WO1995017582A1 - Rotary motion drive, especially for internal combustion engines - Google Patents

Rotary motion drive, especially for internal combustion engines Download PDF

Info

Publication number
WO1995017582A1
WO1995017582A1 PCT/HU1994/000059 HU9400059W WO9517582A1 WO 1995017582 A1 WO1995017582 A1 WO 1995017582A1 HU 9400059 W HU9400059 W HU 9400059W WO 9517582 A1 WO9517582 A1 WO 9517582A1
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
oval
gear
shaft
output shaft
Prior art date
Application number
PCT/HU1994/000059
Other languages
French (fr)
Inventor
Marcell JÁNOSI
Original Assignee
Janosi Marcell
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Janosi Marcell filed Critical Janosi Marcell
Publication of WO1995017582A1 publication Critical patent/WO1995017582A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/02Rotary-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
    • F01C1/063Rotary-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
    • F01C1/077Rotary-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four

Definitions

  • the present invention relates to the rotary drive, that is converting the petrol's energy into rotary motion or if it is rotated by electrical propulsion, it can convert the rotary motion into pressure energy.
  • Its application field is first of all the internal combustion engine, but we can apply in other fields, too.
  • the principle of the rotary drive is applicable for motors or pumps. (The medium can be: petrol, steam, compressed air and oil).
  • the rotary drive is very simple. It has a pair of concentric rotors and one output shaft, all of the three are connected to each other by different solutions.
  • the principle of operation is common in all the above inventions:
  • the rotary drive has two rotors and one output shaft to be driven by two rotors.
  • a cylindrical housing comprises a pair of concentric rotors, each rotor has two vanes.
  • the rotors are rotating with varying speed.
  • the movable combustion chambers are defined by all of two neighbouring vanes, running after one another with cyclically changing speed, in order to periodically approach and move away from one another.
  • the four neighbouring vanes define four working chambers in a cylindrical housing: their relative speed varying, so that the volume of each working chamber is alternately expanded and then contracted.
  • An inlet port, exhaust port and ignition device are provided at appropriate points on the cylindrical housing, so that the expansion and contraction of the working chambers will provide induction, compression expansion and exhaust strokes.
  • thermodinamical efficiency has to be reached - five side of the cubical housing of drive should be free for other subassemblies*
  • the object of the present invention is to provide a new rotary drive for internal combustion engines or for pumps.
  • the key of the new rotary drive is a new connective system.
  • This new connective system will determine and will provide every main performance of the new rotary drive.
  • the new rotary drive is inseparable from this new connection system. Accordingly, more precisely, the object of the present invention is to provide a new rotary drive by a new connective system, which fulfils the requirements presented at the end of the previous chapter.
  • Rotor's speed characteristic (restrictions and possibilities).
  • n x is the r.p.m. of rotor in the "x" time, is the r.p.m. of rotor in
  • rotary engines has four unavoidable components: a housing (not moving), one output shaft (with constant speed) and two rotors (with ⁇ ylindrically varying speed).
  • An engine is defined by so called “capacity” (surface of bore ⁇ stroke ⁇ number of cylinder) as an example we will calculate with 1000 cm 3 net capacity. We add to that the necessary compression area about 100 cm 3 , so we have now 1100 cm 3 , as an internal capacity.
  • the shape of this internal capacity is cylindrical.
  • the 2300 cm 3 is the gross external volume of a theorical engine, on which we don't apply any components besides the housing.
  • the average gross external volume of the present manufactured engines is about 15.000 cm 3 per 1000 cm 3 net capacity.
  • the general solution of rotary drive is that, we connect the output shaft to each rotor with two cyclically varying transmissions, which are at the same execution and are positioned 90° out of phase on output shaft.
  • the periodically varying transmission is producing two different ratio, which are alternating during time, where the whole periodic time is
  • the working Ghamber has a va ⁇ umic pipe (between the exhaust and inlet ports) to clean up the remaining pollutant emissions (after the exhaustion).
  • each rotor's oval gear is connected to the oval gear of output shaft.
  • the drive is simple and robust there are only three unavoidable rotary components and a housing without any other motion component
  • the oval has two axes, which are perpendicular to each other.
  • the lengths of axes are: 2 R min and 2R max and the other radii are between R min and R max .
  • ⁇ x o is the position angle of the driven gear, which is between R min and R ⁇ x o
  • Figure 1 shows a therortical engine with a stroking chamber capacity of 1000 cm 3 and a compression area of 100 cm 3 .
  • the sum of this unavoidable capacity is 1100 cm 3 , its shape is cylindrical and it is built into a cubical casing.
  • Figure 2 shows a vertical section and a cross section and a principal scheme of the simplest rotary drive.
  • Figure 3 shows a vertical section and a cross section of the rotary drive with double oval gear and with coaxial output shaft.
  • Figure 4 shows two vertical section and an elevation of the one-sided rotary drive, with double oval gear and with coaxial output shaft.
  • Figure 5 shows a vertical section and an elevation of the two-sided rotary drive, with oval-curve solution.
  • Figure 6 shows a vertical section and an elevation of the two-sided rotary drive with two external gears.
