WO2020150797A1 - Combustion engine - Google Patents
Combustion engine Download PDFInfo
- Publication number
- WO2020150797A1 WO2020150797A1 PCT/BR2019/050482 BR2019050482W WO2020150797A1 WO 2020150797 A1 WO2020150797 A1 WO 2020150797A1 BR 2019050482 W BR2019050482 W BR 2019050482W WO 2020150797 A1 WO2020150797 A1 WO 2020150797A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- ring
- combustion engine
- engine
- engine according
- combustion
- 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
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
-
- 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
- F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
- F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
- F01C11/004—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle and of complementary function, e.g. internal combustion engine with supercharger
Definitions
- the present invention relates to a structural arrangement for a universal internal combustion engine, stationary, for machines, or mounted on a vehicle, being able to use different types of fuels. More specifically, the present invention relates to an internal combustion engine with improved combustion efficiency, better thermodynamic performance, with reduced fuel consumption, low gas emissions to the environment and minimum size.
- the present invention relates to a combustion engine, alternate rotary mixed formed by one or more sectors for multiple uses such as: Stationary, vehicles, machines, etc. More specifically, the present invention relates to a structural arrangement for an internal combustion engine, using several types of fuels.
- the vehicle can be land, sea, rail or air. More specifically, the present invention relates to an internal combustion engine with improved combustion efficiency, better thermodynamic performance, reduced dimensions, greater power / weight ratio that surpasses airplane turbines that use the Brayton thermodynamic cycle, with reduced consumption of fuels and emission of gases to the environment, up to 3 times less.
- Figure 1 shows an internal combustion engine without external accessories.
- Figures 5B and 2B show the motor shaft with cam and the ring.
- Figures 3A and 3B show the subassembly (ring) of the present invention.
- Figure 4 shows the eccentric of the subassembly of the present invention.
- Figures 5A and 5B show the subassembly of the motor shaft with the eccentric shaft plus the red ring of the present invention.
- Figure 6 shows the subassembly of the seal blades of the present invention.
- Figure 7 shows the structural block for the frame of the motor elements of the present invention.
- Figure 8 shows the cover that separates the engine sectors of the present invention.
- Figure 9 shows the thermodynamic profile of the engine of the present invention.
- Figures 10A and 10B show a subassembly inside with the axis, the eccentric, the ring, the seals and the block, they form the combustion or compression chambers.
- the present invention relates to a combustion engine, alternate rotary mixed formed by one or more sectors for universal use. More particularly, the structural arrangement of the engine presented here is simple, comprising few moving elements, which simplifies the manufacturing and assembly process, requiring the presence of small radiators to cool the system. The system can also be cooled with air.
- This motor comprises only the following sets of moving elements: The ring, the shaft together with the eccentric and the sealing pads.
- the characteristics of the present engine provide a structural arrangement with reduced dimensions, but capable of performing a thermodynamic cycle in each turn of the axis as many times as many combustion chambers have with extremely high efficiency.
- a technician in the subject recognizes that the term sectors used here, includes a minimum set of parts necessary for the formation of an engine.
- the structural arrangement presented here provides the technique of an engine in which the first part of the cycle, the compression occurs in one or more stages, without limit of them.
- the thermodynamic cycle using this engine is more efficient than those currently used, as the compression is performed in one or more steps. With intermediate cooling, which considerably reduces the effort required to carry out the compression, and in the expansion process makes the most of the gas energy. However, in this cycle, the energy generated by the fuel is used as much as possible with minimal waste.
- Compression is carried out in a compression chamber in the first stage and equal in the following stages to an increasingly smaller volume followed each by cooling the system between stages by radiators to the environment, and further compressing in the combustion chamber, can it is also possible to inject water sprayed into the combustion chamber to cool even more the last compression that is made inside this combustion chamber, in this way a compression is made close to the isentropic then the explosion and then the expansion, during this last process of Expansion takes full advantage of energy in the adiabatic expansion up to the suction pressure value.
- This arrangement has a quiet exhaust and low temperature. As previously mentioned, since the exhaust pressure is very low, noise and temperature are also low.
- the engine presented here completes several cycles in each of the combustion sectors, comprising a turn of the axle, which makes it very light and powerful.
- a three-sector engine with 16 combustion chambers per sector can be used, which in each turn would generate 48 explosions (cycles).
