wmax, and type 1 gear 76A rotates at minimum rotational speed, Wmin, between Q1 and pi, during which time gear set 74 meshes at the circular segments 100 and 102 of gears 74A and 74B, respectively, while gear set 76 meshes at the circular segments 101 and 104 of gears 76A and 76B, respectively.
  • Type 1 gear 74A rotates at minimum rotational speed, Wmin
  • type 1 gear 76A rotates at maximum rotational speed, Wmax, between pi+Q1 and 2pi, during which time gear set 74 meshes at the circular segments 101 and 104 of gear 74A and 74B, respectively, while gear set 76 meshes at the circular segments 100 and 102 of gears 76A and 76B, respectively.
  • the rotational angle of type 1 gear 74A while type 2 gear 74B rotates from Q1 to pi is Q3
  • the rotational angle of type 1 gear 76A while type 2 gear 76B rotates from Q1 to pi is Q4.
  • Fig. 9 of the drawings wherein geometries of the noncircular gear set 74 with no gear teeth (or gear bodies of gear set 74) are depicted in detail.
  • Fig. 10 shows details of the gear geometries in the vicinity of the rotational axis 90 of the type 2 gear 74B.
  • Noncircular gear sets 74 and 76 are of the same design so that a detailed description of only one is required.
  • gear set 74 is shown in the position illustrated in Fig. 1, which is 180 degrees out of phase with gear set 76.
  • gears 74A and 74B rotate in the direction of arrows 94 and 96, respectively.
  • the geometries of type 1 and type 2 gears 74A and 74B are determined by the maximum and minimum rotational speeds of type 1 gear 74A relative to the rotational speed of type 2 gear 74B, the angle traveled by type 2 gear 74B while type 1 gear 74A is traveling at these extreme rotational speeds, and the speed profile of type 1 gear relative to the rotational speed of type 2 gear 74B between the two extreme rotational speeds.
  • Y1 radius of circular arc segment 100 of type 1 gear 74A in which the type 1 gear operates at maximum speed (Fig. 9)
  • Y2 radius of circular arc segment 101 of type 1 gear 74A in which the type 1 gear operates at minimum speed (Fig. 10)
  • X1 radius of circular arc segment 102 of type 2 gear 74B in which it meshes with the type 1 gear operating at maximum speed (Fig. 9)
  • X2 radius of circular arc segment 104 of type 2 gear 74B in which it meshes with the type 1 gear operating at a minimum speed (Fig. 10)
  • D distance between the centers of the rotational axes of the type 1 and type 2 gears (Fig. 9).
  • Y1 D/(2 + alpha)
  • Y2 D/(2 - alpha)
  • X1 D(1 + alpha)/(2 + alpha)
  • alpha signifies Greek letter "alpha.”
  • the distance between the rotational center and the point of contact with the type 2 gear varies from Y1 to Y2, and Y2 to Y1 ; and in the nocircular curve segments of the type 2 gear, the distance between the rotational center and the point of contact with the type 1 gear varies from X1 to X2, and X2 to X1.
  • Y1 , Y2, X1 , and X2 defined in Equations (2) through (5) hold for all speed profiles.
  • Y1 and X1 given in (2) and (4), respectively, are shown in Fig. 9, and Y2 and X2 given in (3) and (5), respectively, are shown in Fig. 10.
  • Q0 (105) is the angle created by the type 1 gear's apex, the rotational center of the gear, and its point of contact with the type 2 gear; and at which point the speeds of the type 1 and type 2 gears all become equal; Q0 also is half the angle the type 1 gear travels (in the four piston engine) in the nonactive phase.
  • angle Q0 the equi-speed angle.
  • Q1 is the rotational angle of the noncircular segment 106 of the type 1 gear, and it is also the rotational angle of the noncircular segment 107 of the type 2 gear;
  • Q2 is the rotational angle of each of circular segments 102 and 104 of the type 2 gear;
  • Q3 is the rotational angle of the circular segment 100 of the type 1 gear;
  • Q 4 is the rotational angle of the circular segment 101 of the type 1 gear.
  • Q0 equals the angle of rotation of the trailing piston in the nonactive phase, and it also equals the sum of the thickness of a piston and the gap created by the two pistons when they are closest to each other; half of Q3 equals the rotational angle of the piston at maximum speed, and half of Q4 equals the rotational angle of the piston at minimum speed.
