JPH11303643A - Rotary piston engine and compressor - Google Patents

Abstract

PROBLEM TO BE SOLVED: To obtain a low polution car engine device utilizing both advantages of a recipro type and a rotary type. SOLUTION: In this engine, cylinders 5, 7, and the like are provided in a radial form around a rotor 2 making its rotary shaft as the center, pistons 11, 13, and the like are provided, and, planetary gears 23, 25, and the like are fixed to crankshafts 17, 19, and the like, so as to form a recipro mechanism. A rotary bearing hole is provided to a housing 3, and the suction hole 30; the ignition plug; the exhaust hole 33; the ventilation hole 35; and some other several members; of the stroke mechanisms, are provided on the periphery of the housing 3. A rotary bearing hole is provided to a side housing 4, and a track gear 29 is fixed to the side housing 4. The rotor 2 is assembled in a sandwith form by the housing 3 and the side housing 4. The planetary gears 23, 25, and the like, and the track gear 29 are engaged at the gear number ratio 1:3, and 6 cylinders and 6 strokes are made standard.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a rotary piston engine device which forms a compression mechanism and which is a combination of a reciprocating type and a rotary type.

[0002]

2. Description of the Related Art In automobiles, remarkable progress has been made by high-tech technology, but the basic structure of the engine itself remains unchanged. Therefore, in the conventional reciprocating engine, the structure of the gas exchange between the intake and exhaust is a valve mechanism, so the size, position, number, and heat of the valve. Alternatively, the biggest disadvantage is that gas exchange is significantly impaired because the operation is restricted by the timing of operation. The disadvantages are as follows. , The structure is complicated and expensive. In addition, intake and exhaust are hindered by the restriction of the valve mechanism, resulting in energy loss. In addition, there is an overlap in the opening and closing timings of the valves, resulting in energy loss due to airtight leakage. As a result, the collection of multi-cylinder exhaust pipes causes energy loss due to exhaust interference. , Wankel and rotary engines are said to be lightweight, compact and have a high output, which is advantageous for the practicality of hydrogen engines.However, there is overlap in intake and exhaust, energy loss due to airtightness, poor fuel economy, and low speed torque. It is considered weak.

[0003]

With the increase in the production and the size of automobiles, natural destruction and global warming due to pollution by exhaust gas, especially carbon dioxide, are progressing, and development of low-emission vehicles has become a global urgent issue. . Countermeasures are being taken by stakeholders, and new low-emission vehicles such as battery cars, solar cars, and hydrogen engine cars have been developed. However, there is a problem in price and practicality, and there is currently no significant effect.

[0004] In order to solve the above problems, the present invention provides a simple mechanism and eliminates all the overlaps with valves for intake and exhaust, etc., thereby forming independent processes. The purpose of this device is to develop a new low-emission vehicle engine by making it easier to control the temperature suitable for the vehicle.

[0005]

Means for Solving the Problems A rotating shaft 1 is attached to the rotor.
And fix any number of cylinders 5, 6, 7, 8, 9,
10 (here, six cylinders) are provided, and pistons 11, 12, 13, 14, 15, 16 and crankshafts 17, 18, 19, 20, 21, 22, etc. are provided in a cylinder. At the tip of the crankshaft, planetary gears 23, 24, 25,
26, 27 and 28 are provided. B. A rotary bearing hole is provided in the housing 3, and a suction hole 30, a suction auxiliary groove 31, a spark plug 32, an exhaust hole 33, an exhaust auxiliary groove 34, a ventilation hole 35, a ventilation auxiliary groove 36, and a ventilation valve 3 are provided around the housing 3.
7, a supercharging assist groove 38, a supercharging hole 39, a supercharging valve 39c, a supercharging passage 40, a supercharging passage opening 41 and the like are provided. C: A rotary bearing hole is provided in the side housing 4, and the track gear 29 is fixed and provided. Assemble the D / A rotor in a sandwich with the B housing and the C side housing. E. The ratio of the number of meshing teeth between the planetary gear and the orbital gear is 1: 3
This is a rotary piston engine device based on six cylinders and six processes.

[0006]

Embodiments of the present invention will be described. Among the arbitrary number of embodiments of the present invention, six cylinders and six processes including a basic supercharging process will be described with reference to FIGS. This description will be simply referred to as a basic description.

The six cylinders and six cycles are self-named, and each cycle is defined as a suction, compression, explosion, exhaust, ventilation, and supercharging process. The term “process” mainly refers to the cylinder, and the term “stroke” is distinguished by a name that is based on the crankshaft. As a representative example of the embodiment, FIGS.
2-cylinder 6-stroke engine. Figure 9, 4-cylinder four-step engine device. Figure 10, 6 cylinder two-stage compressor device. FIG. 11, 8-cylinder 8-step expansion process engine device. 12, 13 and 6, there are many such as an engine device with a six-cylinder six-step main crankshaft and the like.

