WO2020060500A1 - Rotary engine - Google Patents
Rotary engine Download PDFInfo
- Publication number
- WO2020060500A1 WO2020060500A1 PCT/TR2018/000093 TR2018000093W WO2020060500A1 WO 2020060500 A1 WO2020060500 A1 WO 2020060500A1 TR 2018000093 W TR2018000093 W TR 2018000093W WO 2020060500 A1 WO2020060500 A1 WO 2020060500A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- combustion chamber
- rotary engine
- engine according
- combustion
- combustion chambers
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C9/00—Oscillating-piston machines or engines
- F01C9/007—Oscillating-piston machines or engines the points of the moving element describing approximately an alternating movement in axial direction with respect to the other element
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/02—Pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/14—Shapes or constructions of combustion chambers
-
- 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
- F01C1/08—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to a rotary engine, which is for use in the internal combustion engines and which comprises two or more than two combustion chambers.
- the engines operate based on the principle of self-ignition of the fuel injected into the air, which is compressed and the pressure and temperature of which are increased. Accordingly, the conversion of heat into the work occurs in the following way.
- the clean air gets sucked or filled into the engine cylinders.
- the pressure of the air compressed by a piston is in the range of about 30-40 kg/cm2 and the temperature thereof is in the range of about 400-600°.
- the combustion follows the ignition and the gases with a pressure in the range of 40-80 kg/cm and a temperature in the range of 400-600° are formed.
- These hot gases with high pressure transfer the work to the crankshaft with the help of a piston and a piston rod (connecting rod).
- Described herein is a rotary engine capable of providing a solution for the drawbacks of the engines of the prior art, which involve the exhaust and intake processes being performed at different times according to the operating principles thereof, i.e. the drawbacks arising from the inability to transfer all the power due to the crankshaft angle of 720° and from the high fuel consumption.
- An object of the present invention is to realize a rotary engine, which enables the exhaust and compression to take place simultaneously and the intake and ignition to take place simultaneously and which will be able to provide a solution for the high fuel consumption of the other engines.
- part 1 a- Shaft shaped interior section of part 1
- the rotary engine according to the invention ( Figure le) comprises a part 1 ( 1 ) in the form of a single-piece with a cylinder shaped exterior section (lc), a cylinder shaped central section (l b) and a shaft shaped interior section (la).
- the cylindrical part 2 (2) of the rotary engine according to the invention is able to overlap with the central section (lb) of the part 1 (1) ( Figure 2a).
- the combustion chamber (6) includes the intake manifold (3a), the exhaust manifold (4a) and the ignition unit (5a) and the combustion chamber (7) located on the other side includes the intake manifold (3b), the exhaust manifold (4b) and the ignition unit (5b), wherein the combustion chamber (6) and the combustion chamber (7) are disposed opposite one another on two sides of the rotary engine ( Figure 3a, Figure 4a).
- Figures 2a-2k schematically illustrate the operating principle of the combustion chamber (6) present in the rotary engine according to the invention.
- the intake stroke occurs in the combustion chamber (6) upon the motion of the part 2 (2) in the direction of the arrow. Said intake process continues until Figure 2g and after this motion, the sucked air and fuel begin to be compressed ( Figure 2h) and the compressed air and fuel are stored in the air and fuel storage area (8) of the combustion chamber (6) ( Figure 2k).
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
The subject of the invention is a rotary engine consisting of 2 parts (Figure le), wherein said rotary engine comprises the part 1 (1) in the form of a single-piece with a shaft shaped interior section (la), a cylinder shaped central section (lb) and a cylinder shaped exterior section (lc), and a cylindrical part 2 (2). 2 or more than 2 combustion chambers (Figure lg) are arranged in a leakproof manner where the part 2 (2) rotates at the central section of the part 1 (1) and where said combustion chambers each comprise the respective intake manifold, exhaust manifold and ignition unit.
Description
ROTARY ENGINE
Relevant Technical Field
The present invention relates to a rotary engine, which is for use in the internal combustion engines and which comprises two or more than two combustion chambers.