  • type 1 and type 2 gears for a special case in which the type 1 gear follows a rotational speed profile that has sinusoidal curve segments and constant speed segments, and the type 2 gear operates at a constant speed are described below.
  • Equation (6) D is the distance between the rotational centers of the type 1 and 2 gears.
  • the rotational speed of the type 1 gear 76A in the noncircular segment that starts at the end of the circular segment with smaller radius (end of rotational speed Wmax) and ends at the beginning of the lareger radius (start of rotational speed Wmin) is expressed as:
  • Equation (7) reads W equals WO plus (WO - Wmin) multiplied by cosine [Q multiplied by (pi) divided by Q1].
  • Fig. 11 of the drawings wherein sample type 1 and type 2 gear designs 74A-A and 74B-A, respectively, are shown.
  • the type 1 gear 74A has a teardrop-shaped body with a round apex, and the corresponding type 2 gear 74B has a heart-shaped body with a round shallow cusp.
  • the type 1 gear is formed with two noncircular segments, in each of which the radius (or the distance between the center of rotation to the contact point with the other gear) changes from 0.37D to 0.77D.
  • the type 2 gear is formed with two noncircular arc segments, in each of which the radius (or the distance between the center of rotation to the contact point with the other gear) changes from 0.63D to 0.23D.
  • the physical geometries of the type 1 and type 2 gears also change.
  • the type 1 and type 2 gears of both gear sets operate perfectly well under any speed variation of the type 2 gear, because rotational speeds of the type 1 gears has been defined relative to rotational speed of the type 2 gears, and thus, any increase/decrease in rotational speed of the type 2 gears will incur proportionately higher/lower rotational speed of the type 1 gears, and any increase/decrease in rotational angle traveled by the type 2 gears due to the rotational speed change within a given time period will incur proportionately higher/lower rotational angle traveled by the type 1 gears in the same time period.
  • a gear set 74 comprising a type 1 gear 74A and a corresponding type 2 gear 74B is shown with outwardly extending round- shaped gear teeth 77 and 79 about the peripheries thereof.
  • the type 1 gear 74A is shown affixed to tubular shaft 82 which, in turn, is rotatably supported on shaft 86 rotatable about shaft axis 88.
  • heart-shaped gear 74B is shown attached to shaft 68 rotatable about axis 90.
  • Pitch line is a line that connects gear teeth's points of contact under special circumstance, in which the contact point is on the line that connects the rotational centers of the two gears.
  • the type 1 and type 2 gears contact each other at the sides of the gear teeth in segments where gear teeth are placed and at the body of the gears represented by the pitch lines near the apex of the type 1 gear and at the concave segment of the type 2 gear.
  • the gear design may be best understood by describing the step-by-step process involved in arranging the gear teeth of the type 1 and type 2 gears with reference to Figs. 13 through 15 of the drawings.
  • the letters A through C in parentheses in the text match the view letters A through C in Fig. 13.
  • FIG. 14 of the drawings showing an expanded view of two neighboring circles with their centers on 100A and 102A, wherein circle 77A is on the periphery 100A of gear body 74A-1 , and circle 79A is on the periphery 102A of gear body 74B-1.
  • Circles 77A and 79A intersect at 180, which is on the pitch line 102A, and at 181.
  • the line 102B represents the trajectories of the maximum overlapping points, such as 183 and 186, and is identified as base line of gear 74B.
  • the line 100B which is drawn in a similar manner, is identified as base line of gear 74A.
  • An involute or similar curve 77C1 that forms a side of a tooth in gear 74A starts at point 184 (which is not on circle 77A) on line 100B, and intersects with line 100A at point 182, which is on circle 77A.
  • an involute or similar curve 79C1 that forms a side of a tooth in gear 74B starts at point 187 in the inserted enlarged view (which is not on circle 79A) on line 102B, and intersects with line 102A at 180, which is on circle 79A.
  • Lines 77C1 and 79C1 contact each other at 183A.
  • 77C1 and 79C1 each may comprise two or more curve segments of different mathematical characteristics.
  • the involute or similar curve 77C1 is terminated at an arbitrary point 183B which is on or within circle 77A.