Further, in each figure, since the number of rotors, the number of cylinders, and the ratio of the orbital gear are changed to enable an infinite number of combinations, a description will be given of FIGS. 13 through (0032 to 0058) as representatives of application examples. I do.

The basic outline of the present invention is as follows. A is a rotor having a rotating shaft, B is a housing, and C is a rotor.
As a D, A is assembled with B and C. It is shown like a case by the condition assembled as E.

A basic description of the present invention will now be given. A. A rotating shaft 1 is fixedly provided at the center of a perfect circular disk-shaped rotor 2, and the rotor rotates about the rotating shaft. Six cylinders 5, 6, 7, 8, 9, and 10 are provided radially every 60 degrees around the rotor around the rotation axis. This position is defined by the angles 0, 60, 120, 180, 24
0, 300 degrees, suction, compression, explosion, exhaust, ventilation,
This is the starting point of the supercharging process. (Ventilation leads to scavenging).
Each cylinder has a sleeve and a piston 11, 12, 13,
Also equipped with pins, conlots, etc., including 14, 15, 16
The crankshafts 17, 18, 19, 20, 21, 22 and the like are provided to form a six-step reciprocating mechanism without a valve.
(Note that an eccentric shaft may be used instead of the crankshaft). Planet gears 23, 24, 2 at the tip of the crankshaft
5, 26, 27 and 28 are fixedly provided. (Note that the rotor may be crimped at the dividing line 47 in FIG. 6)

The housing 3 is a mother body that encloses the rotor and is provided with a rotary bearing hole at the center and a gas flow mechanism in each step around the suction hole 3 based on the starting point of each step.
0, suction auxiliary groove 31, spark plug 32, exhaust hole 33, exhaust auxiliary groove 34, ventilation hole 35, ventilation auxiliary groove 36, ventilation valve 3
7, a supercharging assist groove 38, a supercharging hole 39, a supercharging valve 39c, a supercharging passage 40, a supercharging passage opening 41 and the like are provided.

The C side housing 4 is provided with a rotation bearing hole at the center on the side surface surrounding the rotor, and the track gear 29 is fixed and provided so as to mesh with each planetary gear.

The D and A rotors are assembled in a sandwich manner by the B and C side housings, are rotatable, and are fixed while maintaining airtightness.

E: The ratio of the number of meshing teeth of the planetary gear and the orbital gear is set to 1: 3, and a rotary piston engine device is formed based on 6 cylinders and 6 processes. Therefore, if the planetary gear meshes with the orbital gear and goes around the orbit, the planetary gear rotates three times. In other words, three rotations means that the present invention is based on six steps.
Repeat several times. Therefore, suction and compression, explosion and exhaust, ventilation and supercharging steps are formed.

(By changing the meshing ratio, countless processes can be performed as shown in FIGS. 8, 9 and 10 and by sucking and discharging, as shown in FIGS. 8 to 13.)

With the structure described above, with the rotation axis as the center,
Turning the rotor with external force in the direction of the arrow and checking the flow of gas and the operation of each process, the upper direction on the housing 0-0 line is set as the starting point of 0 degree, and the center point of the cylinder 5 is set as the arrow 0 point. Is determined. At a position where the crankshaft 17 becomes the top dead center at 0 degrees and 0 point, the planetary gear 23 and the orbital gear 29 are engaged. In this way, the relationship between the positions and the engagement of all the crankshafts and the planetary gears forms the same movement at the starting point and the zero point. Therefore, at the position of the cylinder 6, starting with the crankshaft 18 at the bottom dead center, FIG.
8, 19, 20, 21, 22 form the same bottom dead center motion.

As described above, every time all the cylinders rotate, they move while forming the same state over 360 degrees. Therefore, the flow of the mixed gas and each operation will be confirmed while changing the current position in FIG.

When the rotor 2 is rotated by an external force in the direction of the arrow about the rotation axis 1, the cylinder 5 rotates the crankshaft 17 at the zero point in the direction of the arrow, and the suction stroke starts. , The air-fuel mixture flows through the suction hole 30 through the suction assist groove 31.
And will fill at the location of the cylinder 6.

At the same time, when the bottom dead center is reached, the suction process ends, and the compression process starts. At the same time, the supercharging auxiliary groove 38 and the supercharging hole 39 in the supercharging process of the cylinder 10, the supercharging passage 40, and the supercharging passage opening 4.
1 is connected at the position of the cylinder 6. At the same time, the mixture of the outside air and the exhaust gas is compressed by the cylinder 10, and a larger amount of the mixed gas than the volume of the suction process fills the position of the cylinder 6 as a compression body. The pressure is adjusted at 39c.