  • Figure 7 shows a vertical section and two exploded views of the rotor's vanes in the one of embodiments.
  • Figure 8 shows two vertical section and two exploded views of the rotor's vanes.
  • Figure 9 shows a vertical and an elevation of four rotary drives built in a common housing.
  • Figure 10 shows a modified drive, which can be operated by steam or compressed air.
  • Figure 1 shows the theoretical limit of the external volume of the internal combustion engine.
  • this theory is based on some subjective restrictions; e.g. the compression ratio is 10:1, the thickness of wall is 1 cm and etc.
  • oval gears 16, 17, 18, 19 there are two pairs oval gears 16, 17, 18, 19 which are connected to each other, more precisely, two oval gears 17, 19 are connected to the output shaft 15 and the oval gear 16 is connected to the rotor's shaft and the oval gear 18 is connected to the rotor's shaft 7.
  • the oval gear 17 and the oval gear 19 are positioned 90° out of phase on the output shaft 15, from each other. In the elevation we can see the connection between two oval gears 16, 17. The ⁇ angle is only one possibility to the decreasing of sizes.
  • the output shaft 15 is turned back by 45° from the position on the elevation, in order to show the moment of an explosion.
  • the Figure 4 shows a one-sided solution, which is preferable to the double sided solution to present before, because much more place remains to mount other subassemblies to the drive. Further preferable of this solution, the all oval gears are mounted on one place, and the mounting and the oil-, inlet-, exhaust- and cooling systems will be simpler.
  • the one-side solution is the following: two shaft 30 are fastened on the cover 14.
  • the output shaft 15 is located on the cover 14 too.
  • the three shaft are composed angle of 90°, where the output shaft 15 is in the centre, we can see this in the "D" elevation.
  • the oval gear 16 is fastened on the rotor's shaft 26.
  • the double oval gear 28 is connected to the oval gear 16.
  • the oval gear 17 is fastened on the output shaft 15.
  • the oval gear 17 is connected to the double oval gear 28.
  • the oval gear 18 is fastened on the rotor's shaft 27.
  • the cover 13 comprises the oval curve 37.
  • the disk 34 is fastened on the rotor's shaft 6.
  • the disk 33 is fastened on the output shaft 15.
  • the puller rods 31 are connected to the disk 33 and to the pins 35.
  • the pusher rods 32 are connected to the disk 34 and to the pins 35.
  • the rollers 36 are placed free-wheeled on the pins 35.
  • the rollers 36 can be moving according to the oval curve, if the output shaft 15 is rotating with constant speed and the output shaft 15 is connected to the rotor's shaft 6, making use of the puller rods 31 and of the pusher rods 32, when the rotor's shaft will be rotating with cyclical varying speed.
  • the rotor's shaft 6 will be periodically accelerating and retarding according to the position of the output shaft 15. The performance of this solution can reach as such the level as possible with the oval gear.
  • the rotor shafts 6, 7 and the output shaft 15 are connected each other by the rods and the oval curve on the one-side.
  • the oval curve and the roads (without gears) give the solution to the connection, which is necessary between output shaft 15 and two rotors 6, 7.
  • the Figure 6 shows an other curve solution with two gears.
  • the gear 38 is fastened on the rotor's shaft 6.
  • the gear 39 is locating in the cover 13.
  • the output shaft 15 is located inside of the gear 39, but eccentrically. Its eccentricity is "e”.
  • the output shaft 15 is locating in the rotor's housing 1.
  • the inside of the disk 41 has an curve which is represented in a straight line. But the forme of this curve can be at optional.
  • the roller 40 can be moving in this curve.
  • the roller 40 is located rotatably on the side of gear 39.
  • the disk 41 is fastened on the output shaft 15. If the output shaft 15 turns with constant speed, the disk 41 is the driving wheel and the gear 39 is the driven wheel.
  • the disc 41 and the gear 39 are connected by the roller 40.
  • the gear 39 is connected to the gear 38.
  • the ratio is 1:2.
  • the rotor's shaft 6 is rotating alternately with varying speed.
  • the rotary drive is built up two sides. The two side are making in the same way, but they are mounted with two roller 40, which are positioned 180° out of phase from each other.
  • the Figure 7 shows the two rotors.
  • the rotor's shaft 6, 7 which are located in one axis.
  • the rotor's vanes 8, 9 are fastened on the rotor's shaft 6.
  • the rotor's vanes 10, 11 are fastened on the rotor's shaft 7. Restriction is the two sizes marked by L and L/2.
  • the Figure 8 shows an other solution, this is very usable for longer size of L, because the distribution of the working load is uniform.
  • the rotor systems contain more elements.
  • the rotor's vanes 8, 9 are fastened on the rotor's shaft 26. There is necessary two uniform pieces of them.
  • the rotor's vanes 10, 11 are located on the rotor's shaft 27.
  • the Figure 9 shows a rotary drive with four rotors, where the four rotors are built in a common housing 43. There are four cylindrical rotor's area 2 in a common housing 43. The common housing is closed by the common covers 44, 45. The "B" elevation presents the four gears 42, which are connected to each others. Precisely, four gears 42 are fastened on the four rotor's shaft.
  • the oval gear 18 is fastened on the output shaft 15 (the other oval gear 18 is fastened on the other end of the same output shaft 15, but it is positioned 90o out of phase on the output shaft 15).
  • the oval gear 17 is rotatably located on the rotor's shaft.
  • the oval gear 16 is fastened on the rotor's shaft.
  • the oval gears 16, 17, 18 are connected to each other. All other operations are in the some way, which have already presented before in Figure 2.
  • the Figure 10 shows a cross section of the rotary drive, which is applicable for other mediums (e.g. steam or compressed air).
  • mediums e.g. steam or compressed air.