- the torque of this motor is very high and continuous with little oscillation, which allows low revolutions per minute, therefore, less consumption at minimum rpm.
- the torque can be improved by tilting the seal blades at a predetermined angle proven in the laboratory and only when the seal pastes are arranged in the block.
- the engine can be regenerative, accumulating energy in the compression part in an extra tank, which works as a reserve tank, only in vehicles such as trucks, trains, etc.
- the extra tank when the vehicle makes the descent movement, can accumulate the compressed air that is later used on the climbs as an extra energy reused free of charge, without having to use the brake to descend.
- the condensation water from the extra tank at the reserve pressure can be re-injected at the end of the combustion cycle for a cooling of the system without energy cost. This cooling occurs at the time of escape, further cooling the combustion sections. of the system.
- the heating of the system is completely uniform around the engine without hot spots and is very low.
- the system can be cooled with a fan fitted to the balance counterweight between sectors.
- the engine proposed here has a low friction speed between its elements, promoting high revolutions per minute.
- a high-powered sports vehicle can have 20,000 rpm. or more.
- the speed of the seal blades against the ring or against the block is minimal, since it is oscillating with alternating movements back and forth, achieving perfect lubrication of the seal blades with very low consumption of lubricating oil.
- the engine object of the present invention can be arranged in very small spaces, contributing to a greater useful space in every transport vehicle.
- air vehicles for example, airplanes; this engine has a low frontal section, reducing drag, and these mixed turbofan engines (with inverter included in the propeller, intubated propellers) can be made of very high power, much more efficiency and more than 100,000 HP at 1500 rpm with less weight than the turbines and for speeds similar to current commercial airplanes (1000 klmts./Hr.).
- this engine still operates at low exhaust temperatures, practically undetectable by the infrared and are very quiet. Without using any reducer or flow diverters for braking, only the reversible turbofan, or intubated reversible propeller. It can be used in supersonic airplanes with a very special design adding one or more axial or centrifugal turbochargers, combustion chambers and expansion heads, this mixed engine would be extremely efficient and would not need a turbine. In addition to vertical takeoff planes, helicopters, etc.
- the compression ratio can increase to a very high value without detonation, as the air and fuel are previously cooled.
- the exhaust valves work at low temperatures and low pressures. This fact contributes to the fact that production processes and materials can be used simpler, reducing manufacturing costs. Among the materials that could be used, we have aluminum, titanium, stainless steel, among others.
- any of the possible combinations can be used, being able to use one or more different sectors and any number of combustion and / or compression chambers in each sector, which may vary between them.
- This engine could also be used for energy production, in thermoelectric form, using only 1/3 of fuel, and machines with power greater than 1000 M.W., of an extremely small and super economical size could also be manufactured.
- the present engine contributes to the health of the planet, as global warming would be reduced, since there would be a lot of reduction in the CO2 emission rates into the atmosphere.
- the motor of the present invention can comprise only a single sector or comprise a plurality of sectors that work together as if they were a single motor, as shown in Figure 1.
- Said sectors are ordered according to the engine design, and the engine may have one or more sectors in its different shapes, sizes, order and composition for each particular use.
- Figure 1 shows the assembly of an internal combustion engine without the external elements. Said engine is provided with several holes for entry and exit of gases and liquids in each sector of the engine.
- a motor comprising several sectors along its longitudinal axis, which are provided inside with cylindrical, ring-shaped structures and hereinafter referred to as subassembly. Said subassemblies are better detailed by Figures 2A, 2B, 3A, 3B, 5A and 5B).
- said subassemblies adjust to the outside diameter of its own eccentric throughout its length, in addition to having free rotation over the eccentric.
- the eccentric forms an inseparable part of the engine, which also comprises its axis and its ring, these elements being fixedly assembled together the axis with the eccentric and the ring with the eccentric free, as shown in Figure 2B.
- the axle and cam may be one piece on single sector engines, but on more than one sector engines they must be separated and assembled together fixed later when the final assembly is done see Figure 11
- Figure 5B shows an engine with 8 combustion or compression chambers
- Figure 2B shows an engine with 9 combustion or compression chambers.
- Figure 6 of the present invention shows the additional elements of the engine, such as the seals, which work together with the subassemblies. Said seals are arranged one in each groove of the subassembly or one in each groove of the structural block.