The cylinder 5 comes to the position of the cylinder 6,
The filled cylinder undergoes a further compression step. At the position of the cylinder 7, an ignition explosion is caused by the spark plug 32, and the crankshaft 17 receives explosion energy and goes around the explosion stroke. Further, the cylinder 5 gives rotational energy to the rotor 2 by the planetary gear 23 of the crankshaft 17, and at the position of the cylinder 8, becomes exhaust gas through the exhaust hole 33 and is discharged to the atmosphere. (It is the engine device with an expansion step shown in FIG. 11 that is provided with an expansion step before discharge and separates the high-pressure gas.)

The exhaust hole 33 is connected to the exhaust auxiliary groove 34, the ventilation hole 35, the ventilation auxiliary groove 36, and the ventilation valve 37. When the cylinder 5 proceeds to the exhaust process of the cylinder 8, the position of each cylinder and the operation state are checked.

The cylinder 6 is in the process of ventilating the cylinder 9. Without exploding without a mixture,
The compression process, the explosion process, and the exhaust process are rotated by an external force, and the outside air is about to be sucked from the ventilation hole 35 through the exhaust auxiliary groove 34 and simultaneously with the exhaust body of the cylinder 5.

It is to be noted that the ventilation valves 37 and 37a and the supercharging valve 3 generally control the intake and exhaust of the exhaust body.
9c. Both valves are partially cut off with circular rotary valves. The circular part is connected to the rotor 2 and is held by the housing and the side housing. The supercharging valve keeps airtight and regulates the supercharging pressure.

The cylinder 7 is in the process of supercharging the cylinder 10. The explosion process, the exhaust process, and the ventilation process are rotated by external force, and the external air is sucked in to reduce the supercharging in the supercharging process.

The cylinder 8 is proceeding to the starting point suction step of the cylinder 5. It turns around the ventilation process by external force, inhales the outside air, performs supercharging compression in the supercharging process of the cylinder 10, holds the compressed body in the supercharging path 40, and sucks the air-fuel mixture in the suction process. waiting.

The cylinder 9 is proceeding to the cylinder 6 compression step. The air-fuel mixture is sucked in the suction process, and the supercharging pressure is maintained in the supercharging process to receive the supercharged air from the supercharging path.

The cylinder 10 is in the process of exploding the cylinder 7. In the inhalation process, the air-fuel mixture is inhaled in the inhalation process, and in the compression process, the supercharged air is also received from the supercharging port. Waiting for ignition.

In such a position and situation, the cylinder 5
Goes to the exhausting process of the cylinder 8, and at the moment when the piston 11 of the cylinder 5 moves by inertia from the starting point of the exhausting process, the piston 16 of the cylinder 10 waiting for ignition in the explosion process.
Receives the explosion energy by the spark plug 32, rotates the crankshaft 22, and the planetary gear 28
9 rotates the rotor in the direction of the arrow in response to the rotational energy of the reaction.

Subsequently, the piston 15 of the cylinder 9 which is proceeding to the compression process receives the explosion energy, rotates the crankshaft 21, and the planetary gear 27 changes to the orbital gear 29.
Thus, the rotor receives the rotational energy of the reaction and rotates the rotor in the direction of the arrow.

In this way, the explosion started from the cylinder 5 in succession with the cylinder 5, followed by the cylinders 10, 9, 8, and 7, followed by another rotation of the rotor after returning to the starting point of the cylinder 5 gas. Explosions from cylinders 6, 5,
It becomes permanent by repeating interlocking with 10, 9, 8, 7, 6, and 5.

According to the present invention, when the rotor is 6
For every 0 degree rotation, each crankshaft rotates 60 degrees and 18
Orbit for one week in three revolutions while rotating at 0 degree. Therefore, the present invention has achieved the object without any valve for gas exchange, each step is independent, and there is no overlap. A rotary piston characterized by a six-cylinder, six-step meshing gear ratio of 1: 3, in which six cylinders form six steps each time the rotor makes one revolution, thereby generating six rotations. It is an engine device. (The curved arrow indicates the rotation direction, and the short arrow indicates the fluid direction.)

[0032]

[Case 2] As shown in FIG. 8, a 12-cylinder 6-process engine device is described, although it is the same as the basic description. A. A rotating shaft is fixedly provided at the center of the rotor 2 having a perfect circle and a disk shape. The rotor rotates about a rotation axis. Twelve cylinders 5, around the rotor, around the rotor,
6, 7, 8, 9, 10, 5a, 6a, 7a, 8a, 9
a and 10a are provided radially every 30 degrees. This position is defined by the angles 0, 30, 60, 90, 120, 150, 180, 2
10, 240, 270, 300, and 330 degrees are the starting points of the suction, compression, explosion, exhaust, ventilation, supercharging, suction, compression, explosion, exhaust, ventilation, and supercharging steps. Sleeves and pistons 11, 12, 13, 14, 1 for each cylinder
5, 16, 11a, 12a, 13a, 14a, 15a,
16a as well as pins, con-lots, etc., and crankshafts 17, 18, 19, 20, 21, 22, 17a, 18
A, 19a, 20a, 21a, 22a, etc. are provided to form a six-step reciprocating mechanism without a valve. The planetary gears 23, 24, 25, 26, 27,
28, 23a, 24a, 25a, 26a, 27a, 28
a is fixedly provided.