Landscapes

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

Abstract

Rotary motion drive, which comprises rotor's housing (1), in which there are a cylindrical rotor's area (2) with inlet port and exhaust port. Two pairs of rotors which are rotatably mounted in the cylindrical rotor's area (2). Each rotor has a rotor's shaft (6, 7), which are fastened to two pairs of vanes (8, 9) and (10, 11). The cylindrical rotor's area (2) is divided by the neighbouring vanes to four working chambers (48), which are alternately expanded and then contracted. There is an output shaft (15) which is connected with rotor's shaft (6) and rotor's shaft (7) by at least two oval gears. Precisely, one oval gear (16) is fastened on the rotor's shaft (6). The other oval gear (18) is fastened on the rotor's shaft (7). Two oval gears (17, 19) are fastened on the output shaft (15). These oval gears (17, 19) are positioned 90° out of phase on the output shaft (15). The oval gear (16) is connected with the oval gear (17). The oval gear (18) is connected with the oval gear (19). These connections can be direct or an additional oval gear can be inserted.

Description

ROTARY MOTION DRIVE, ESPECIALLY FOR INTERNAL COMBUSTION
ENGINES
BACKGROUND OF THE INVENTION
1./ Field of the Invention
The present invention relates to the rotary drive, that is converting the petrol's energy into rotary motion or if it is rotated by electrical propulsion, it can convert the rotary motion into pressure energy. Its application field is first of all the internal combustion engine, but we can apply in other fields, too. The principle of the rotary drive is applicable for motors or pumps. (The medium can be: petrol, steam, compressed air and oil). The rotary drive is very simple. It has a pair of concentric rotors and one output shaft, all of the three are connected to each other by different solutions.
2./ Brief Description of the Prior Art.
The idea of rotary drive is very old and well known. The first invention was in 1906 /No 826.985 USA, D. APPEL/ and nowadays hundreds of the same invention are published. Some of them are as follows:
- PCT WO 90/07632 Energy converting machine.
Priority data 09.11.1989.
- USA 5112204 Oscillatory rotating engines...
Foreign Application Priority data 15.11.1989.
- EPA 0554227A1 Engine with rotary pistons...
Priority data 30.01.1992.
The principle of operation is common in all the above inventions: The rotary drive has two rotors and one output shaft to be driven by two rotors.
A cylindrical housing comprises a pair of concentric rotors, each rotor has two vanes. The rotors are rotating with varying speed. The movable combustion chambers are defined by all of two neighbouring vanes, running after one another with cyclically changing speed, in order to periodically approach and move away from one another. The four neighbouring vanes define four working chambers in a cylindrical housing: their relative speed varying, so that the volume of each working chamber is alternately expanded and then contracted. An inlet port, exhaust port and ignition device are provided at appropriate points on the cylindrical housing, so that the expansion and contraction of the working chambers will provide induction, compression expansion and exhaust strokes.
The solution of speed variation aren't common in all inventions:
- They are different from each other in mechanical solution
- Their speed characteristic are consequently also
different from each other
There are three important components of such drives:
- two rotors
- one output shaft
Accordingly, nowadays the main question is:
How should we connect the three important components to each other?
The solution has to fulfil the following requirements:
- has to be simple and robust
- number of components has to be as low as possible
- dimensions and weight reduction ("down sizing")
- preferably no application of eccenter, crankshaft*
- preferably no application of linkage, piston's rod*
- preferably no application of internal gears*
- a good thermodinamical efficiency has to be reached - five side of the cubical housing of drive should be free for other subassemblies*
- the balancing problems have to eliminated*
- the combustion process has to be equivalent to that of a four-stroke eight cylinder engine. /Eight explosions during two revolutions of output shaft/.
*The above requirements haven't been fulfilled totally by the known inventions, till now.
OBJECTS AND SUMMARY OF THE INVENTION
The object of the present invention is to provide a new rotary drive for internal combustion engines or for pumps. The key of the new rotary drive is a new connective system. This new connective system will determine and will provide every main performance of the new rotary drive. The new rotary drive is inseparable from this new connection system. Accordingly, more precisely, the object of the present invention is to provide a new rotary drive by a new connective system, which fulfils the requirements presented at the end of the previous chapter.
In the first step we have to clear some theoretical questions, as follows:
- the rotor's speed characteristic, what we can reach theoretically
- the minimum number of components, what we can reach theoretically
- the smallest external dimension, what we can reach theoretically
Rotor's speed characteristic (restrictions and possibilities).
There are two restrictions of the rotor's speed characteristic. The time of one revolution is
, where the "no" is the output shaft's revolution
Figure imgf000005_0001
per minute. Accordingly, the periodic time of rotor's speed characteristic is , this is the first restriction. The
Figure imgf000006_0001
speed characteristic of the rotor has to fulfil the following equivalent:
Figure imgf000006_0002
this is the second restriction, where nx is the r.p.m. of rotor in the "x" time, is the r.p.m. of rotor in
