Wankel Aircraft Engine - Now and in the future, flying vehicles (as well as drones) will flourish. They need small, powerful, environmentally friendly machines. Four-stroke engines and turbine engines are not suitable. This engine replaces those engines.
The Wankel engine does not have a separate lubrication chamber. Lubricant is mixed with fuel and injected directly into the combustion chamber. As a result, poor lubrication results in reduced exhaust quality and less durability. Turbine engines are smaller in size, more efficient, more advanced manufacturing techniques and higher maintenance costs. So, expensive price, not good for small use.
Wankel Aircraft Engine
This device solves the above problems. Each rotor, when combined with the body, forms three chambers. Two chambers are used to form the combustion chamber and the other chamber is used for lubrication. The inlet and outlet are arranged in two side bodies. These doors are opened and closed by the rotor.
Radial And Rotary
The propeller is used as a compressor. The device works in two cycles. The impeller discharges and charges air to each combustion chamber. All rotor faces rotate inside the lubrication chamber, which is lubricated and cooled. Extends the life of the engine. At high power, each rotor has three combustion chambers, whose power is tripled for each revolution of the shaft.
Unlike turbine engines, this engine can be built using existing four-stroke engine technology. This engine has fewer components than a four-stroke engine and only has three moving parts (rotor, shaft and propeller). Therefore, this engine can compete with four-stroke engines and its price is much lower than a turbine with the same power. At the same time, the maintenance cost is low.
This engine is a combination of rotary engine and turbine engine. With the same power, this engine is more compact than a rotary engine, more efficient than a turbine engine, more durable than a Wankel engine, better exhaust quality. When replacing an aircraft turbine engine, the engine can reduce the amount of fuel it carries and increase time and range. Definition of Alternator Actually, the rotation of Wankel experimental aircraft today is the work of two companies: American Rotary Engine and Auto PSRU (see next list). The first produces an engine, the second produces a propeller gearbox.
American Rotary Engine is the aviation sidebar of Atkins Rotary, a hot rod shop that modifies and supports Mazda Wankels for racing. Makes hop-up parts and adapters for anything that moves and fits Wankel. When Mazda parts are phased out, American Rotary Motor is busy producing replacements, including improved rotor housings and more complex parts like timing. Water pump covers and housings.
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For aviation, the American rotary engine focuses on the Mazda 13B engine. While American Joke says all customers want is a "500-hp engine that weighs 30 pounds," it offers a standard 200-hp turbo package. A special American Aviation development is a spring-loaded pop-off valve set at 4 pounds that prevents overinflation after landing or during takeoff.
Big Chevy V-8 power is a customer demand at AutoPSRU. The LS-3 engine is mated to an SD550 gear reduction unit, which has a centrifugal clutch to reduce starting and other recoil loads.
Transmission and engine package specialist Auto PSRU are looking to source their naturally aspirated and turbocharged Mazda 13B engines from American Rotary Motor (see previous listing). Auto PSRU's longstanding offering is a 200hp firewall for the RV-7. Interestingly, after a six-year drought, interest in Wankels has picked up again in 2020, particularly in high-powered 13B options.
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English: German engineer Felix Wankel developed his rotary engine in 1924 and patented it in 1936. It consisted of a triangular cam attached to a drive shaft that acted like a piston in a four-stroke cycle engine. Wankel sent his plans to the German automobile company NSU. Wankel and NSU built and tested the first rotary device in early 1957. The engine found great success in Mazda cars, but was also used in motorcycles, go-karts, air conditioning systems, and airplanes.
Wright Aviation modified the three-engine RC2-60 for flight testing in 1970. Shown here is probably the first Wankel engine to power the Cessna Cardinal. Another Lockheed piloted the Q-Star to demonstrate its feasibility, performance and quiet flight. The third man operated a Hughes TH-55 helicopter.
Economic considerations (eg fuel burning, greenhouse gas emissions) have recently greatly reduced interest in Wankel's concept.
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This file contains additional information, such as Exif metadata, that was added by the digital camera, scanner, or software program used to create or digitize it. If the file has been converted from its original state, some details such as the time stamp may not fully reflect the details of the original file. While the time stamp is only as accurate as the clock on the camera, it can be completely wrong. In general, Wankel engines are limited to a rotor speed of 3000 revolutions per minute (rpm) due to excessive crankshaft bending caused by centrifugal force. The eccentric rotor forces of the Szorenyi machine were not updated in this context, as it used a uniform rotor.
The Wankel rotary engine is an excellent choice for many small propeller aircraft owners and operators. Compared to conventional piston engines, Wankel rotary engines are smaller, lighter, and have a higher power-to-weight ratio. They are virtually vibration free, can't be picked up or hit, and have fewer moving parts (to break). At this point, it is difficult to improve Wankel's design. That is, unless you want to change the shape of the rotor dynamically.
A new rotary engine configuration - the Szorenyi rotary engine - was developed by the Melbourne-based Rotary Engine Development Agency (REDA). Although the stator or fixed part of the Szorenyi motor is similar to the Wankel motor, the rotor geometry of the motor is a rhombus, which is deformed by rotation at the edge of the stator. Szorenyi rotary engine cycle
This geometry results in a rotary engine with four combustion chambers as opposed to Wankel's three rotary chambers. Each revolution of the crankshaft completes one rotor revolution and one complete engine cycle in each of the four chambers: or four power strokes. In contrast, the Wankel engine produces one stroke of power per crankshaft revolution.
Ode To The Radial
A typical Wankel rotary engine uses a three-way rotor to create cavities inside the stator to create a seamless cycle of intake, compression, combustion and exhaust. Point A represents one of the three ends of the rotor, point B represents the eccentric shaft and the white area of the eccentric shaft lobe. (Image credit: Y Tambe)
According to REDA, each Szorenyi four-stroke rotary block is equivalent to a reciprocating or opposed eight-cylinder engine.
The Szorenyi engine is more suitable for multi-rotor configurations than the Rotary Wankel due to the use of side ports compared to the Wankel engine which uses complex side ports. The ability to easily configure multi-rotor and four-stroke engines can result in rotary power plants that produce power equivalent to 8-, 16-, or 24-cylinder reciprocating engines. Also, the development of standard modules can reduce production and life cycle maintenance costs. No-Idle Speed Wankel engines are generally limited to a rotor speed of 3000 revolutions per minute (rpm) due to excessive crankshaft bending caused by eccentric rotor centrifugal forces. Szorenyi's machine was not updated in this regard, as it used a uniform rotor.
The higher potential rev range means that the Szorenyi engine has a higher power density than the Wankel engine, which means greater range, endurance and payload capacity. Also, the Szorenyi engine has more space for internal rotor cooling and does not require a reduction gear in airplanes and unmanned aerial vehicles (UAVs) with large propellers.
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According to this article, the Szorenyi engine can be made to run on gasoline, aviation gasoline (avgas), butane, or hydrogen (since the intake and exhaust ports are well separated).
REDA also noted that if a pre-compression stage was introduced, the engine could run on diesel fuel - which would be in line with the US military's "one-fuel" concept, making the engine a significant case for military applications.
An abridged version of Szorenyi's four-chamber rotary engine development and other technical papers on small aircraft and drone engines is available in the latest International book.
This book covers several UAV propulsion technologies
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