B. The housing 3 is a base body surrounding the rotor and has a rotary bearing hole at the center, and a gas flow mechanism in each step around the suction hole 3 based on the starting point of each step.
0, 30a, suction assist grooves 31, 31a, spark plug 32,
32a, exhaust holes 33, 33a, exhaust auxiliary grooves 34, 34a,
Ventilation holes 35, 35a, ventilation auxiliary grooves 36, 36a, ventilation valves 37, 37a, supercharging auxiliary grooves 38, 38a, supercharging holes 39,
39a, supercharge roads 40, 40a, supercharge road openings 41, 41a, etc. are provided.

The side housing 4 is provided with a rotation bearing hole at the center on the side surface enclosing the rotor, and the track gear 29 is fixed so as to mesh with each planetary gear.

The D and A rotors are assembled in a sandwich manner by the B and C side housings, and are rotatably fixed while maintaining airtightness.

E. The ratio of the number of meshing teeth between each planetary gear and the orbital gear is set to 1: 6, and 6 steps for 12 cylinders are performed simultaneously.
It is a rotary piston engine device characterized by being formed in places. Therefore, if the planetary gears mesh with the orbital gears and move the orbit for one week, each planetary gear will rotate six times. Therefore, the present invention forms 12 cylinders at the same time in two places, suction, compression, explosion, exhaust, ventilation, supercharging process,
The spark plugs 32 and 32a ignite and explode at the same time,
It is a rotary piston engine device that generates explosive energy for one time. (The details conform to the basic explanation).

[0037]

[Case 3] As shown in FIG. 9, the description of the four-cylinder four-process engine device is the same as the basic description, though it is the same. A. A rotating shaft is fixedly provided at the center of the rotor 2 having a perfect circle and a disk shape.
The rotor rotates about a rotation axis. Four cylinders 5, 6, around the rotor around the rotation axis
7, 8 are provided radially every 90 degrees. This position is defined as angles 0, 90, 180, and 270 degrees, which are the starting points of the suction, compression, explosion, and exhaust processes. Each cylinder is provided with sleeves and pistons 11, 12, 13, 14 as well as pins, con-lots, etc., and crankshafts 17, 18, 19, 20 and the like are provided to form a four-step reciprocating mechanism without valves. At the tip of the crankshaft, planetary gears 23, 24, 25,
26 is fixedly provided.

The housing 3 is a mother body surrounding the rotor and has a rotary bearing hole at the center, and a gas flow mechanism at each step around the suction hole 3 based on the starting point of each step.
0, suction auxiliary groove 31, spark plug 32, exhaust hole 33, exhaust auxiliary groove 34, ventilation valve 37, supercharging hole 39, supercharging passage 40,
The supercharging way 41 etc. are made.

The side housing 4 is provided with a rotary bearing hole at the center on the side surface enclosing the rotor to fix the orbital gear 29 so as to mesh with each planetary gear.

The D and A rotors are assembled in a sandwich manner by the B and C side housings, and are rotatably fixed while maintaining airtightness.

E. This is a rotary piston engine apparatus characterized in that the ratio of the number of meshing teeth between each planetary gear and the orbital gear is 1: 2, and four steps are performed in four cylinders. Therefore, if the planetary gears mesh with the orbital gears and move the orbit for one week, each planetary gear will make two revolutions. Therefore, the present invention is a rotary piston engine device that forms a supercharging process simultaneously with inhalation, compression, explosion, and exhaustion, ignites and explodes with a spark plug 32, and generates four explosion energies. (still,
Details follow the basic description).

[0042]

[Case 4] As shown in FIG. 10, a 6-cylinder two-stage compression apparatus will be described although it overlaps the basic description. Note that the basic description is replaced with a compression device. A. A rotating shaft is fixedly provided at the center of the rotor 2 having a perfect circle and a disk shape. The rotor rotates about a rotation axis. Six cylinders 5, 6, 7, around the rotor around the rotation axis
8, 9, and 10 are provided radially every 60 degrees. This position is defined as angles 0, 60, 120, 180, 240, and 300 degrees, and is set as the starting point of the suction, compression, suction, compression, suction, and compression processes. Each cylinder has a sleeve and a piston 11, 12,
13, 14, 15, 16 as well as pins, con-lots and the like, and crankshafts 17, 18, 19, 20, 21, 22
And the like to form a two-step reciprocating mechanism without a valve. Planet gears 23, 24, 2 at the tip of the crankshaft
5, 26, 27 and 28 are fixedly provided.

