Hewland AE75 aero-engine | |
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Type | Piston aero engine |
National origin | United Kingdom |
Manufacturer | Hewland |
The Hewland AE75 is a lightweight aircraft engine that was manufactured in the mid-1980s by Hewland in Maidenhead, United Kingdom. The engine, a two-stroke inverted inline triple of 750 cc (46 cu in) displacement, is liquid-cooled and yields 75 hp (56 kW)
Th AE75 was developed from Hewland’s own 500 cc (31 cu in) twin-cylinder microlight engine. The engine was designed specifically for the ARV Super2, a lightweight two-seater shoulder wing aircraft. The AE75's design is compact and light at 49 kg (108 lb) and yields a power-to-weight ratio of 1.14 kW/kg. Lubrication is via 40:1 pre-mix two-stroke oil.
Each of the engine’s three cylinders has its own carburetor, with an alternate air device to provide carburetor heat. Each cylinder has twin spark plugs, the sparks being provided by a dual ignition system using engine-triggered amplifiers and coils, rather than the more common aviation magneto. The ignition circuit redundancy is such that if one circuit should fail, all three cylinders will still run. Even if two circuits fail, the engine will still fire on two out of three cylinders.
The engine has a 2.7:1Propeller Speed Reduction Unit (PSRU) with helical gears in an oil bath. Final drive to the wooden 63 in (160 cm) diameter 2-blade Hoffman propeller was via a rubber “doughnut” coupling. The PSRU design sited the axis of the propeller below that of the crankshaft. This feature allowed a more pointed nose on the ARV, at the cost of slightly reduced propeller clearance.
The Hewland AE75 was never fitted to any aircraft apart from the ARV Super2, and when ARV production ceased, Hewland stopped AE75 production also. The rights to the AE75 were bought by MidWest, who were developing their AE100 twin-rotor Wankel aero-engine. MidWest had intended to restart production of the AE75 near Stroud, Gloucestershire, but this never materialised. MidWest based the AE100’s gearbox on the AE75’s PSRU, amending it so that the propeller axis was above the eccentric shaft's axis. This increased propeller clearance, but also raised the ARV's thrust line.