US3636930A - Rotary engine - Google Patents

Rotary engine Download PDF

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Publication number
US3636930A
US3636930A US8247A US3636930DA US3636930A US 3636930 A US3636930 A US 3636930A US 8247 A US8247 A US 8247A US 3636930D A US3636930D A US 3636930DA US 3636930 A US3636930 A US 3636930A
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Prior art keywords
cylinder
pistons
shaped
engine
equal
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Expired - Lifetime
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US8247A
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Fukumatsu Okada
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    • 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
    • F01C1/36—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 both the movements defined in sub-groups F01C1/22 and F01C1/24

Definitions

  • the present invention relates to a rotary engine in which the cylinder is ring shaped and is constructed by an elliptical outer circumferential wall, a leaf-shaped inner circumferential wall, a front wall and rear wall. and the cross section of said cylinder is rectangular and becomes larger at first, smaller next, then larger and smaller at last along the cylinder circumference. lnto said ring-shaped cylinder several leaf-shaped pistons are inserted airtightly at equal intervals and the engine has a device to revolve said pistons around the center of said cylinder maintaining their attitudes always in horizontal state. Further the engine has, in the outside ofcylinder, the device of connecting the engine output shaft and the piston axes which are fixed to the pistons, whereby the force of explosion gas which acts on the pistons is transmitted smoothly to the output shaft of engine.
  • the present invention relates to a rotary engine which is an internal combustion engine using gasoline and the like, and in volves pistons and a cylinder which have special constructions and functions.
  • the primary object of this invention is to provide a rotary engine which does not involve the above-mentioned defects as seen in the conventional internal combustion engine and makes all of its moving parts engaged in circular motion.
  • the second object of this invention is to provide a rotary engine which lowers the engine vibration and raises the combustion efficiency as much as possible during engine operation.
  • the third object of this invention is to provide a rotary engine in which the suction of mixed gas and the discharge of combustion gas are conducted smoothly.
  • the fourth object of this invention is to provide a rotary engine which improves the airtightness of combustion chamber, revolves the pistons smoothly in the cylinder around the cylinder center and lowers the friction between the pistons and the cylinder during engine operation.
  • the last object of this invention is to provide a rotary engine which makes smooth the mutual action between its pistons and output shaft and consequently the revolution of output shaft.
  • FIGS. I-Il show the principle of this invention and a process of producing this rotary engine
  • FIG. 13 is a front view of this engine in which front portion of the engine is removed to show the inner part of this engine;
  • FIGS. I I and I show mainly the perspective views of piston
  • FIG. I6 is a front view of this engine in which some front portion of the engine is removed;
  • FIG. I7 shows mainly a radial lever of the engine which is fixed to engine output shaft
  • FIG. I8 shows a front view of this engine
  • FIG. I9 is a sectional view of the portion defined by a one point dotted line in FIG. I8.
  • arcs 34 to which chords 35 correspond, are taken to divide a circle 33 in FIG. I which has a predetermined radius into several equal parts (in this example a circle is divided into eight equal parts).
  • FIG. 2 shows that a circle 37, the center of which is 36, has an equal radius to that of said circle 33 of FIG. I which is divided into eight equal parts, and a circle 39, the center of which is 33 and which has an equal radius to that of said circle 37, is apart from the circle 37 by the distance of chord 35 shown in FIG. I.
  • Arc II has its center at the point III which is one of the intersection points of circles 37 and 39 and its radius is equal to the diameter of circle 37.
  • the arc II touches the circles 37 and 39 at the points of tangency I I and d5 respectively.
  • are 43 has its center at the point I2 which is the other intersection point of circles 37 and 39 and its radius is equal to the diameter of circle 3' and it touches the circles 37 and 39 at the points of tangency d7 and do respectively.
  • an elliptical outer circumferential wall is made by the arc II between the two contact points lli and d5, the arc portion of circle 39 between two contact points did and as, the are 43 between the two contact points as and Q7 and the arc portion of circle 37 between two contact points d7 and d ll.
  • a leaf-shaped inner circumferential wall is made by two are portions between the intersection points It) and M of the two circles 37 and 39.
  • Inner wall of the ringshaped cylinder is made by the inner surface of said elliptical outer circumferential wall and the outer surface of said leaf shaped inner circumferential wall.
  • points 30 divided the circumference of a circle I9 into eight equal arcs, said circle I9 having an equal radius to that of circle 37 of FIG. 2 and its center M3 at the middle point of the distance SI of FIG. 4i between the center 36 of circle 37 and the center 33 of circle 39.