B. The housing 3 is a base body surrounding the rotor and provided with a rotary bearing hole at the center, and a gas flow mechanism in each step around the suction hole 3 based on the starting point of each step.
0, 30a, 30b suction assist grooves 31, 31a, 31b exhaust holes 33, 33a, 33b exhaust assist grooves 34 34a 34b
Etc.

C. The side housing 4 is provided with a rotary bearing hole at the center on the side surface surrounding the rotor, and the track gear 29 is fixed so as to mesh with each planetary gear.

The D and A rotors are assembled in a sandwich manner with the B and C side housings, and are rotatably fixed while maintaining airtightness.

E. The ratio of the number of meshing teeth between each planetary gear and the orbital gear is 1: 3, and a rotor-piston compression apparatus characterized by two steps of six cylinders is formed. Therefore, if the planetary gears mesh with the orbital gears and move the orbit for one week, each planetary gear will rotate three times. Therefore, according to the present invention, by rotating by external force, inhalation and exhalation are repeated three times,
This is a rotor-piston compression device that generates compression energy by performing compression, suction, compression, suction, and compression steps three times. (The details conform to the basic explanation).

[0047]

[Case 5] An eight-cylinder eight-process engine device as shown in FIG. A. A rotating shaft is fixedly provided at the center of the rotor 2 having a perfect circle and a disk shape. The rotor rotates about a rotation axis. Eight cylinders 5 around the rotor around the rotation axis,
6, 7, 8, 9, 10, 10a, and 10b are provided radially every 45 degrees. This position is defined by the angles 0, 45, 90, 13
5, 180, 125, 270, 315 degrees, inhalation,
It is the starting point of the compression, explosion, exhaust, expansion, exhaust, expansion, and exhaust processes. Sleeve and piston 11, 1 for each cylinder
2, 13, 14, 15, 16, 16a, 16b as well as pins, con-lots, etc.
By providing 9, 20, 21, 22, 22a, 22b, etc., an eight-step reciprocating mechanism without a valve is formed. The planetary gears 23, 24, 25, 26, 27,
28, 28a and 28b are fixedly provided.

B. The housing 3 is a base body surrounding the rotor and provided with a rotary bearing hole at the center, and a gas flow mechanism for each step around the suction hole 3 based on the starting point of each step.
0, suction assist groove 31, spark plug 32, exhaust holes 33, 33
a, 33b exhaust auxiliary grooves 34, 34a34b, ventilation valve 3
7b, a supercharging hole 39, a supercharging path 40, a supercharging path 41, and expansion holes 42, 43, 44, expansion paths 45, 46, etc. are formed.

The side housing 4 is provided with a rotation bearing hole at the center on the side surface enclosing the rotor, and the track gear 29 is fixed and provided so as to mesh with each planetary gear.

The D and A rotors are assembled in a sandwich manner by the B and C side housings, and are rotatably fixed while maintaining airtightness.

E. This is a rotary piston engine apparatus characterized in that the ratio of the number of meshing teeth between each planetary gear and the orbital gear is 1: 4, and eight cylinders and eight processes are provided. Therefore, if the planetary gears mesh with the orbital gears and move the orbit for one week, each planetary gear will rotate four times. When the cylinder 7 receives explosive energy from the spark plug 32 at a rotor angle of 90 degrees and advances to near 105 degrees, the expansion holes 42, 43, 4
4 and the expansion passages 45, 46, the cylinders 7, 9, 10
a is connected and the explosion pressure is reduced to 3
By exhausting by 3, 33a, 33b, exhaust interference is reduced and low-speed torque is increased. Therefore, the present invention relates to inhalation,
This is a rotary piston engine device that generates compression, explosion, expansion, expansion and exhaust simultaneously in three steps, ignites and explodes with a spark plug 32, and generates eight explosion energies. (The details conform to the basic explanation).

[0052]

[Case 6] An engine device with a 6-cylinder, 6-step main crank as shown in FIGS. A. A hollow rotor shaft 51, 51c is provided at the center of a perfect circular disk-shaped rotor 2. The rotor rotates about the rotor axis. Six cylinders 5, 6, 7c, 8, around the rotor around the rotation axis
9 and 10c are provided radially every 60 degrees. The positions are defined as angles 0, 60, 120, 180, 240, 300, and degrees, and are the starting points of the suction, compression, explosion, exhaust, ventilation, and supercharging processes. Sleeve and piston 11, 1 for each cylinder
2, 13c, 14, 15, 16c as well as pins, con-lots, etc., and crankshafts 17, 18, 20, 21, etc. are provided, and planetary gears 23, 24, 2,
6, 27 are fixedly provided. The main crankshaft 52 is rotatably provided in the hollow of the rotor shaft, and the large bay portion is provided by sliding the two divided slots 54 and 55 so that the small gear 50 is fixed to the tip of the main crankshaft.