  • the involute or similar curve 79C1 is terminated at an arbitrary point 180B which is on or within circle 79A.
  • the points of termination 180B and 183B of the involute or similar curves 77C1 and 79C1 are the boundaries of the side and the top segments of gear teeth. Geometries of the curves 77C1 and 79C1 are selected to satisfy the condition such that curves 77C1 and 79C1 will generally in contact to each other while they travel the distance of a full gear tooth width (i.e., 201 to 200A in Fig. 14).
  • the gear teeth in the completed gear design are shown in Fig. 15 of the drawings.
  • Surface of gear tooth 77 of gear 74A comprises two sides 77C1 and 77C2 and top 77C3, and surface of gear tooth 79 of gear 74B comprises two sides 79C1 and 79C2, and top 79C3.
  • the top surface 77C3 of gear tooth 77A is within circle 77A
  • the top surface 79C3 of gear tooth 79A is within circle 79A in Fig. 14.
  • a gap between neighboring gear teeth 77 is shown as 77D
  • a gap between neighboring gear teeth 79 is shown as 79D.
  • the boundary between a gear tooth side 79C1 and gap 79D is shown by point 187 in the inserted enlarged view.
  • the curves forming gaps 77D and 79D are arbitrary curves that do not cause interference of gear teeth.
  • Fig. 16 of the drawings shows a modified gear tooth design wherein the involute or similar curve 77C1 shown in Fig. 15 is replaced by a circular arc 77F1, and the involute or similar curve 77C2 is replaced by another circular arc 77F2.
  • the geometric designs of the corresponding gear tooth arcs 79C1-2 and 79C2-2 must be adjusted to accommodate the circular geometries of gear tooth arcs 77F1 and 77F2. This is the basis for an alternative gear set design, in which one of the gears will have rollers instead of teeth.
  • Figs. 17 and 18 of the drawings wherein an alternative gear set 120 comprising a modified form of the type 1 gear 120A and corresponding type 2 gear 120B is shown, which gear set may be used in place of gear sets 74 and 76.
  • the type 1 gear 120A is shown affixed to tubular shaft 82, which, in turn, is rotatably supported on shaft 86, rotatable about shaft axis 88, in the manner of gear set 74 shown in Fig. 12.
  • type 2 gear 120B is shown attached to shaft 68 rotatable about axis 90.
  • the type 1 gear 120A uses rollers and the type 2 gear 120B uses a nonroller gear tooth design. Rollers 132A of the type 1 gear mesh only with gear teeth 124A of the type 2 gear and rollers 132B mesh only with gear teeth 124B.
  • gears 120A and 120B are split into two one-sided gears, each gear having teeth for meshing only on one side. That is, each gear's teeth of the two one-sided gears are angularly offset so that the two one-sided gears mesh only on one side to function as one gear set.
  • type 1 gear 120A comprises one-sided gears 120AA and 120AB with rollers 132A and 132B sandwiched between walls 128.
  • Gear teeth in the form of rollers 132A and 132B are located on the periphery of the gear and are rotatably supported on axles 134A and 134B extending between the gear walls 128.
  • the type 2 gear 120B comprises one-sided gears 120BA and 120BB with gear teeth 124A and 124B attached with connecting piece 126.
  • Rollers 132A and 132B are adapted for engagement with teeth 124A and 124B, respectively, formed about the periphery of the type 2 gear.
  • Gear tooth 132A of type 1 one-sided gear 120AA and gear tooth 124A of type 2 one-sided gear 120BA, and gear tooth 132B of type 1 one-sided gear 120AB and gear tooth 124B of one-sided gear 120BB continuously contact each other while they travel one full gear tooth width in the vicinity of the contact point.
  • Gear sets that include a combination of nonroller gear teeth and roller types of teeth may be used.
  • the circular arc sections of gears 120A and 120B may be provided with nonroller gear teeth in place of the illustrated roller types of teeth 132A and 132B on gear 120A and associated teeth 124A and 124B on gear 120B.
  • Fig. 19 of the drawings comprising type 1 gears 74A and 76A, each having gear segments A1 , A2, A3, and A4 and type 2 gears 74B and 76B, each having gear segments B1 , B2, B3, and B4, wherein segment A1 meshes with B1 , A2 with B2, A3 with B3, and A4 with B4.