  • any line parallel with the segment of line SI will be called a horizontal line.
  • a leaf-shaped body 55 in section is formed by two oppositely facing arcs 53, said arc 53 being the same with that which is cut off as a horizontal segment of line 52 from the circle I9.
  • These eight leaf-shaped bodies 55 are called pistons of this engine, which revolve in the ringshaped cylinder maintaining always equal intervals between themselves and their horizontal attitudes.
  • Inlets 56 are provided on the portion of ring-shaped cylinder where the cross section of said cylinder becomes larger at first, ignition plugs 57 are installed on the cylinder portion where the cross section of said cylinder becomes smaller at first and outlets 58 are provided on the cylinder portion where the cross section of said cylinder becomes smaller at last.
  • pistons move in said cylinder keeping both of their ends in touch with the inner surfaces of said cylinder when they are between two contact points 45 and 46 and between two contact points l7 and 44 during their revolution around the center of said cylinder.
  • the pistons have a portion of one of their arcs and a portion of the other are contact the opposite inner surfaces of said cylinder when they are moving between two contact points MI and I5 and between two contact points sin and 37.
  • the inner space of said ring-shaped cylinder is divided into eight airtight chambers by the eight pistons and said eight airtight chambers revolve around the center of said cylinder.
  • each airtight chamber changes as the chamber revolves around the center of said cylinder, for example, an airtight chamber moves from position I in FIG. 7 to position 5 in FIG. 7 in said cylinder through position 2 in FIG. Ill, position 3 in FIG. 9 and position t in FIG. III. Then the chamber moves from position 5 in FIG. 7 to position b in FIG. 3 and finally returns to position I in FIG. 7 through position 32 in FIG. III and after that this motion is repeated.
  • the volume of an airtight chamber becomes smaller as the cross-sectional area of said cylinder becomes smaller and becomes larger as that cross-sectional area becomes larger during one complete revolution of the airtight chamber in said ring-shaped cylinder. Consequently the volume of an airtight chamber becomes larger at first, smaller next, then larger and smaller at last during one complete revolution of pistons in said cylinder.
  • the gas mixture is sucked through inlets st of FIG. 6 into the airtight chamber which is located at the position from I to 8 in the cylinder 63 (see FIG. I3), compressed in the airtight chamber at the position from 9 to I7 in FIG. 7, ignited at the position 17, expands in the airtight chamber at the position from 17 to 25 of FIG. 7 and is discharged, through outlets 58 (see FIGS. 6 and 13), from the airtight chamber at the position from 26 (FIG. 8) to 32 (FIG.
  • This engine conducts the above-described strokes continuously as pistons revolve in the ring-shaped cylinder around the center thereof.
  • this engine is a rotary engine which has a special cylinder and pistons.
  • a circle 59 which will hereinafter be called a fixed circle has an appropriate radius and is surrounded by eight smaller circles of equal diameters provided at equal intervals, which will hereinafter be called secondary circles 60.
  • Eight circles, which will hereinafter be called third circles 61, have the same radius with that of fixed circle 59 and touch the respective secondary circles 60 at the outside thereof and their centers are located respectively on eight radial lines passing the center of fixed circle 59 and the centers of eight secondary circles 60.
  • the fixed gear is fixed at the center of inner front wall of said ring-shaped cylinder and the driven gears, which are attached rotatably to the arms of radial lever 62 respectively, revolve around the fixed gear through the intermediate gears, which are also attached rotatably to the arms of the radial lever 62 respectively, when said radial lever 62 rotates with engine output shaft.
  • each driven gear rotates oppositely against the direction of the rotation of radial lever 62 and its number of rotation is equal to that of radial lever 62. Consequently the horizontal line marked on each driven gear 69 shown in FIG. 16 remains horizontal, and each piston revolves maintaining its horizontal attitude in the ring-shaped cylinder because each shaft 78 (FIG. 16) to which each piston axis 68 (see FIG. 14) is connected in alignment with it holds said driven gear 69 (see FIG. 14) on it.
  • the ring-shaped cylinder 63 is comprised of an elliptical outer circumferential wall, a leaf-shaped inner circumferential wall, a front wall and a rear wall 64; the cross section of said cylinder 63 is rectangular and a hole 66 for mounting the output shaft of the engine is opened at the center of rear wall 64.
  • inlets 56, (FIG. 13), ignition plug 57 (FIG. 13) and outlets 58 (FIG. 13) are provided on the cylinder portion at which the sectional area of the cylinder becomes larger at first, smaller next and smaller at last respectively.
  • the pistons 67 which are inserted airtightly into the said cylinder 63 at equal intervals are formed like leaves in section by two oppositely facing arcs and have same breadth with that of the chamber of the said cylinder 63.