The housing 3 is a base body surrounding the rotor, and has a rotor bearing hole at the center thereof. The gas flow mechanism of each process is formed around the suction hole 30, the suction assist groove 31, based on the starting point of each process. Spark plug 32, exhaust hole 33, exhaust auxiliary groove 34, ventilation hole 35, ventilation auxiliary groove 36, ventilation valve 3
7, supercharging assist groove 38c, supercharging hole 39, supercharging valve 39c,
A supercharged road 40, a supercharged road opening 41 and the like are provided. A counter house 3c is provided on the side of the housing, and counter gears are arranged.

The side housing 4 is provided with a rotor bearing hole at the center on the side surface enclosing the rotor.
9 is fixed and provided so as to mesh with each planetary gear.

The D. counter house 3c sets the rotation ratio between the main crankshaft 52 and the rotor shaft 51 to 3: 1, that is, the gear ratio of the planetary gears to the orbital gears is 1: 3. It is a ratio combination mechanism for making the same as one. A large gear 60 is provided on the rotor shaft 51 and a small gear 50 is fixed on the main crankshaft 52. The gear ratio of the large gear to the small gear is 3 to 2. Counter shaft 53
The small gear 50c and the large gear 60c are fixed to the large gear 60 and the small gear 50c.
0 is engaged. Therefore, the rotation ratio of the rotor shaft to the main crankshaft is 1: 3.

The side housing 4c has a main crank bearing hole at the center on the side surface surrounding the counter house 3c and a counter gear bearing hole on the side surface.

The F / A rotor is assembled in a sandwich manner by the B housing and the C side housing, and the D counter house is sandwiched by the E side housing.

G. The ratio of the number of meshing teeth between each planetary gear and the orbital gear is 1: 3. The rotary piston engine device is characterized by having six cylinders and six processes, with a main crankshaft and a two-part con-lot. Therefore the cylinder 7c,
10c pistons 13c and 16c are
5, the rotor is rotated while applying explosive energy linearly to the main crankshaft 52 from a diagonal direction of 180 degrees, and is resistant to low-speed torque generated in conjunction with the energy together with the piston mechanism of each cylinder. (still,
Details follow the basic description).

[0059]

A. Since the structure is simple, a multi-step mechanism can be freely obtained. Since the process is independent, multiple cycles such as ventilation, expansion, and supercharging processes and the free design of the combustion chamber can be obtained.
Since there are no intake and exhaust valves, there is no restriction or hindrance to the exchange gas system. Not subject to restrictions such as surging and bursting. B. The performance, characteristics, and the process are independent, so that temperature control suitable for the process can be easily obtained, resulting in low pollution, high fuel efficiency, high torque, and high horsepower. No energy loss due to no overlap between processes. Energy loss due to exhaust interference in the exhaust stack is small. Low torque fluctuation due to continuous rotation energy generation by multi-step mechanism. C, simple structure, light weight, compact, low pollution, high fuel efficiency, high torque, high horsepower.

[0060]

[Brief description of the drawings]

FIG. 1 is a front perspective view of a section AA of the present invention.

FIG. 2 is a front view of the present invention.

FIG. 3 is a sectional view taken along line BB of the front view of the present invention.

FIG. 4 is a sectional view taken along the line CC of the front view of the present invention.

FIG. 5 is a sectional view taken along line DD of the front view of the present invention.

FIG. 6 is a sectional view taken along line EE of the front view of the present invention.

7 is a front sectional view of FIG. 2 along the line FF of FIG. 3 of the present invention.

FIG. 8 is a front sectional view taken along line FF of FIG. 3 of the present invention from FIG.

FIG. 9: Cases 3 and 4 cylinders. FIG. 8 is a front sectional view taken along line FF of FIG. 3 of the present invention from FIG. 7.

FIG. 10 Cases 4, 6 cylinders. FIG. 8 is a front sectional view taken along line FF of FIG. 3 of the present invention from FIG. 7.

FIG. 11: Case 5, 8 cylinders. FIG. 8 is a front sectional view taken along line FF of FIG. 3 of the present invention from FIG. 7.

FIG. 12: Case 6, 6 cylinders. FIG. 8 is a front sectional view taken along line FF of FIG. 3 of the present invention from FIG. 7.

FIG. 13: Case 6, 6 cylinders. FIG. 12 is a cross-sectional view of FIG. 12 taken along the line DD in FIG.