  • the four segments in type 1 gear 74A and 76A are defined in such a manner that at the boundary of A1 and A2, denoted by 1P in Fig.
  • x-axis is the rotational angle of the type 2 gears 74B and 76B
  • the y-axis is the rotational speeds of the type 1 and type 2 gears.
  • the rotational angle of gears 74B and 76B is zero when gear set 74 is meshing at 1 P, and gear set 76 is meshing at 2P.
  • Type 1 and type 2 gears are not necessarily symmetric to A-A and B-B. It must satisfy, however, in addition to the condition given in Equation (1), the angle traveled by the type 1 gear in A1 equals the angle traveled by the type 1 gear in A4, and the angle traveled by the type 1 gear in A2 equals the angle traveled by type 1 gear in A3, both under constant speed operation of the type 2 gear.
  • a type 1 gear that causes speed profiles A1-S1 , A2-S, A3-S1 , and S4-S shown in dotted line in Fig. 20 satisfying the above conditions is a valid design.
  • Figs. 21 and 7 Operation of the novel engine of this invention will best be understood with reference also to Figs. 21 and 7. Reference first is made to Fig. 21 wherein sequential operating positions of the engine pistons and gear sets 74 and 76 at four time points T1 through T4 are schematically illustrated, and functions at the four engine subchambers are identified. Each subchamber is identified by the leading and trailing pistons of the subchamber.
  • fuel is injected during the compression phase.
  • fuel may be injected at the end of the compression phase.
  • a fuel/air mixture may be supplied to the engine through the inlet port, in which case no fuel injection means are required.
  • Fig. 21 shows the angular positions of the piston assemblies 30 and 32 and gear sets 74 and 76 of a four-piston engine during almost one revolution of the piston assemblies. Since the gear sets 74 and 76 are connected to the piston assemblies through circular gear pairs 70 and 72 having a 1 :2 gear ratio, in the four-piston design the type 1 gears 74A and 76A and type 2 gears 74B and 76B complete two revolutions for each revolution of the piston assemblies, output shaft 86 also completes two revolutions for each revolution of the piston assemblies.
  • pistons 30A and 32A are at their closest positions and subchamber 30A-32A is at its minimum volume; ignition has already taken place in subchamber 30A-32A.
  • the exhaust of spent gases starts through the exhaust port at subchamber 32B-30A.
  • the power and exhaust phases occurring at the respective subchambers 30A-32A and 32B-30A continue from time point T1 through time point T4 of the engine cycle in Fig. 21.
  • Fuel is injected into subchamber 32A-30B at some point in piston travel.
  • the exhaust port may be cut wider than the piston width to allow for the exhaust of spent gases before time point T1. Spark ignition timing may be advanced or delayed as required.
  • gear sets 74 and 76 are both rotating at the same speed.
  • Fig. 7 a diagram showing the rotational speed profiles of gears 74A and 76A and interconnected gears 74B and 76B.
  • the rotational speeds of type 1 gears 74A and 76A are identified by reference characters 74A-S and 76A-S, respectively
  • the rotational speeds of type 2 gears 74B and 76B are identified by reference characters 74B-S and 76B-S, respectively.
  • times T1 to T4 are shown, which correspond to times T1 to T4 in Fig. 21. As seen in Fig.
  • both gear sets 74 and 76 have reached constant rotational speed and have been rotating at those constant speeds for a while.
  • Type 1 gears 74A and 76A are rotating at speed Wmax and Wmin, respectively, at time T3 shown in Fig. 7.
  • the rotational speed 74A-S of type 1 gear 74A decreases, and simultaneously, the rotational speed 76A-S of type 1 gear 76A increases between times T3 and T4.
  • ignition takes place in subchamber 32A-30B, in preparation for the next cycle.
  • FIG. 22 of the drawings wherein an alternative design of engine 200 is shown to include a stationary engine housing 259 having a toroidal working chamber within.
  • the engine housing 259 comprises housing walls 259A and 259B, attached by means such as bolts, not shown.
  • the piston assemblies 230 and 232 in this embodiment of the invention are practically of the same design described earlier and shown in Fig. 2 except that the piston hubs of this embodiment are smaller than that described in Fig. 2.
