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The LCR - 814 TGti engine is a twin-rotor four-stroke, 814 cc (49.7 cu in) displacement, liquid-cooled, fuel injected, petrol, Wankel engine design, with a toothed poly V belt reduction drive with a reduction ratio of 3:1. It employs dual electronic ignition and produces 75 hp (56 kW) at 6000 rpm. [1]
Diamond discontinued production of the MidWest twin-rotor engine, but for a period they continued building the single-rotor model, mainly for the motor glider market. Diamond then designed and produced two replacement models, both single-rotor Wankel engines: the 55 hp (41 kW) Austro Engine AE50R and the 75 hp (56 kW) Austro Engine AE75R. These ...
Mistral Engines SA was a Swiss developer and manufacturer of wankel rotary aviation light aircraft, helicopter and unmanned military vehicle engines. [1] Its headquarters was in Geneva, Switzerland [ 2 ] and was majority owned by DEA General Aviation, a Chinese company based in Guangdong .
The engine was made with a chamber volume V k of 2,500 in 3 (41 dm 3), and a power output of 550 hp (410 kW) per rotor. Both single, and twin-rotor engines were made (producing 550 hp (410 kW) or 1,100 hp (820 kW) respectively). The engines ran on natural gas and had a relatively low engine speed due to its application. [197]
Austro Engine is an Austrian manufacturer of aircraft engines based at Wiener Neustadt in Lower Austria. ... Twin rotor Wankel engine with 588 cm 3 (36 cu in ...
Wankel aircraft engine. The company's aircraft engine line consists of the single rotor Wankel AG LCR - 407 SGti four-stroke, 407 cc (24.8 cu in) displacement, liquid-cooled, fuel injected, petrol, Wankel engine that produces 37 hp (28 kW) at 6000 rpm and the dual rotor Wankel AG LCR - 814 TGti 814 cc (49.7 cu in) displacement, liquid-cooled, fuel injected, petrol, Wankel engine design, that ...
The company was founded in 2008 by Gilo Cardozo, who designed the company's first Wankel engine to power a paramotor flight over Mount Everest on 14 May 2007. [ 2 ] [ 3 ] The company's RT300 is a Wankel single-rotor design that produces 31 to 50 hp (23 to 37 kW), while the twin-rotor RT600 produces 53 to 100 hp (40 to 75 kW).
Bristol "Heliogyro" RI/II (experimental helicopter) Cierva W.5 - 2-seater twin outrigger rotor helicopter, first flight 1938. Cierva W.6 - twin rotor helicopter, flown in 1939; Cierva W.9 - jet efflux torque compensation design. Built in 1944 and flown in 1945.