[0061]

[Brief description of reference numerals]

1 rotating shaft 31, 31
a, 31b Suction aid groove 2 Rotor 32, 32a
Spark plug 3 Housing 33, 33
a, 33b Exhaust hole 4, 4c Side housing 34, 34
a, 34b Exhaust auxiliary groove 5, 5a Cylinder 35, 35a
Ventilation hole 6, 6a Cylinder 36, 36a
Ventilation aid groove 7, 7a, 7c Cylinder 37, 37a
Ventilation valve 8, 8a Cylinder 38, 38
a, 38c Supercharging aid groove 9, 9a Cylinder 39, 39a
Supercharging hole 10, 10a, 10b, 10c Cylinder 40, 40
a Supercharged road 11, 11a Piston 41, 41
a Supercharging port 12, 12a Piston 42 Inflated pore 13, 13a, 13b, 13c Piston 43 Inflated pore 14, 14a Piston 44 Inflated pore 15, 15a Piston 45 Inflated path 16, 16a, 16b, 16c Piston 46 Inflated passage 17, 17a Crankshaft 47 Parting line 18, 18a Crankshaft 19, 19a Crankshaft 50, 50
small gear 20, 20a crankshaft 51, 51
c rotor shaft 21, 21a crankshaft 52 main crankshaft 22, 22a, 22b crankshaft 53 counter shaft 23, 23a planetary gear 54 split conrot 24, 24a planetary gear 55 split conlot 25, 25a planetary gear 60, 60
c Large gear 26, 26a Planetary gear 27, 27a Planetary gear 3c Counter house 28, 28a, 28b Planetary gear 39c Supercharging valve 29 Orbital gear 30, 30a, 30b Suction hole

Claims (6)