  • Piston assembly 230 includes a pair of diametrically opposed pistons 230A, 230B, and piston hub 230C.
  • Piston assembly 232 includes a pair of diametrically opposed pistons 232A, 232B, and piston assembly 232C.
  • Pistons 230A and 230B are affixed to outer piston shaft 36 through piston hub 230C.
  • An inner piston shaft 38 is rotatably mounted on the tubular shaft 36.
  • Pistons 232A and 232B of second piston assembly 232 are attached to inner piston shaft 38 through piston hub 232C at diametrically opposite positions.
  • Piston assemblies 230 and 232 are rotatable about a common axis 40.
  • the working chamber is divided into two pairs of diametrically opposed subchambers by four pistons 230A, 230B, 232A, and 232B in a four-piston engine as shown in Fig. 22.
  • Each piston assembly alternately rotates at a faster and slower speed such that trailing pistons rotate at a slower speed than leading pistons during the power and intake phases of engine operation, and periodically variable volume subchambers are provided between adjacent pistons.
  • FIG. 23of the drawings showing a cross-sectional view of the engine's working chamber with an enlarged view of a spark plug 214 installed within piston 232A.
  • a spark plug 214 is embedded inside a hole 264 drilled in each piston (a spark plug embedded in 232A is shown in solid line and a spark plug embedded in 232B is shown in dotted line) between piston rings 252; through this hole, the spark plug 214 can be accessed.
  • a hole 211 is bored in the middle of one side of the piston surface through which the spark plugs' electrodes with spark gaps 210 communicate with a subchamber.
  • Spark plug 214 is plugged to spark plug socket 216 made of a nonconductive material and equipped with power terminals 216B from which an electric wire is extended to the power source, not shown. Spark plug 214 is secured in its place by a screw 218. Spark plug hole 264, in which the spark plug case 216 is embedded is closed off by a lid 260 with bolts 261. The engine housing wall 259A has a spark plug maintenance hole 285 for accessing the spark plugs 214, which is closed off by a lid 258A with bolts 263. The spark plug cases and spark plugs attached to pistons 232A and 232B are accessible from opening 285 on the engine housing wall 259A whenever necessary.
  • a spark plug is provided for each of the subchambers into which the working chamber is divided by the pistons.
  • a spark plug 214 and its peripheral parts that are housed in piston 232B are shown in dotted line.
  • spark plugs (not shown) embedded in pistons 230A and 230B are accessible through a spark plug maintenance hole 286 which is closed off by a lid 286A under normal operation.
  • Sealing of subchambers to prevent the flow of gases therebetween is provided by any suitable means, including for example, semicircular piston rings 252 along the outer convex surfaces of pistons 232A and 232B.
  • Circular seal means 247 and 248 are placed along the crevices between each of the pistons and the inner surface of engine housing wall for sealing engagement.
  • a circular seal means 246 is placed along the crevices between the pistons at the inner wall of the engine housing 259 for sealing engagement between the two pistons.
  • Ball bearings 225 are placed between piston assemblies 230 and 232, and between piston assembly 230 and the engine housing 259 for secure but rotatable mounting of the piston assemblies.
  • the engine housing 259 is equipped with a water jacket 280; the pump that pumps cooling water into the water jacket is not shown.
  • Fig. 24 of the drawings wherein schematic representation of alternative gear sets 274 and 276 (with no gear teeth) are shown.
  • Identically shaped gear sets 274 and 276, which are positioned 90 degrees off-phase of each other just like piston assemblies 30 and 32 do in Fig. 1 are used in place of gear sets 74 and 76 shown in Fig. 1 , respectively.
  • circular gear pairs 70 and 72 in Fig. 1 will become 1 :1 gear ratio whereby gears 70B and 72B undergo one complete revolution for each complete revolution of piston shafts 36 and 38, respectively, and gears 274A and 276B undergo one complete revolution for each complete revolution of the pistons.
  • gear ratio of gear pair 80 in Fig. 1 will become 1 :2 regardless of the number of pistons in the engine, whereby gear 80B undergoes two complete revolutions for each complete revolution of gear 80A.
  • gear ratio of gear pairs 70 and 72 in Fig. 1 will become 1:2 gear ratio, whereby gears 70B and 72B undergo two complete revolutions for each complete revolution of piston shafts 36 and 38, respectively, and gears 274A and 276A undergo two complete revolution for each complete revolution of the pistons.