  • Eight piston axes 68 and 78, which are fixed to eight pistons respectively, are rotatably mounted respectively in the eight holes made at equal intervals on a rotational ring 70 and fixed to the axes 78 of driven gears 69 in alignment therewith.
  • a circular inner front wall 71 holds pistons 67 in the ringshaped cylinder 63 and closes the said cylinder at the inside of rotational ring 70, and has a hole 73, through which the output shaft 65 is rotatably mounted, and mounts a fixed gear 72 having the same number of teeth as driven gears 69 at the boss of its center portion.
  • the elliptical outer front wall 74 closes the said cylinder at the outside of rotational ring 70 which is inserted airtightly and rotatably into the slit between the inner and outer front walls.
  • the output shaft 65 which is rotatably mounted in the hole 70 of inner front wall 71 and the hole 66 of rear wall 64, holds a radial lever 62 (FIG. 12) at the outside of said cylinder, which carries eight arms 75 radially extending from its center portion at equal angles.
  • Each arm 75 mounts rotatably an intermediate gear 76 at its middle portion and has a hole 77, in which axis 78 of a driven gear 69 is rotatably mounted, at its end portion.
  • Each driven gear 69 rotates oppositely against the fixed gear 72 with the aid of intermediate gear 76.
  • each piston 55 (FIG. 6) always holds its horizontal attitude in the ring-shaped cylinder 63 with the help of fixed gear 72, intermediate gear 76 and driven gear 69 when it revolves around the center of said cylinder 63.
  • the inner space of said cylinder 63 is divided into eight airtight chambers and the airtightness of the chambers is never lost during engine operation.
  • the volume of each airtight chamber becomes larger at first, smaller next, then larger and smaller at last as it completes one revolution.
  • Each airtight chamber sucks mixed gas into it through inlet 56 when it grows larger at the first step, then compresses the gas in it when it becomes smaller at the second step, then the gas expands strongly by combustion when said chamber becomes larger at the third step and the exhaust gas is discharged from said chamber through outlets 58 when the chamber becomes smaller at the last step.
  • a stroke of suction, compression, ignition, expansion and discharge of mixed gas is repeated continuously and smoothly and an even torque is generated by the transmission of force acting on each piston to the output shaft of engine through piston axis fixed to the piston and radial lever fixed to output shaft.
  • a rotary engine comprising an elliptically symmetrically ring-shaped cylinder having at least one suction inlet, exhaust outlets and ignition plug; a plurality of pistons which revolve around the center of said cylinder holding their attitude in parallel relation in said cylinder and a device outside of said cylinder which holds said pistons in parallel relation and transmits the force acting on the pistons to output shaft mounted in the center of said cylinder at the outside thereof;
  • said ring-shaped cylinder is comprised of an elliptical outer circumferential wall with a given breadth; a leaf-shaped inner circumferential wall cross-sectionally shaped as opposing intersection segmental arcs of equal radius coaxial with, and having the same breadth as said outer circumferential wall; a front wall and a rear wall parallel with each other and perpendicular to the axis of rotation, the cross section of said cylinder in the plane of rotation being rectangular and its sectional area increases at first, decreases next, then increases, then decreases along the cylinder circumference during a 360 revolution;
  • each of said pistons having a foillike cross section formed by two oppositely facing arcs; said arcs being of the same radius as the radius locating the axis of rotation of said pistons; the thickness of said piston being equal to half of the difference between the narrowest width between the inner faces of said elliptical outer circumferential wall of said cylinder and the largest dimension across the high points of the said leaf-shaped inner circumferential wall; whereby said pistons are capable of a regular circular movement around said shaft of said engine, while maintaining their parallel position in relation to each other and their sliding contact clearance with the inner surfaces of said cylinder.
  • a rotary engine as claimed in claim ll wherein a fixed gear is fixedly exteriorly mounted to said inner front wall of said cylinder, said piston axes which are rotatably mounted in said rotational ring and on the end portion of arms of said radi al lever respectively.
  • said driven gears fixedly mounted on said axis having the same number of teeth as said fixed gear and intermediate gears are mounted rotatably on the arms of said radial lever between the fixed gear and the driven gears, and engage with both the fixed gear and the driven gears, whereby the pistons are held in a parallel position in relation to each other during their revolution in said cylinder, said fixed gear, said intermediate gears and said driven gears forming a planetary gear system.
  • outer circumferential wall forms an elliptical contour which is composed by two arcs of two intersecting circles of same radius and two arcs which touch the two arcs of said two circles and has a radius equal to the diameter of said circles, and the centers of which coincide with the intersection points of said two circles.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
US8247A 1969-03-28 1970-02-03 Rotary engine Expired - Lifetime US3636930A (en)