- the surfaces of the seals are where the sealing occurs by means of a sliding-oscillating movement against the ring or against the structure block and laterally sliding against the engine covers.
- Subassemblies are responsible for the operation of the engine presented here. If the ring (subassembly) is not present in the project, the engine would only work with the seal blades on the block and the relative speed would be very high against the eccentric, the part where the lubrication would be weak, therefore the engine could only have low rpm and its useful life would also be very low, emissions would also be very high, because if you would need to use a lot of oil, or if you could manufacture large engines, these would be impossible due to the very high relative speed.
- the motor shaft rotates together when the cam starts to move. However, during the rotating movement of the motor shaft and eccentric, the ring, the subassembly, oscillates, as it is free, as shown in Figures 5A and 5B.
- the combustion or compression chambers are formed by the closed internal space for combustion between the parts (subassemblies), which is formed by two intermediate or final covers, a carcass (frame, structure or block), two consecutive stamp seals and the ring.
- Figure 8 shows this cover, which separates the different sectors that make up the engine and can vary in size, shape and composition according to the project.
- the main benefit of the presence of the ring in the engines of the present invention is the relative speed between this and the seal pads, this is often less than that applied to current engines.
- the subassemblies of the seals are provided with at least one push spring on the innermost end of each seals or pressure air.
- Said springs are not shown in the Figures accompanying the present application. Particularly, said springs are arranged against the ring or against the block, pushing against them according to the case, as shown in Figures 2B, 10A and 10B.
- This engine also includes valves for the entry and exit of combustion and compression gases not shown in the figures.
- Figure 9 of the present invention shows a theoretical thermodynamic profile representative of pressure-volume of the present internal combustion engine.
- the present invention provides the technique of a ring as a whole in which the relative speed between said ring and the seal blades is extremely low which allows for an excellent lubrication of the system, adequate sealing, durability and minimum consumption of lubricating oil . Therefore, the paddle wear is reduced and the engine revolutions per minute can be significantly increased, which makes it possible to make engines of smaller size and weight, for high power, high speed (rpm), high efficiency, low consumption , low pollution rate and long service life.
Abstract
Description
Claims
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP19911892.8A EP3916199A4 (en) | 2019-01-24 | 2019-11-08 | Combustion engine |
MX2021008424A MX2021008424A (en) | 2019-01-24 | 2019-11-08 | Combustion engine. |
CA3125696A CA3125696A1 (en) | 2019-01-24 | 2019-11-08 | Combustion engine |
CN201980088934.6A CN113544359A (en) | 2019-01-24 | 2019-11-08 | Combustion engine |
KR1020217026655A KR20210113686A (en) | 2019-01-24 | 2019-11-08 | combustion engine |
JP2021537133A JP2022519442A (en) | 2019-01-24 | 2019-11-08 | Combustion engine |
US17/420,672 US20210388758A1 (en) | 2019-01-24 | 2019-11-11 | Combustion engine |
IL284839A IL284839A (en) | 2019-01-24 | 2021-07-13 | Combustion engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRBR1020190015217 | 2019-01-24 | ||
BR102019001521A BR102019001521A8 (en) | 2019-01-24 | 2019-01-24 | COMBUSTION ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2020150797A1 true WO2020150797A1 (en) | 2020-07-30 |
Family
ID=71735574
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/BR2019/050482 WO2020150797A1 (en) | 2019-01-24 | 2019-11-08 | Combustion engine |
Country Status (9)