  • Noncircular gears 274A consists of two circular arc segments 322 and 322A with central angle Q13; two circular arc segments 320 and 326 with central angle Q14; and four non-circular arc segments 321 , 324, 321 A, and 324A with central angle (Q1)/2.
  • Noncircular gear 276A consists of two circular arc segments 300 and 307 with central angle Q13; two circular arc segments 301 and 301 A with central angle Q14; and four non-circular arc segments 305, 306, 305A, and 306A with central angle (Q1)/2.
  • Noncircular gear 274B consists of two circular segments 318 and 319 with central angle Q2, and two non-circular arc segments 328 and 330 with central angle Q1.
  • Noncircular gear 276B consists of two circular segments 302 and 304 with central angle Q2, and two non-circular arc segments 309 and 311 with central angle Q1.
  • gears 274A and 276A rotate in the direction of arrow 94
  • gears 274B and 276B rotate in the direction of arrow 96.
  • gears 78A and 78B are connected to gears 274A and 276A, respectively, and gear 80B that meshes with ⁇ OA at the ratio of 2:1; i.e., gear ⁇ OB undergoes two complete revolutions for each complete revolution of gear 80A, is connected to gears 274B and 276B, the relationship given in (1) is rewritten as
  • W0 rotational speed of gears 274B and 276B
  • W3 rotational speed of gear 274A
  • W4 rotational speed of gear 276A.
  • the speed profile of type 3 gears shows the way the speed of type 3 gears 274A and 276A vary as they rotate relative to the rotational angle of type 4 gears 274B and 276B, wherein type 4 gears 274B and 276B keep a constant rotational speed WO.
  • the horizontal axis (Q) indicates the rotational angle of type 4 gears 274B and 276B in radian
  • the vertical axis (W) indicates the rotational speed of type 3 gears 274A and 276A and type 4 gears 274B and 276B.
  • type 3 gear 274A The rotational speed of type 3 gear 274A is represented by 274A-S, that of type 3 gear 276A by 276A-S, that of type 4 gear 274B is represented by 274B -S, and that of type 4 gear 276B by 276B-S.
  • the positions of type 3 and type 4 gears corresponding to the gear operation at time point 0 in Fig. 25 are given in Fig. 26.
  • the type 3 gear 274A meshes with the type 4 gear at 370
  • the type 3 gear 276A meshes with the type 4 gear 276B at 371.
  • type 3 gear 274A is at point 370 which is at the end of circular segment 319 (Fig. 26), ready to increase its rotational speed
  • type 3 gear 276A is at point 371 which is at the end of circular segment 300 (Fig. 26) ready to decrease its rotational speed.
  • Type 3 gear 274A rotates at maximum speed, Wmax
  • Type 3 gear 274A rotates at minimum rotational speed, Wmin
  • Rotational angle of type 3 gears 274A and 276A in noncircular segments (321 , 324, 305 and 306 in Fig. 26) is (Q1)/2
  • rotational angle of type 4 gears 274B and 274B in noncircular segments (328, 330, 309 and 311) is Q1.
  • the rotational angle of type 3 gears 274A and 276A in circular segments (322, 300, 307) in which those gears operate at maximum speed is Q13
  • the rotational angle of type 3 gears 274A and 276A in circular segments (320, 326, 301) in which those gears operate at minimum speed is Q14.
  • Fig. 27 of the drawings wherein geometries of noncircular gear set 276 (with no gear teeth) are depicted in detail.
  • the geometries of type 3 and type 4 gears 276A and 276B are determined by the maximum and minimum rotational speeds of type 3 gear 276A relative to the rotational speed of type 4 gear 276B, the angle traveled by type 4 gear 276B while type 3 gear 276A is traveling at these extreme rotational speeds, and the speed profile of type 3 gear relative to the rotational speed of type 4 gear 276B between the two extreme rotational speeds.