.
the " " time.
Figure imgf000006_0003
Figure imgf000006_0004
There are three possibilities:
- depend on max output r.p.m., we can choose the convenient acceleration
Figure imgf000006_0005
f
- the run up and run down of speed can be the same
(the characteristic can be symmetrical).
Figure imgf000006_0006
- between the + — and the — , the acceleration can
Figure imgf000006_0007
Figure imgf000006_0008
be "0" for a long time (about for )
Figure imgf000006_0009
These possibilities are theoretical of course.
The minimum number of components (we can reach theoretically).
Let's consider those group of the elements of the drive as one component, which do not moving independently from each other (e.g. there is a shaft with two fastening wheels, this group of three elements is one component, if the wheels aren't rotatable or movable independently on the shaft).
Accordingly, rotary engines has four unavoidable components: a housing (not moving), one output shaft (with constant speed) and two rotors (with σylindrically varying speed).
The smallest external dimension.
An engine is defined by so called "capacity" (surface of bore × stroke × number of cylinder) as an example we will calculate with 1000 cm3 net capacity. We add to that the necessary compression area about 100 cm3, so we have now 1100 cm3, as an internal capacity. The shape of this internal capacity is cylindrical. We make a cubical theoretical engine, the thickness of its walls is one centimetre. The external sizes of this cubical engine are the followings: 13,2 cm × 13,2 cm × 13,2 cm = 2300 cm3.
These external sizes are including the following:
engine' s capacity . .. . .. . . .. . .. . . .. . .. . . .. . .. . . . 1000 cm3 compression's capacity . .. . .. . . .. . .. . . .. . .. . . .. . . 100 cm3 volume of the walls . .. . .. . . .. . .. . . .. . .. . . .. . .. . . 1200 cm3 pistons, shafts, piston's rods, crankshafts,
valves , springs and others components . .. . .. . .. . . 0 cm 3
2300 cm3
Of course, the other assemblies (carburetter, cooling system, compression system, transmission, gearbox, generator, starter motor and other assemblies) don't belong to the present invention.
The 2300 cm3 is the gross external volume of a theorical engine, on which we don't apply any components besides the housing. The average gross external volume of the present manufactured engines is about 15.000 cm3 per 1000 cm3 net capacity.
In the second step we are presenting the invention.
The general solution of rotary drive is that, we connect the output shaft to each rotor with two cyclically varying transmissions, which are at the same execution and are positioned 90° out of phase on output shaft. The periodically varying transmission is producing two different ratio, which are alternating during
Figure imgf000007_0001
time, where the whole periodic time is
Figure imgf000007_0002
(no is the r.p.m. of output shaft). One of the ratios is
(about 1,5-2) the other is (about 0,66-0,5).
Figure imgf000007_0004
This is a principal solution.
Figure imgf000007_0003
Every main performances of new rotary drive is decided by the real solution of periodically varying transmission. One of the real elegant solutions is the use of two pairs of oval gears, which are fastened on the output shaft and on the rotors. The realisable rotary drive is detailed as follows:
- the working chamber must be cylindrical
- in this cylinder there are two rotors, on each rotor there are two vanes (or blades, or pistons) and an oval
- the shape of gears is oval (elliptical)
are suggested (by inventor)
Figure imgf000008_0001
- there is an output shaft with two oval gears, which are positioned 90° out of phase on the output shaft
- the working Ghamber has a vaσumic pipe (between the exhaust and inlet ports) to clean up the remaining pollutant emissions (after the exhaustion).
- each rotor's oval gear is connected to the oval gear of output shaft.
The above solution provide the fulfilment of all requirements (see 2-3 pages), all restrictions (see 4 page) and reaches nearly all theoretical possibilities. The summary of the results is the following:
- the drive is simple and robust there are only three unavoidable rotary components and a housing without any other motion component
- there is minimum number of components (there aren't camshaft, valves, spring for valves, exhaust manifold, inlet manifold etc)
- external volume is very small (about 5000 cm3 /1000 cm3/
- there aren't eccenter and crankshaft
- there aren't link age and piston's rod
- there aren't internal gears
- we can reach a good thermodinamical efficiency by good rotor's speed characteristic, that is symmetrical, straight for a long period, and its acceleration is variable to a certain extent, and a new process is inserted between the exhaust port and inlet port (so called "rinse stroke")
- we left five side of the cubical housing free for other assemblies
- the drive hasn't balancing problems
- the combustion process of drive is equivalent a four- stroke, eight cylinder engine. In addition it has a "fifth stroke" that is called "rinse stroke"
- there isn't changing direction of rotary components
In the following we like to present the calculation of rotary drive with oval gears (for technicians):
The oval gear.
The oval has two axes, which are perpendicular to each other. The lengths of axes are: 2 Rmin and 2Rmax and the other radii are between Rmin and Rmax. The axial distance of the two oval gears is C = constant:
C = Rmin + Rmax = Rαºx+ Rβx° This is the first restrictions for oval gears,
where α ºx is the position angle of the driving gear
which is between Rmin and Rαxº
βxº is the position angle of the driven gear, which is between Rmin and Rβxº
This is the second restriction for oval
Figure imgf000009_0003
gears,