[Claims] 1. A rotating shaft (1) is fixed to a rotor (2) and an arbitrary number of cylinders (5, 6, 7, 8, 9, 1) are fixed.
0) and pistons (11, 12, 1
3, 14, 15, 16) and crankshafts (17, 18, 1)
9, 20, 21, 22) and the like, and planetary gears (23, 24, 25, 26, 27, 28) at the tip of the crankshaft. B. A rotary bearing hole is provided in the housing (3), and a suction hole (30) a suction auxiliary groove (31) a spark plug (32) an exhaust hole (33) an exhaust auxiliary groove (34) a ventilation hole (35) a ventilation auxiliary groove around the rotation bearing hole. (36) Ventilation valve (37) Supercharging assist groove (38) Supercharging hole (39) Supercharging valve (39c) Supercharging path (40) Supercharging port (41) and the like are provided. C. A rotary bearing hole is provided in the side housing (4), and the track gear (29) is fixedly provided. Assemble the DA rotor with the B housing and the C side housing in a sandwich manner. E-Rotary piston engine device based on a 6-cylinder 6-stroke process with a ratio of the number of meshing teeth of the planetary gear and the orbital gear of 1: 3. 2. As shown in FIG. 8, a rotating shaft (1) is fixed to an A rotor (2), and cylinders (5, 6, 7, 8,
9, 10, 5a, 6a, 7a, 8a, 9a, 10a), and pistons (11, 12, 13, 1
4, 15, 16, 11a, 12a, 13a, 14a, 1
5a, 16a) and crankshafts (17, 18, 19, 2)
0, 21, 22, 17a, 18a, 19a, 20a, 2
1a, 22a) and the like, and planetary gears (23, 24, 25, 26, 27, 28, 23a, 2a,
4a, 25a, 26a, 27a, 28a) are provided. B. A rotary bearing hole is provided in the housing (3), and suction holes (30, 30a) suction assist grooves (31, 31a) ignition plugs (32, 32a) exhaust holes (33, 33a) exhaust assist grooves (34, 34a) ventilation holes (35, 35a) ventilation auxiliary grooves (3
6, 36a) Ventilation valve (37, 37a)
8, 38a) Supercharging holes (39, 39a) Supercharging roads (40, 4)
0a) Provide supercharging entrances (41, 41a). C. A rotary bearing hole is provided in the side housing (4), and the track gear (29) is fixedly provided. Assemble the DA rotor with the B housing and the C side housing in a sandwich manner. 2. The rotary piston engine apparatus according to claim 1, wherein the ratio of the number of meshing teeth between the planetary gear and the orbital gear is 1 to 6, and the number of processes is 12 in 6 cylinders. 3. As shown in FIG. 9, a rotary shaft (1) is fixed to an A rotor (2), cylinders (5, 6, 7, 8) are provided, and pistons (11, 12, 13, 1
4) and crankshafts (17, 18, 19, 20), etc., and planetary gears (23, 24, 2) at the tip of the crankshaft.
5, 26) are provided. B. A rotary bearing hole is provided in the housing (3), and a suction hole (30) a suction auxiliary groove (31) a spark plug (32) an exhaust hole (33) an exhaust auxiliary groove (34) a ventilation valve (37) a supercharging hole around the housing. (39) Supercharge road (40) Provide supercharge road entrance (41). C. A rotary bearing hole is provided in the side housing (4), and the track gear (29) is fixedly provided. Assemble the DA rotor with the B housing and the C side housing in a sandwich manner. 2. The rotary piston engine device according to claim 1, wherein the ratio of the number of meshing teeth between the planetary gear and the orbital gear is 1: 2, and four cylinders and four processes are used. 4. As shown in FIG. 10, a rotating shaft is fixed to an A rotor (2), and cylinders (5, 6, 7, 8, 9, 1) are fixed.
0) and pistons (11, 12, 1
3, 14, 15, 16) and crankshafts (17, 18, 1)
9, 20, 21, 22) and the like, and a track gear (23, 24, 25, 26, 27, 28) is provided at the tip of the crankshaft. B. A rotary bearing hole is provided in the housing (3), and suction holes (30, 30a, 30b) and suction auxiliary grooves (31, 31) are provided around the housing.
a, 31b) Exhaust holes (33, 33a, 33b), exhaust auxiliary grooves (34, 34a, 34b) and the like are provided. C. A rotary bearing hole is provided in the side housing (4), and the track gear (29) is fixedly provided. Assemble the DA rotor with the B housing and the C side housing in a sandwich manner. E. A rotary piston compression apparatus characterized in that the ratio of the number of meshing teeth between the planetary gear and the orbital gear is 1: 3, and the case of two processes of six cylinders. 5. As shown in FIG. 11, a rotating shaft is fixed to an A rotor (2) and cylinders (5, 6, 7, 8, 9, 1) are fixed.
0, 10a, 10b) and pistons (11, 12, 13, 14, 15, 16, 16a, 16
b) and the crankshaft (17, 18, 19, 20, 21, 2)
2, 22a, 22b) and the like, and orbital gears (23, 24, 25, 26, 27, 28, 28) are provided at the tip of the crankshaft.
a, 28b) and the like. B. A rotary bearing hole is provided in the housing (3), and a suction hole (30) suction assist groove (31) spark plug (32) exhaust hole (33, 33a, 33b) exhaust assist groove (34, 34a,
34b) Ventilation valve (37b) Supercharged air hole (39) Supercharged airway (40) Supercharged airway opening (41) Inflated airhole (42, 43, 4)
4) Provide inflated airways (45, 46) and the like. C. A rotary bearing hole is provided in the side housing (4), and the track gear (29) is fixedly provided. Assemble the DA rotor with the B housing and the C side housing in a sandwich manner. 2. The rotary piston engine device according to claim 1, wherein the ratio of the number of meshing teeth of the planetary gear and the orbital gear is 1: 4, and the expansion process is performed in eight cylinders and eight processes. 6. As shown in FIGS. 12 and 13, the A rotor (2) is provided with a rotor shaft (51, 51c) and a cylinder (5, 51).
6, 7c, 8, 9, 10c) pistons (11, 12, 1)
3c, 14, 15, 16c) crankshafts (17, 18,
20, 21), etc., and planetary gears (23, 24, 26, 27) are provided at the tip of the crankshaft. At the center of the rotor shaft, the main crankshaft (52)
4, 55) are provided. B. A rotor bearing hole is provided in the housing (3), and a suction hole (30) a suction assist groove (31) and a spark plug (32) are provided around the rotor bearing hole.
Exhaust hole (33) Exhaust auxiliary groove (34) Ventilation hole (35) Ventilation auxiliary groove (36) Ventilation valve (37) Supercharge auxiliary groove (38c) Supercharge hole (39) Supercharge valve (39c) Supercharge path ( 40) A supercharging entrance (41) is provided. A counter house (3c) is provided on the side. C. A rotor bearing hole is provided in the side housing (4), and the track gear (29) is fixedly provided. In the D. counter house (3c), a large rotor gear (60) is fixed to the tip of the rotor shaft (51), and a small main crank gear (50) is fixed to the main crank shaft (52). A small counter gear (50c) and a large counter gear (60c) are fixedly provided. E. Provide a main crank bearing hole and a counter bearing hole in the side housing (4c). Assemble the rotors of FA and A in a sandwich shape with the housing of B and the side housing of C, and the counter house of D with the side housing of E. The ratio of the number of meshing teeth of G / planetary gear to orbital gear, small main crank gear / large rotor gear is 1: 3,
2. The rotary piston engine apparatus according to claim 1, wherein the rotary piston engine apparatus has six cylinders and six strokes, and includes a main crankshaft and a two-part conlot.