  • Y3 radius of circular arc segment 300 of type 3 gear 276A in which the type 3 gear operates at maximum speed
  • Y4 radius of circular arc segment 301 of type 3 gear 276A in which the type 3 gear operates at minimum speed
  • X3 radius of circular arc segment 302 of type 4 gear 276B in which it meshes with the type 3 gear operating at maximum speed
  • X4 radius of circular arc segment 304 of type 4 gear 276B in which it meshes with the type 3 gear operating at a minimum speed
  • D distance between the centers of the rotational axes of the type 3 and type 4 gears.
  • gamma can take any value between 0 and 1.
  • Patent Numbers 4,003,681 and 4,028,019 is a special case of the Wildhaber-Sakita gear set, wherein the central angles of circular segments of type 3 and type 4 gears are all zero, and the speed profile of the type 3 gears follow a sinusoidal curve.
  • Q0 (305B) is the angle created by the type 3 gear's apex, the rotational center of the gear, and its point of contact with the type 4 gear at which point the speeds of the type 3 and type 4 gears all become equal; Q0 also is half the angle the type 3 gear travels in the nonactive phase. In the four-piston design, Q0 (305B) equals the sum of the thickness of a piston and the gap created by the two pistons when they are closest to each other.
  • W0 Rotational speed of the type 4 gear (276B-S in Fig. 25)
  • W Rotational speed of the type 3 gear (276A-S in Fig. 25)
  • Equation (18) D is the distance between the rotational centers of the type 3 and 4 gears.
  • the rotational speed of the type 3 gear 276A in the noncircular segment that starts at the end of the circular segment with smaller radius (end of rotational speed Wmax) and ends at the beginning of a circular segment with lareger radius (start of rotational speed Wmin) is expressed as:
  • Equation (19) reads W equals (W0)/2 plus [(W0)/2 - Wmin] multiplied by cosine [Q multiplied by (pi) divided by Q1].
  • gamma (WO - 2Wmin)/W0, then from Equations (18) and (19), we have
  • Equation (22) is rewritten as:
  • Fig. 28 of the drawings wherein sample type 3 and type 4 gear designs 274A-A and 274B-A, respectively, are shown.
  • the type 3 gear 274A-A has an eye-shaped body with round apexes, and the corresponding type 4 gear 274B-A has a heart-shaped body with a round shallow cusp.
  • the type 3 gear is formed with two noncircular segments, in each of which the radius (or the distance between the center of rotation to the contact point with the other gear) changes from 0.54D to 0.87D.
  • the type 4 gear is formed with two noncircular arc segments, in each of which the radius (or the distance between the center of rotation to the contact point with the other gear) changes from 0.46D to 0.13D.
  • the physical geometries of the type 3 and type 4 gears also change.
  • Type 3 and type 4 gears with gamma 1.0 are eye and heart shaped with sharp apexes in the type 3 gear and a sharply cut cusp in the type 4 gear.
  • Figs. 29A through 29D of the drawings show, using mathematical notations and commonly used Greek letters for some variables and constants, aforementioned Equations (1) through (24).
  • the shape of the piston surface may be made rectangular or square instead of circular as described in the present invention, and the shape of the working chamber may be cylindrical instead of toroidal.
  • the engine described in this invention may be also used in diesel engines.
  • Number of pistons attached to a piston assembly may not be limited to four or eight: As many pistons as practicable may be attached to a piston assembly as long as gear set 70 and 72 shown in Fig. 1 is adjusted to a proper rotation ratio, and the number of pistons attached to a piston assembly is a multiple of four.
  • the use of the specified gear teeth is not required for operation of the engine. It is intended that the above and other such changes and modifications shall fall within the spirit and scope of the invention defined in the appended claims.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

L'invention concerne un moteur à pistons rotatifs (20) comportant un logement (22), une chambre de travail toroïdale équipée de ports d'entrée et de ports d'évacuation (56,54), et des premiers et seconds ensembles de pistons (30,32) dotés d'au moins une paire de pistons diamétralement opposés (30A, 30B, 32A, 32B) et situés dans la chambre de travail. Les ensembles de pistons (30, 32) sont reliés à un axe de sortie grâce à un différentiel (78), un pignon 1 de type Sakita (74A ou 76A) et un pignon 2 de type Sakita (74B ou 76B). Ces ensembles de pistons (30 et 32) tournent à une vitesse variable, si bien que les pistons fonctionnant à une vitesse inférieure les talonnent à certains moments des phases de puissance et d'entrée lors du fonctionnement du moteur. Le pignon 1 de type Sakita comprend des dents sous forme de cylindres et de bougies d'allumage incrustés dans les ensembles de pistons (30 et 32) et sont accessibles depuis l'extérieur.