where Lα xº = length of curve (which belongs to αxº) and
= length of curve (which belongs to (90°-βxº)
Figure imgf000009_0002
Average ratio:
if the driving oval gear turns away an angle 45º /from 0º-to αº45/
when the driven oval gear turns away an angle εº and the average ratio is
Figure imgf000009_0001
if the driving oval gear turns away further angle
45º (from αº45 -to αº90 ) when the driven oval gear turns away an angle (90°-εº) and
the average ratio is
Figure imgf000010_0002
Figure imgf000010_0001
DESCRIPTION OF THE DRAWINGS
Figure 1 shows a therortical engine with a stroking chamber capacity of 1000 cm3 and a compression area of 100 cm3. The sum of this unavoidable capacity is 1100 cm3, its shape is cylindrical and it is built into a cubical casing.
This is the "engine" which has the smallest external volume, theoretically.
Figure 2 shows a vertical section and a cross section and a principal scheme of the simplest rotary drive.
Figure 3 shows a vertical section and a cross section of the rotary drive with double oval gear and with coaxial output shaft.
Figure 4 shows two vertical section and an elevation of the one-sided rotary drive, with double oval gear and with coaxial output shaft.
Figure 5 shows a vertical section and an elevation of the two-sided rotary drive, with oval-curve solution.
Figure 6 shows a vertical section and an elevation of the two-sided rotary drive with two external gears.
Figure 7 shows a vertical section and two exploded views of the rotor's vanes in the one of embodiments.
Figure 8 shows two vertical section and two exploded views of the rotor's vanes.
Figure 9 shows a vertical and an elevation of four rotary drives built in a common housing.
Figure 10 shows a modified drive, which can be operated by steam or compressed air.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Figure 1 shows the theoretical limit of the external volume of the internal combustion engine. Of course this theory is based on some subjective restrictions; e.g. the compression ratio is 10:1, the thickness of wall is 1 cm and etc. We can see this theoretical engine built in a cubical casing 5, which has an external volume of
2300 cm3 its wall thickness is 1 cm and the cylindrical total capacity is 1100 cm3 from the net capacity of
1000 cm3 and the 100 cm3 compression area 4. This "engine" is equal to a four stroke, 1000 cm3 capacity engine without the unavoidable operating components. This theoretical engine hasn't got any operating components, only one empty stroking chamber 3. Of course, a real working engine of 1000 cm3 has never reached the the external volume of 2300 cm3, but we can hope this new rotary drive can reach an external volume of 5000 cm3/1000 cm3 working chamber. In the figure 2 we are showing a simplest embodiment of the rotary drive. In the vertical section and in the "A" cross section we can see in the rotor's housing 1 the cylindrical rotor's area 2 and in it there is the rotor shaft 6, on which the rotor's vane 8 and the rotor's vane 9 are fastened. In the same way there is the rotor's shaft 7, on which the rotor's vane 10 and the rotor's vane 11 are fastened. The cover 13 and the cover 14 are fastened to the rotor's housing 1. The covers and the rotors housing 1 define the cylindrical rotor's area 2. In the principal scheme we can see two principal transmissions 49, which are connected to the output shaft 15 and to the rotor's shaft 6 and to the rotor's shaft 7. In the real embodiment, there are two pairs oval gears 16, 17, 18, 19 which are connected to each other, more precisely, two oval gears 17, 19 are connected to the output shaft 15 and the oval gear 16 is connected to the rotor's shaft and the oval gear 18 is connected to the rotor's shaft 7. The oval gear 17 and the oval gear 19 are positioned 90° out of phase on the output shaft 15, from each other. In the elevation we can see the connection between two oval gears 16, 17. The α angle is only one possibility to the decreasing of sizes. In the "A" cross section, the output shaft 15 is turned back by 45° from the position on the elevation, in order to show the moment of an explosion. In the compression area 4, we can see the ignition spark plug 20, and in opposite are the vacumiσ pipe 23 and the fresh-cooling air pipe 24, so clean up the remaining pollutant emissions after exhaust stroke. Next to them, there are the inlet port 21 and the exhaust port 22. In the "A" cross section shows the moment of the starting explosion. The moment that, the following working process are starting;
- in the compression area 4 (at the top, next to the spark plug 20) the combustion process starts
(expansion-stroke)
- in the opposite side, in the other compression area 4 (at the bottom) the clean process goes (the vacumic pipe 23 and the fresh-cooling air pipe 24 have opened and started the rinse)
(rinse-stroke)
- after the vacumic pipe 23 is closed by the rotor's vane 9, the suction process will start from the inlet port 21 (induction-stroke)
- in the working chamber 48 (on the right) the exhaust process starts.
(exhaust-stroke)
- in the opposite side, in the other working chamber 48, the compression process starts.
(compression-stroke)
The above processes are repeated four times per one revolution of output shaft 15, according to the position of the oval gears 17, 19.
The solution, which we can see in the Figure 3 differs from Figure 2, because its transmissions are built up two pairs of oval gears per side. This solution gives a possibility; the output shaft 15 can be located in the centre of the rotor's shaft 6. The oval gear 16 is fastened on the rotor's shaft 6. The double oval gear 12 is connected to the oval gear 16. The two oval gears of the double oval gear 12 are positioned 90° out phase from each other. The shaft 25 is fastened on the cover 13 and the double oval gear 12 is rotatably mounted on the shaft 25. The double oval gear 12 is driving the oval gear 17, which is fastened on the output shaft 15. In the Figure 3 we Gan see the rotor's housing 1, in which the cylindrical rotor's area 2, the compression area 4 and the working chamber 48 are located. All others components are operating in the same way, which have already presented before in Figure 2.
