Rotax 914
From Wikipedia, the free encyclopedia
The Rotax 914 is an Austrian turbo-charged, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads. Designed and built by Rotax the engine commonly powers certified light aircraft, homebuilt aircraft, autogyros and military UAVs such as the MQ-1 Predator.
Applications
- Aero Adventure Pegasus
- Aerospool WT9 Dynamic
- Air Copter A3C
- Alisport Yuma
- Alpi Pioneer 300
- Australian Aircraft Kits Hornet STOL
- AutoGyro MT-03
- AutoGyro Calidus
- AutoGyro Cavalon
- B&F Fk14 Polaris
- Bauer BAD-12 Gyrotrainer
- Bushcaddy R-80
- Bushcaddy R-120
- The Butterfly Super Sky Cycle
- Celier Kiss
- Celier Xenon 2
- Chayair Sycamore
- Criquet Storch
- Denel Dynamics Bateleur
- Diamond HK36 Super Dimona
- Dorna Parandeh Abi
- Dova DV-1 Skylark
- Dyn'Aéro MCR4S
- Dynali H2S
- ELA 07
- Eurodisplay SR-01 Magic
- Europa XS
- FD-Composites ArrowCopter
- Flying Legend Hawker Hurricane Replica
- General Aviation Design Bureau T-32 Maverick
- Heli-Sport CH-7 Kompress helicopter
- IAI Heron
- Idea Hydropteron
- Just Superstol
- Magni M-14 Scout
- Magni M-24 Orion
- M&D Flugzeugbau Samburo
- MQ-1 Predator
- NAL Hansa
- Norman Aviation Nordic VI
- Norman Aviation Nordic 8 Mini Explorer
- Pagotto Brakogyro
- Phenix Aviation Phenix
- RMT Bateleur
- Roko Aero NG4
- Rotor Flight Dynamics Dominator
- RotorSport UK Calidus
- RotorSport UK MT-03
- Softeks V-24 Lastochka
- SlipStream Genesis
- Stemme S10 motor glider
- Titan T-51 Mustang
- Ultravia Pelican
- Wild DoubleEnder
- Wüst Seahawk
Specifications (914)
General characteristics
- Type: four-cylinder, four-stroke liquid- / air-cooled engine with opposed cylinders
- Bore: 79.5 mm (3.13 in)
- Stroke: 61 mm (2.4 in)
- Displacement: 1,211.2 cc (73.91 cu in)
- Length: 561 mm (22.1 in)
- Width: 576 mm (22.7 in)
- Dry weight: 78 kg (172 lb) with electric starter, carburetors, fuel pump, air filters and oil system
Components
- Valvetrain: OHV, hydraulic lifters, pushrods, rocker arms
- Fuel system: Dual CD carburetors, mechanical diaphragm pump
- Fuel type: Unleaded: 87 octane AKI (Canada/USA) / 90 octane RON (European) or higher
- Oil system: Dry sump with trochoid pump, camshaft driven
- Cooling system: Liquid-cooled cylinder heads, air-cooled cylinders
- Reduction gear: Integrated reduction gear 1:2.273; 1:2.43 optional
- Electronic dual ignition
Performance
- Power output: Maximum 84 kW (115 hp) at 5,800 rpm, with 5 minute time limit; 73 kW (100 hp) continuous
See also
- Rotax aircraft engines
- Related lists
References
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