PCT/US2002/019112 2001-07-20 2002-06-15 Moteur a pistons rotatifs WO2003008781A1 (fr)

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US09/910,545 US6457451B1 (en) 2001-07-03 2001-07-20 Rotary piston engine
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10273661B2 (en) 2016-08-05 2019-04-30 Woodward, Inc. Multi-chamber rotary piston actuator
US10563677B2 (en) 2016-12-21 2020-02-18 Woodward, Inc. Butterfly rotary piston type actuator
EP3747925A1 (fr) 2019-06-07 2020-12-09 Henkel AG & Co. KGaA Composition durcissable par rayonnement par polymérisation anionique
US10954973B2 (en) 2017-07-14 2021-03-23 Woodward, Inc. Unsupported piston with moving seal carrier

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Publication number Priority date Publication date Assignee Title
US3990405A (en) * 1975-01-16 1976-11-09 Joseph Kecik Rotary internal combustion engine
US4026249A (en) * 1973-03-14 1977-05-31 Carlos Ayesta Larrea Rotary cycloidal continuous toroidal chamber internal combustion engine
US4057374A (en) * 1976-09-02 1977-11-08 Seybold Frederick W Rotary internal combustion engine with uniformly rotating pistons cooperating with reaction elements having a varying speed of rotation and oscillating motion
US5192201A (en) * 1990-10-15 1993-03-09 Jacek Beben Rotary engine and drive coupling
JPH062559A (ja) * 1992-06-15 1994-01-11 Tadao Akimoto ロータリエンジン
US5381766A (en) * 1993-11-05 1995-01-17 Sakita; Masami Rotary piston engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4026249A (en) * 1973-03-14 1977-05-31 Carlos Ayesta Larrea Rotary cycloidal continuous toroidal chamber internal combustion engine
US3990405A (en) * 1975-01-16 1976-11-09 Joseph Kecik Rotary internal combustion engine
US4057374A (en) * 1976-09-02 1977-11-08 Seybold Frederick W Rotary internal combustion engine with uniformly rotating pistons cooperating with reaction elements having a varying speed of rotation and oscillating motion
US5192201A (en) * 1990-10-15 1993-03-09 Jacek Beben Rotary engine and drive coupling
JPH062559A (ja) * 1992-06-15 1994-01-11 Tadao Akimoto ロータリエンジン
US5381766A (en) * 1993-11-05 1995-01-17 Sakita; Masami Rotary piston engine

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10273661B2 (en) 2016-08-05 2019-04-30 Woodward, Inc. Multi-chamber rotary piston actuator
US10655303B2 (en) 2016-08-05 2020-05-19 Woodward, Inc. Multi-axis rotary piston actuator
US10883522B2 (en) 2016-08-05 2021-01-05 Woodward. Inc. Multi-chamber rotary piston actuator
US11280356B2 (en) 2016-08-05 2022-03-22 Woodward, Inc. Multi-axis rotary piston actuator
US11391305B2 (en) 2016-08-05 2022-07-19 Woodward, Inc. Multi-chamber rotary piston actuator
US12012976B2 (en) 2016-08-05 2024-06-18 Woodward, Inc. Multi-axis rotary piston actuator
US10563677B2 (en) 2016-12-21 2020-02-18 Woodward, Inc. Butterfly rotary piston type actuator
US10935054B2 (en) 2016-12-21 2021-03-02 Woodward, Inc. Butterfly rotary piston type actuator
US10954973B2 (en) 2017-07-14 2021-03-23 Woodward, Inc. Unsupported piston with moving seal carrier
US11512719B2 (en) 2017-07-14 2022-11-29 Woodward, Inc. Unsupported piston with moving seal carrier
EP3747925A1 (fr) 2019-06-07 2020-12-09 Henkel AG & Co. KGaA Composition durcissable par rayonnement par polymérisation anionique
WO2020244992A1 (fr) 2019-06-07 2020-12-10 Henkel Ag & Co. Kgaa Composition durcissable par rayonnement par polymérisation anionique

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