The Figure 4 shows a one-sided solution, which is preferable to the double sided solution to present before, because much more place remains to mount other subassemblies to the drive. Further preferable of this solution, the all oval gears are mounted on one place, and the mounting and the oil-, inlet-, exhaust- and cooling systems will be simpler. The one-side solution is the following: two shaft 30 are fastened on the cover 14. The output shaft 15 is located on the cover 14 too. The three shaft are composed angle of 90°, where the output shaft 15 is in the centre, we can see this in the "D" elevation. There are mounted the rotor's shaft 26, 27 in the centre. The oval gear 16 is fastened on the rotor's shaft 26. The double oval gear 28 is connected to the oval gear 16. The oval gear 17 is fastened on the output shaft 15. The oval gear 17 is connected to the double oval gear 28. The oval gear 18 is fastened on the rotor's shaft 27. The double oval gear 29 is connected to the oval gear 17 and to the oval gear 18.
In the Figure 5 we present the solution of the oval curve, which is instead of the solution of the oval gear. This solution doesn't use gears, but use some roads and one oval curve. The cover 13 comprises the oval curve 37. The disk 34 is fastened on the rotor's shaft 6. The disk 33 is fastened on the output shaft 15. The puller rods 31 are connected to the disk 33 and to the pins 35. The pusher rods 32 are connected to the disk 34 and to the pins 35. The rollers 36 are placed free-wheeled on the pins 35. The rollers 36 can be moving according to the oval curve, if the output shaft 15 is rotating with constant speed and the output shaft 15 is connected to the rotor's shaft 6, making use of the puller rods 31 and of the pusher rods 32, when the rotor's shaft will be rotating with cyclical varying speed. The rotor's shaft 6 will be periodically accelerating and retarding according to the position of the output shaft 15. The performance of this solution can reach as such the level as possible with the oval gear.
On the base of this principle, the rotor shafts 6, 7 and the output shaft 15 are connected each other by the rods and the oval curve on the one-side. The oval curve and the roads (without gears) give the solution to the connection, which is necessary between output shaft 15 and two rotors 6, 7.
The Figure 6 shows an other curve solution with two gears. The gear 38 is fastened on the rotor's shaft 6. The gear 39 is locating in the cover 13. The output shaft 15 is located inside of the gear 39, but eccentrically. Its eccentricity is "e". The output shaft 15 is locating in the rotor's housing 1. The inside of the disk 41 has an curve which is represented in a straight line. But the forme of this curve can be at optional. The roller 40 can be moving in this curve. The roller 40 is located rotatably on the side of gear 39. The disk 41 is fastened on the output shaft 15. If the output shaft 15 turns with constant speed, the disk 41 is the driving wheel and the gear 39 is the driven wheel. The disc 41 and the gear 39 are connected by the roller 40. The gear 39 is connected to the gear 38. The ratio is 1:2. According to the position of the output shaft 15, the rotor's shaft 6 is rotating alternately with varying speed. Of course, only one side is represented by figure 6, but the rotary drive is built up two sides. The two side are making in the same way, but they are mounted with two roller 40, which are positioned 180° out of phase from each other.
The Figure 7 shows the two rotors. We can see in exploded views two rotor's shaft 6, 7 which are located in one axis. The rotor's vanes 8, 9 are fastened on the rotor's shaft 6. The rotor's vanes 10, 11 are fastened on the rotor's shaft 7. Restriction is the two sizes marked by L and L/2. The Figure 8 shows an other solution, this is very usable for longer size of L, because the distribution of the working load is uniform. The rotor systems contain more elements. The rotor's vanes 8, 9 are fastened on the rotor's shaft 26. There is necessary two uniform pieces of them. The rotor's vanes 10, 11 are located on the rotor's shaft 27. There is necessary one piece of them. Restrictions are the four sizes, marked by øA, øA, ød<øD. The Figure 9 shows a rotary drive with four rotors, where the four rotors are built in a common housing 43. There are four cylindrical rotor's area 2 in a common housing 43. The common housing is closed by the common covers 44, 45. The "B" elevation presents the four gears 42, which are connected to each others. Precisely, four gears 42 are fastened on the four rotor's shaft. The oval gear 18 is fastened on the output shaft 15 (the other oval gear 18 is fastened on the other end of the same output shaft 15, but it is positioned 90º out of phase on the output shaft 15). The oval gear 17 is rotatably located on the rotor's shaft. The oval gear 16 is fastened on the rotor's shaft. The oval gears 16, 17, 18 are connected to each other. All other operations are in the some way, which have already presented before in Figure 2.
The Figure 10 shows a cross section of the rotary drive, which is applicable for other mediums (e.g. steam or compressed air). We can see the location of high pressure pipe 46 and the location of low pressure pipe 47. The driving medium is arriving in the high pressure pipe 44 and after expanding the "tired" medium is moving off in the low pressure pipe 47.

