GIAE110R | |
---|---|
Type | Aircraft engine |
National origin | Austria |
Manufacturer | Austro Engine |
The Austro Engine GIAE110R is an Austrian aircraft engine, designed and produced by Austro Engine of Wiener Neustadt for use in light aircraft. [1]
Austria, officially the Republic of Austria, is a country in Central Europe comprising 9 federated states. Its capital, largest city and one of nine states is Vienna. Austria has an area of 83,879 km2 (32,386 sq mi), a population of nearly 9 million people and a nominal GDP of $477 billion. It is bordered by the Czech Republic and Germany to the north, Hungary and Slovakia to the east, Slovenia and Italy to the south, and Switzerland and Liechtenstein to the west. The terrain is highly mountainous, lying within the Alps; only 32% of the country is below 500 m (1,640 ft), and its highest point is 3,798 m (12,461 ft). The majority of the population speaks local Bavarian dialects as their native language, and German in its standard form is the country's official language. Other regional languages are Hungarian, Burgenland Croatian, and Slovene.
An aircraft engine is a component of the propulsion system for an aircraft that generates mechanical power. Aircraft engines are almost always either lightweight piston engines or gas turbines, except for small multicopter UAVs which are almost always electric aircraft.
Austro Engine is an Austrian manufacturer of aircraft engines based at Wiener Neustadt in Lower Austria.
As of 2015 the engine is not listed as available on the company website and may not have been developed past prototype stage. [2]
The engine is a twin rotor four-stroke, air and liquid-cooled, 588 cc (35.9 cu in), gasoline Wankel engine design, with a mechanical gearbox reduction drive, employing a helical gear set, with reduction ratio of 2.96:1. It employs dual capacitor discharge ignition and produces 105 hp (78 kW) at 7500 rpm. [1]
The Wankel engine is a type of internal combustion engine using an eccentric rotary design to convert pressure into rotating motion.
A reduction drive is a mechanical device to shift rotational speed. A planetary reduction drive is a small scale version using ball bearings in an epicyclic arrangement instead of toothed gears.
Capacitor discharge ignition (CDI) or thyristor ignition is a type of automotive electronic ignition system which is widely used in outboard motors, motorcycles, lawn mowers, chainsaws, small engines, turbine-powered aircraft, and some cars. It was originally developed to overcome the long charging times associated with high inductance coils used in inductive discharge ignition (IDI) systems, making the ignition system more suitable for high engine speeds. The capacitive-discharge ignition uses capacitor discharge current to the coil to fire the spark plugs.
Data from World Directory of Leisure Aviation 2011-12 [1]
A propeller speed reduction unit is a gearbox or a belt and pulley device used to reduce the output revolutions per minute (rpm) from the higher input rpm of the powerplant. This allows the use of small displacement internal combustion automotive engines to turn aircraft propellers within an efficient speed range.
The static compression ratio,, of an internal combustion engine or external combustion engine is a value that represents the ratio of the volume of its combustion chamber from its largest capacity to its smallest capacity. It is a fundamental specification for many common combustion engines.
The Mistral G-300 is a Swiss aircraft engine, designed and produced by Mistral Engines of Geneva for use in light aircraft.
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