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JP2361069A JPS5618772B1 (enrdf_load_stackoverflow) 1969-03-28 1969-03-28

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Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3885531A (en) * 1973-06-29 1975-05-27 Raymond Lee Organization Inc Rotary internal combustion engine
US4055156A (en) * 1976-03-12 1977-10-25 Gundlach, S.A. Rotary engine
EP0379832A1 (de) * 1989-01-24 1990-08-01 André Feyereisen Verbrennungsmotor
US5156541A (en) * 1991-05-07 1992-10-20 Lew Hyok S Revolving vane pump-motor-meter with a toroidal working chamber
WO1994027031A1 (en) * 1993-05-13 1994-11-24 Brent Charles R Rotary vane mechanical power system
US5819699A (en) * 1997-05-13 1998-10-13 Burns; William A. Rotary internal combustion engine
US20040011320A1 (en) * 2002-07-16 2004-01-22 Wooldridge Joseph B. Continuous torque inverse displacement asymmetric rotary engine
RU2270924C2 (ru) * 2003-06-23 2006-02-27 Михаил Владимирович Спикин Планетарный роторно-поршневой двигатель внутреннего сгорания
US7350500B1 (en) 2006-02-24 2008-04-01 Webb David W Inverted cardioid engine
EP1921252A1 (en) * 2006-11-09 2008-05-14 Special Product Supplier GmbH Paddling blades engine
US20090074567A1 (en) * 2007-09-17 2009-03-19 John Howard Seagrave Positive-displacement turbine engine
US20100242897A1 (en) * 2009-03-25 2010-09-30 Lumenium Llc Inverse displacement asymmetric rotary (idar) engine
US20130224053A1 (en) * 2011-10-03 2013-08-29 Jan Hendrik Ate Wiekamp Coaxial progressive cavity pump
US8714135B2 (en) 2012-03-14 2014-05-06 Lumenium Llc IDAR-ACE inverse displacement asymmetric rotating alternative core engine
US9309765B2 (en) 2012-03-14 2016-04-12 Lumenium Llc Rotary machine
US10184392B2 (en) 2012-03-14 2019-01-22 Lumenium Llc Single chamber multiple independent contour rotary machine
US20190040867A1 (en) * 2017-08-02 2019-02-07 Poolstar Canada Limited Hydraulic rotary drive
US11168608B2 (en) 2015-04-13 2021-11-09 Lumenium Llc Single chamber multiple independent contour rotary machine
US11725515B2 (en) 2018-11-27 2023-08-15 Lumenium Llc Rotary engine with recirculating arc roller power transfer
US11920476B2 (en) 2015-04-13 2024-03-05 Lumenium Llc Rotary machine
US11927128B2 (en) 2020-05-15 2024-03-12 Lumenium Llc Rotary machine with hub driven transmission articulating a four bar linkage
US12146411B2 (en) 2015-04-13 2024-11-19 Lumenium Llc Rotary machine

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59232508A (ja) * 1983-06-17 1984-12-27 中松　義郎 睡眠誘導枕
JPS6319364U (enrdf_load_stackoverflow) * 1986-07-23 1988-02-08

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1831263A (en) * 1926-05-13 1931-11-10 Walter F Ross Internal combustion engine
US1922477A (en) * 1929-06-18 1933-08-15 Flind Herbert Charteris Construction of motive power engines and pumps
US2136066A (en) * 1935-05-13 1938-11-08 C J Bartlett Rotary engine
US3207425A (en) * 1965-03-22 1965-09-21 John E Morse Rolling body engine with multiple rotors

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1831263A (en) * 1926-05-13 1931-11-10 Walter F Ross Internal combustion engine
US1922477A (en) * 1929-06-18 1933-08-15 Flind Herbert Charteris Construction of motive power engines and pumps
US2136066A (en) * 1935-05-13 1938-11-08 C J Bartlett Rotary engine
US3207425A (en) * 1965-03-22 1965-09-21 John E Morse Rolling body engine with multiple rotors

Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3885531A (en) * 1973-06-29 1975-05-27 Raymond Lee Organization Inc Rotary internal combustion engine
US4055156A (en) * 1976-03-12 1977-10-25 Gundlach, S.A. Rotary engine
EP0379832A1 (de) * 1989-01-24 1990-08-01 André Feyereisen Verbrennungsmotor
US5156541A (en) * 1991-05-07 1992-10-20 Lew Hyok S Revolving vane pump-motor-meter with a toroidal working chamber
WO1994027031A1 (en) * 1993-05-13 1994-11-24 Brent Charles R Rotary vane mechanical power system
US5375987A (en) * 1993-05-13 1994-12-27 Brent; Charles R. Rotary vane mechanical power system utilizing positive displacement
US5819699A (en) * 1997-05-13 1998-10-13 Burns; William A. Rotary internal combustion engine
US6758188B2 (en) * 2002-07-16 2004-07-06 Joseph B. Wooldridge Continuous torque inverse displacement asymmetric rotary engine
CN100360775C (zh) * 2002-07-16 2008-01-09 卢门纽姆公司 产生连续转矩的相反置换的非对称旋转式发动机
RU2362894C2 (ru) * 2002-07-16 2009-07-27 Люмениум Ллс Обращенный асимметричный роторный двигатель с непрерывно действующим крутящим моментом
US20040011320A1 (en) * 2002-07-16 2004-01-22 Wooldridge Joseph B. Continuous torque inverse displacement asymmetric rotary engine
RU2270924C2 (ru) * 2003-06-23 2006-02-27 Михаил Владимирович Спикин Планетарный роторно-поршневой двигатель внутреннего сгорания
US7350500B1 (en) 2006-02-24 2008-04-01 Webb David W Inverted cardioid engine
EP1921252A1 (en) * 2006-11-09 2008-05-14 Special Product Supplier GmbH Paddling blades engine
US20080135013A1 (en) * 2006-11-09 2008-06-12 Abdalla Aref Adel-Gary Paddling blades engine
US8079343B2 (en) * 2007-09-17 2011-12-20 John Howard Seagrave Positive-displacement turbine engine
US20090074567A1 (en) * 2007-09-17 2009-03-19 John Howard Seagrave Positive-displacement turbine engine
US20100242897A1 (en) * 2009-03-25 2010-09-30 Lumenium Llc Inverse displacement asymmetric rotary (idar) engine
US9714605B2 (en) 2009-03-25 2017-07-25 Lumenium Llc Rotary machine
CN102575522A (zh) * 2009-03-25 2012-07-11 卢门纽姆公司 逆位移非对称旋转(idar)发动机
US8607762B2 (en) 2009-03-25 2013-12-17 Lumenium Llc Inverse displacement asymmetric rotary (IDAR) engine
CN102575522B (zh) * 2009-03-25 2014-04-30 卢门纽姆公司 逆位移非对称旋转(idar)发动机
US20130224053A1 (en) * 2011-10-03 2013-08-29 Jan Hendrik Ate Wiekamp Coaxial progressive cavity pump
US8714135B2 (en) 2012-03-14 2014-05-06 Lumenium Llc IDAR-ACE inverse displacement asymmetric rotating alternative core engine
US9309765B2 (en) 2012-03-14 2016-04-12 Lumenium Llc Rotary machine
US9822642B2 (en) 2012-03-14 2017-11-21 Lumenium Llc Rotary machine
US10184392B2 (en) 2012-03-14 2019-01-22 Lumenium Llc Single chamber multiple independent contour rotary machine
US11168608B2 (en) 2015-04-13 2021-11-09 Lumenium Llc Single chamber multiple independent contour rotary machine
US11920476B2 (en) 2015-04-13 2024-03-05 Lumenium Llc Rotary machine
US12146411B2 (en) 2015-04-13 2024-11-19 Lumenium Llc Rotary machine
US20190040867A1 (en) * 2017-08-02 2019-02-07 Poolstar Canada Limited Hydraulic rotary drive
US11725515B2 (en) 2018-11-27 2023-08-15 Lumenium Llc Rotary engine with recirculating arc roller power transfer
US11927128B2 (en) 2020-05-15 2024-03-12 Lumenium Llc Rotary machine with hub driven transmission articulating a four bar linkage

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JPS5618772B1 (enrdf_load_stackoverflow) 1981-05-01

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