Claims

1. Rotary motion drive, which comprises rotor's housing (1), in which there are a cylindrical rotor's area (2) with inlet port and exhaust port, two pairs of rotors which are rotatably mounted in the cylindrical rotor's area (2); each rotor has a rotor's shaft (6, 7), which are fastened to two pairs of vanes (8, 9) and (10, 11), the cylindrical rotor's area (2) is divided by the neighbouring vanes to four working chambers (48), which are alternately expanded and then contracted, and there is an output shaft (15); this rotary motion drive being characterised by;
the said output shaft (15) being coupled with said rotor's shaft (6) and said rotor's shaft (7) by at least two oval gears, precisely, one said oval gear (16) being mounted on said the rotor's shaft (6) and the other said oval gear (18) being mounted on rotor's shaft (7), and two said oval gear (17, 19) being mounted on the output shaft (15), these said oval gears (17, 19) are positioned 90° out of phase on the output shaft (15), the said oval gear (16) being coupled with said oval gear (17) and said oval gear (18) being coupled with said oval gear (19), these said connections having a such formation, that provides an alternating movement between the said two rotors, these said connections can be direct or an additional said oval gear can be inserted e.g. the double said oval gear (12); the rolling or pitch curve of these said oval gears is the same, and it has to fulfil two said restrictions; first restriction is this;
Rsin + Rmax = Rαxº + R βx° where Rαºx= radius of driving oval gear, Rβx°= radius of driven oval gear, where αxº and βx° are the position angles, which are between Rsin and Rαx, or Rβx°, if they are= Rsin, when α xº and βxº are="0"; second restriction is this; L αxº= L(90º-βxº) where "L αxº " is length of the curve, which belongs to α x, " L (90°-(x°) " is length of the curve, which belongs to (90°-βx°).
2. Rotary motion drive according to claim 1, wherein the said output shaft (15) is placed coaxially in the centre of said rotor's shaft (6) and said oval gear (17) being mounted on said output shaft (15), and the said oval gear (16) being mounted on said rotor's shaft (6), the said double oval gear (12) being coupled with said oval gear (16) and said oval gear (17).
3. Rotary motion drive according to claims 1 and 2, wherein the said output shaft (15) being placed on said common cover (45), tile oval gear (18) is mounted to said output shaft (15) and the oval gear (16) is mounted to the rotor shaft (6), and the oval gear (17) is a said connection between said oval gear (16) and said oval gear (18), the centres of three said oval gears (16, 17, 18) have to constitute an. isosceles right-angled triangle.
4. Rotary motion drive according to claim 1 wherein there are the said vacumic pipe (23) and the said fresh-cooling air pipe (24), their position is the opposite of spark plug (2-0),
5. Rotary motion drive according to claim 1, in which there is an said oval curve (37) instead of the oval gears, the said oval curve (37) is fastened on the rotor's housing, the roller (3-6) can be moved on the restricted way of said oval curve (37), the roller (36) being rotatably mounted on said puller rod (31) and on said pusher rod (32), the puller rod (31) is turnably and tangentially mounted for said disk (33) which is fastened on the output shaft (15), the pusher rod (32) is turnably and tangentially mounted for the disk (34) which being mounted on rotor's shaft (6).
6. Rotary motion drive according to claim 1, in which there are two external gears (38, 39) instead of the oval gears, the said gear (38) is mounted on the rotor's shaft (6), the said gear (39) is rotatably mounted on the cover (13), the ratio is 2:1 between said gear (38) and said gear (39), the output shaft (15) is rotatable mounted in the rotor's housing (2), the position of the output shaft (15) being placed eccentrically at the centre of said gear (39), the roller (40) is rotatably mounted on the side of said gear (39), the said roller (40) is connected with the disc (41) which is fastened on output shaft (15).
PCT/HU1994/000059 1993-12-23 1994-12-08 Rotary motion drive, especially for internal combustion engines WO1995017582A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
HU9303737A HU215194B (en) 1993-12-23 1993-12-23 Rotary energy-transfer machine, mainly internal combustion engine