Prior Art
The engines operate based on the principle of self-ignition of the fuel injected into the air, which is compressed and the pressure and temperature of which are increased. Accordingly, the conversion of heat into the work occurs in the following way. First, the clean air gets sucked or filled into the engine cylinders. The pressure of the air compressed by a piston is in the range of about 30-40 kg/cm2 and the temperature thereof is in the range of about 400-600°. Thus, the combustion follows the ignition and the gases with a pressure in the range of 40-80 kg/cm and a temperature in the range of 400-600° are formed. These hot gases with high pressure transfer the work to the crankshaft with the help of a piston and a piston rod (connecting rod). While this is happening, a great portion of the heat energy that is generated upon the combustion of the fuel is converted into the mechanical energy, which enables the crankshaft to rotate. The crankshaft enables the generation of the electrical energy by utilizing the rotary motion transmitted to it to rotate the rotor of the alternator. At the end of the work stroke, the gases the pressure and temperature of which have decreased are exhausted into the atmosphere and the step of filling the clean air into the cylinders is repeated for a new cycle.
Described herein is a rotary engine capable of providing a solution for the drawbacks of the engines of the prior art, which involve the exhaust and intake processes being performed at different times according to the operating principles thereof, i.e. the drawbacks arising from the inability to transfer all the power due to the crankshaft angle of 720° and from the high fuel consumption.
Object of the Invention
An object of the present invention is to realize a rotary engine, which enables the exhaust and compression to take place simultaneously and the intake and ignition to take place simultaneously and which will be able to provide a solution for the high fuel consumption of the other engines.
Description of the Invention
The combustion chambers realized to achieve the object of the present invention are illustrated in the appended figures in which: Figures l a-lg, 2a-2k, 3a-3f and 4a-4f are the schematic views of the operating principle of the rotary engine according to the invention.
The parts on the figures are individually assigned with reference numerals and the designations of said reference numerals are provided below.
1 - Part 1
2- Part 2
1 a- Shaft shaped interior section of part 1
lb- Cylinder shaped central section of part 1
lc- Cylinder shaped exterior section of part 1
3a- Intake manifold of combustion chamber (6)
4a- Exhaust manifold of combustion chamber (6)
5a- Ignition unit of combustion chamber (6)
3b- Intake manifold of combustion chamber (7)
4b- Exhaust manifold of combustion chamber (7)
5b- Ignition unit of combustion chamber (7)
6- lsl combustion chamber
7- 2K combustion chamber
8- Air and fuel storage area
The rotary engine according to the invention (Figure le) comprises a part 1 ( 1 ) in the form of a single-piece with a cylinder shaped exterior section (lc), a cylinder shaped central section (l b) and a shaft shaped interior section (la).
The cylindrical part 2 (2) of the rotary engine according to the invention is able to overlap with the central section (lb) of the part 1 (1) (Figure 2a).
When the part 2 (2) moves in the direction of the arrow, the combustion chamber (6) (Figure 3a) and the combustion chamber (7) (Figure 4a) appear. The combustion chamber (6) includes the intake manifold (3a), the exhaust manifold (4a) and the ignition unit (5a) and the combustion chamber (7) located on the other side includes the intake manifold (3b), the exhaust manifold (4b) and the ignition unit (5b), wherein the combustion chamber (6) and the combustion chamber (7) are disposed opposite one another on two sides of the rotary engine (Figure 3a, Figure 4a). Figures 2a-2k schematically illustrate the operating principle of the combustion chamber (6) present in the rotary engine according to the invention. Referring to the work stroke of the combustion chamber (6) in Figure 2b, the intake stroke occurs in the combustion chamber (6) upon the motion of the part 2 (2) in the direction of the arrow. Said intake process continues until Figure 2g and after this motion, the sucked air and fuel begin to be compressed (Figure 2h) and the compressed air and fuel are stored in the air and fuel storage area (8) of the combustion chamber (6) (Figure 2k).