Country | Link |
---|---|
EP (1) | EP3916199A4 (en) |
JP (1) | JP2022519442A (en) |
KR (1) | KR20210113686A (en) |
CN (1) | CN113544359A (en) |
BR (1) | BR102019001521A8 (en) |
CA (1) | CA3125696A1 (en) |
IL (1) | IL284839A (en) |
MX (1) | MX2021008424A (en) |
WO (1) | WO2020150797A1 (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3909161A (en) * | 1972-04-10 | 1975-09-30 | Eric John Stenner | Rotary pumps or engines of the sliding, rocking, abutment type |
US4177024A (en) * | 1976-05-14 | 1979-12-04 | Kaltenbach & Voigt Gmbh & Co. | Vane air motor with eccentric adjustment ring and bearing ring for vane ends |
US4191032A (en) * | 1978-01-27 | 1980-03-04 | August Daniel A | Rotary energy-transmitting mechanism |
US20010014294A1 (en) * | 1999-03-01 | 2001-08-16 | Mallen Brian D. | Vane pumping machine utilizing invar-class alloys for maximizing operating performance and reducing pollution emissions |
WO2003091545A1 (en) * | 2002-04-24 | 2003-11-06 | Viitamaeki Tapio | Hydraulic motor |
JP2011241790A (en) * | 2010-05-20 | 2011-12-01 | Nippon Soken Inc | Two-stage boost compressor |
EP2942524A1 (en) * | 2013-01-25 | 2015-11-11 | Beijing Rostar Technology Co. Ltd | Rotating device and rotor compressor using same, and fluid motor |
KR20180000808A (en) * | 2016-06-24 | 2018-01-04 | 김재호 | Vane motor |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3955540A (en) * | 1974-05-22 | 1976-05-11 | Blanchard James G | Rotary internal combustion engine |
US3951112A (en) * | 1974-11-21 | 1976-04-20 | Lee Hunter | Rotary internal combustion engine with rotating circular piston |
US4915071A (en) * | 1987-09-08 | 1990-04-10 | Hasen Engine Corporation | Orbit internal combustion engine |
WO1999004141A1 (en) * | 1997-07-16 | 1999-01-28 | O'brien, Thea, Johanna | A vane type rotary engine |
-
2019
- 2019-01-24 BR BR102019001521A patent/BR102019001521A8/en unknown
- 2019-11-08 JP JP2021537133A patent/JP2022519442A/en active Pending
- 2019-11-08 MX MX2021008424A patent/MX2021008424A/en unknown
- 2019-11-08 CA CA3125696A patent/CA3125696A1/en active Pending
- 2019-11-08 CN CN201980088934.6A patent/CN113544359A/en active Pending
- 2019-11-08 KR KR1020217026655A patent/KR20210113686A/en unknown
- 2019-11-08 WO PCT/BR2019/050482 patent/WO2020150797A1/en unknown
- 2019-11-08 EP EP19911892.8A patent/EP3916199A4/en not_active Withdrawn
-
2021
- 2021-07-13 IL IL284839A patent/IL284839A/en unknown
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3909161A (en) * | 1972-04-10 | 1975-09-30 | Eric John Stenner | Rotary pumps or engines of the sliding, rocking, abutment type |
US4177024A (en) * | 1976-05-14 | 1979-12-04 | Kaltenbach & Voigt Gmbh & Co. | Vane air motor with eccentric adjustment ring and bearing ring for vane ends |
US4191032A (en) * | 1978-01-27 | 1980-03-04 | August Daniel A | Rotary energy-transmitting mechanism |
US20010014294A1 (en) * | 1999-03-01 | 2001-08-16 | Mallen Brian D. | Vane pumping machine utilizing invar-class alloys for maximizing operating performance and reducing pollution emissions |
WO2003091545A1 (en) * | 2002-04-24 | 2003-11-06 | Viitamaeki Tapio | Hydraulic motor |
JP2011241790A (en) * | 2010-05-20 | 2011-12-01 | Nippon Soken Inc | Two-stage boost compressor |
EP2942524A1 (en) * | 2013-01-25 | 2015-11-11 | Beijing Rostar Technology Co. Ltd | Rotating device and rotor compressor using same, and fluid motor |
KR20180000808A (en) * | 2016-06-24 | 2018-01-04 | 김재호 | Vane motor |
Non-Patent Citations (1)
Title |
---|
See also references of EP3916199A4 * |
Also Published As
Publication number | Publication date |
---|---|
MX2021008424A (en) | 2021-10-26 |
EP3916199A4 (en) | 2022-11-09 |
EP3916199A1 (en) | 2021-12-01 |
BR102019001521A2 (en) | 2020-08-04 |
BR102019001521A8 (en) | 2023-04-04 |
JP2022519442A (en) | 2022-03-24 |
KR20210113686A (en) | 2021-09-16 |
IL284839A (en) | 2021-08-31 |
CA3125696A1 (en) | 2020-07-30 |
CN113544359A (en) | 2021-10-22 |
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