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The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.
Unlike a four-stroke engine, the crankcase of which is closed except for its ventilation system, a two-stroke engine uses the crankcase as part of the induction tract, so oil must be mixed with gasoline to be distributed throughout the engine for lubrication. [1] The resultant mix is referred to as premix or petroil. [2]
The 2si 215 is a family of single-cylinder, fan-cooled, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by JLO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.
Simple two-stroke engines are lubricated by oil mixed into the fuel or injected into the induction stream as a spray. Early slow-speed stationary and marine engines were lubricated by gravity from small chambers similar to those used on steam engines at the time — with an engine tender refilling these as needed.
Lubrication is by use of pre-mixed fuel and oil at 50:1. The 532 has a single Bosch flywheel magneto ignition system. It can be equipped with either one or two piston-type carburetors. It uses a manifold-driven pneumatic fuel pump to provide fuel pressure. [1] The engine's propeller drive is via a Rotax type B or C style gearbox.
It is equipped with a recoil starter system or optionally electric start and a 2.1 or 2.6:1 belt reduction drive. [1] [2] [3] The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 45 hp (34 kW) at 5800 rpm, the G-50 competed in the early 1980s ultralight powerplant market against the similar Rotax 447. Production of the ...
Data from Cliche & 2si General characteristics Type: Three-cylinder, two-stroke aircraft engine Bore: 69.5 mm (2.74 in) Stroke: 60 mm (2.36 in) Displacement: 684 cc (41.7 cu in) Length: 21.6 in (549 mm) Width: 19.05 in (484 mm) Height: 13.9 in (353 mm) Dry weight: 89 lb (40 kg) Components Valvetrain: reed valve porting Fuel type: Minimum 92 octane Oil system: premixed oil and fuel at 50:1 ...
Data from McCulloch Kart Engines, Bore and Stroke, MC101B Kart Engine Illustrated Parts List and Cliche General characteristics Type: single cylinder, two-stroke engine Bore: 2.280 in (5.791 cm) Stroke: 1.835 in (4.661 cm) Displacement: 7.5 cu in (122.90 cc) Components Fuel system: carburetor Oil system: pre-mixed Cooling system: air-cooled Performance Power output: 12.5 hp (9 kW) at 9000 rpm ...
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