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Data from European Aviation Safety Agency, Federal Aviation Administration, Flying. General characteristics Length: 6.9 m (22 ft 8 in) Wingspan: 7.7 m (25 ft 3 in) Height: 2.56 m (8 ft 5 in) Wing area: 11.3 m 2 (122 sq ft) Gross weight: 998 kg (2,200 lb) Fuel capacity: 311 litres (68 imp gal; 82 US gal) Powerplant: 1 × Lycoming AEIO-580-B1A horizontally opposed, six-cylinder aircraft engine ...
The Lycoming IO-580 engine is a horizontally opposed, six-cylinder aircraft engine featuring three cylinders per side, manufactured by Lycoming Engines. [1] There is no carburetted version of the engine, which would have been designated O-580 and therefore the base model is the IO-580. [2] This engine family competes with the Continental IO-550 ...
The GSO-580 family of engines covers a range from 375 hp (280 kW) to 400 hp (298 kW). All have a displacement of 578 cubic inches (9.47 litres) and the cylinders have air-cooled heads . Compared to other horizontally opposed engines of similar displacement this family of engines produces high output power by supercharging and high maximum rpm ...
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.
The GE Passport is a high bypass ratio turbofan. The engine is a twin-spool, axial-flow turbofan with a high bypass ratio of 5.6:1 and an overall pressure ratio of 45:1. The front fan is attached to the three-stage low-pressure compressor; the 23:1 pressure ratio 10-stage high-pressure compressor includes five blisk stages for weight reduction.
The acceptable power range is 100 to 160 hp (75 to 119 kW) and the standard engines used are the 100 hp (75 kW) Rotax 912ULS or the 130 hp (97 kW) ULPower UL350iS powerplant. [ 4 ] The aircraft has a typical empty weight of 740 lb (340 kg) and a gross weight of 1,320 lb (600 kg), giving a useful load of 580 lb (260 kg).
Rolls-Royce Avon early jet engine showing 1 of 2 sets of 3 valves at the top and 1 of 2 valves at the bottom which release some air from the compressor, pressure ratio 7.45:1, for starting and low speed running. Also visible at the front is the row of bearings for the variable inlet guide vanes.
In total, 28 test engines will be used by CFM to achieve engine certification, and 32 others will be used by Airbus, Boeing and COMAC for aircraft certification and test programs. [1] [17] The first engine entering the test program reached and sustained 33,000 lbf (150 kN) of thrust, required to satisfy the highest rating for the Airbus A321neo ...