Publications (1)

Publication Number Publication Date
WO1995017582A1 true WO1995017582A1 (en) 1995-06-29

Family

ID=10984299

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/HU1994/000059 WO1995017582A1 (en) 1993-12-23 1994-12-08 Rotary motion drive, especially for internal combustion engines

Country Status (2)

Country Link
HU (1) HU215194B (en)
WO (1) WO1995017582A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2065560A2 (en) 2007-11-30 2009-06-03 MONDL, Fritz Internal combustion engine
US7631632B2 (en) * 2003-11-21 2009-12-15 Anatoly Arov Orbital engine/pump with multiple toroidal cylinders

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1482628A (en) * 1919-02-24 1924-02-05 Frank A Bullington Rotary engine
US2050603A (en) * 1933-03-11 1936-08-11 Gardner Cummings Engine
US3430573A (en) * 1965-10-01 1969-03-04 Aero Commerce Gmbh Rotary piston apparatus
DE1576912A1 (en) * 1967-07-25 1970-12-10 Robert Kaufmann Roka rotary piston machine
FR2147390A5 (en) * 1971-07-26 1973-03-09 Lampson Serge
DE2443290A1 (en) * 1973-09-10 1975-03-13 Luigi Maria Murone MACHINE WITH HYPERELLIPTICAL GEARS
GB2138094A (en) * 1983-04-12 1984-10-17 Cefin Spa Device for converting uniform rotary motion into variable speed rotary motion
US5083539A (en) * 1990-10-19 1992-01-28 Cornelio Seno L Concentric rotary vane machine with elliptical gears controlling vane movement

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1482628A (en) * 1919-02-24 1924-02-05 Frank A Bullington Rotary engine
US2050603A (en) * 1933-03-11 1936-08-11 Gardner Cummings Engine
US3430573A (en) * 1965-10-01 1969-03-04 Aero Commerce Gmbh Rotary piston apparatus
DE1576912A1 (en) * 1967-07-25 1970-12-10 Robert Kaufmann Roka rotary piston machine
FR2147390A5 (en) * 1971-07-26 1973-03-09 Lampson Serge
DE2443290A1 (en) * 1973-09-10 1975-03-13 Luigi Maria Murone MACHINE WITH HYPERELLIPTICAL GEARS
GB2138094A (en) * 1983-04-12 1984-10-17 Cefin Spa Device for converting uniform rotary motion into variable speed rotary motion
US5083539A (en) * 1990-10-19 1992-01-28 Cornelio Seno L Concentric rotary vane machine with elliptical gears controlling vane movement

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7631632B2 (en) * 2003-11-21 2009-12-15 Anatoly Arov Orbital engine/pump with multiple toroidal cylinders
EP2065560A2 (en) 2007-11-30 2009-06-03 MONDL, Fritz Internal combustion engine

Also Published As

Publication number Publication date
HU215194B (en) 1998-10-28
HUT72454A (en) 1996-04-29

Similar Documents

Publication Publication Date Title
CN1074083C (en) Opposed piston combustion engine
US6739307B2 (en) Internal combustion engine and method
US6401686B1 (en) Apparatus using oscillating rotating pistons
CN101205812A (en) Four-piston cylinder engine
US5501182A (en) Peristaltic vane device for engines and pumps
JP2016535193A (en) Internal combustion engine
US6071098A (en) Rotary internal combustion engines
WO1995017582A1 (en) Rotary motion drive, especially for internal combustion engines
EP0851970B1 (en) Rotary internal combustion engines
US20210381377A1 (en) Engine Crank and Connecting Rod Mechanism
RU2477377C2 (en) Internal combustion engine: five-stroke rotary engine with one central rotary gate shared by separate working medium compression and expansion sections, and isolated invariable-volume combustion chambers
EP2268898A1 (en) System for construction of pumps, compressors and rotary engine composed of two rotors with one, two or more displacer&#39;s each, that move themselves in the same direction at speeds that are varying and alternativly opposite each other
CN110546359A (en) mechanism with rotating vanes
CN2287208Y (en) Double rotary piston gasoline engine
CN102011643A (en) Combustion engine
EP0597104A1 (en) Oldham drive engine
WO2002046581A1 (en) Rotary combustion engine
KR20010033874A (en) Method and means for varying piston-in-cylinder motion
RU2109966C1 (en) Piston-type rotary internal-combustion engine
AU735561B2 (en) Rotary internal combustion engines
WO2012166080A1 (en) Multy-cylinder reciprocating rotary engine
WO2022018627A9 (en) Reciprocating mechanism
CN201269135Y (en) Rotary piston type engine
CN114738114A (en) Shuttle type free piston engine with positive and negative screw rods
RU2340782C2 (en) Internal combustion engine

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): CA CN JP US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FR GB GR IE IT LU MC NL PT SE

121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: CA

122 Ep: pct application non-entry in european phase