At this point, the part 2 (2) is pushed in the direction of the arrow by means of the pressure that has developed as a result of the combustion taking place in the combustion chamber (6) (Figure 3a).
Owing to this motion, the intake process is caused to occur in the combustion chamber (7) on the other side (Figure 4a). Throughout this motion, the combustion continues in the combustion chamber (6) (Figures 3a-3d) and the intake process continues in the combustion chamber (7) (Figures 4a-4d). As a result of this motion, the exhaust is stored in the combustion chamber (6) (Figure 3d) and the sucked fuel is stored in the combustion chamber (7) (Figure 4d).
The continuation of this motion in this direction causes the discharge of the exhaust in the combustion chamber (6) (Figure 3e) and the compression of the sucked fuel in the combustion chamber (7) (Figure 4e). As a result of the process, the exhaust has been discharged from the combustion chamber (6) (Figure 3f) and the sucked fuel has been compressed and stored in the air and fuel storage area (8) of the combustion chamber (7) (Figure 4f),
As the continuation of this motion, the work stroke intake process is carried out in the combustion chamber (6), while the ignition and the generation of the pressure and power are performed in the combustion chamber (7) on the other side.
Owing to the facts that, in the rotary engine according to the invention a cycle of which has been described above, the intake and ignition take place simultaneously and the compression and exhaust take place simultaneously, the process continues without any stopping being required and the operation takes place without any greater extent of motion being necessary with respect to the 4-stroke engines, the rotary engine according to the invention will be able to provide solutions for the problems in the other engines. Consequently, with the rotary engine according to the invention, more power may be generated as compared to the 4-stroke cylinders. Some of the preferred embodiments of the rotary engine according to the invention are illustrated in the enclosed drawings, which are not intended to limit the invention.
Claims
1- A rotary engine characterized by a leakproof arrangement where a cylindrical part 2 (2) is able to move at the central section of a part 1 (1).
2- A rotary engine according to Claim 1 characterized by the combustion chambers (6 and 7) disposed in a leakproof manner resulting when the part 2 (2) moves at the central section of the part 1 (1).
3- A rotary engine according to Claim 1 characterized by the combustion chamber (6) and the combustion chamber (7) and the respective intake manifold, exhaust manifold and ignition unit disposed in each of said combustion chambers.
4- A rotary engine according to Claim 1 characterized by 2 or more than 2 combustion chambers as shown in Figure lg.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/TR2018/000093 WO2020060500A1 (en) | 2018-09-18 | 2018-09-18 | Rotary engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/TR2018/000093 WO2020060500A1 (en) | 2018-09-18 | 2018-09-18 | Rotary engine |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2020060500A1 true WO2020060500A1 (en) | 2020-03-26 |
Family
ID=69888821
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/TR2018/000093 WO2020060500A1 (en) | 2018-09-18 | 2018-09-18 | Rotary engine |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2020060500A1 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR571128A (en) * | 1922-12-09 | 1924-05-12 | Rotary explosion engine | |
JPS5575501A (en) * | 1978-11-30 | 1980-06-06 | Toshio Okumura | Rotary type internal combustion engine |
CN201103494Y (en) * | 2007-10-31 | 2008-08-20 | 姚玉善 | Air injection rotor engine |
JP2019203924A (en) * | 2018-05-21 | 2019-11-28 | 株式会社ミツトヨ | Focal distance variable lens device and focal distance variable lens control method |
-
2018
- 2018-09-18 WO PCT/TR2018/000093 patent/WO2020060500A1/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR571128A (en) * | 1922-12-09 | 1924-05-12 | Rotary explosion engine | |
JPS5575501A (en) * | 1978-11-30 | 1980-06-06 | Toshio Okumura | Rotary type internal combustion engine |
CN201103494Y (en) * | 2007-10-31 | 2008-08-20 | 姚玉善 | Air injection rotor engine |
JP2019203924A (en) * | 2018-05-21 | 2019-11-28 | 株式会社ミツトヨ | Focal distance variable lens device and focal distance variable lens control method |
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