Avian Gyroplane
Encyclopedia

The Avian 2/180 Gyroplane was a two seat, single engine autogyro
Autogyro
An autogyro , also known as gyroplane, gyrocopter, or rotaplane, is a type of rotorcraft which uses an unpowered rotor in autorotation to develop lift, and an engine-powered propeller, similar to that of a fixed-wing aircraft, to provide thrust...

 built in Canada in the 1960s. Several prototypes were built but production was not achieved.

Design

Avian Aircraft was started by Peter Payne and colleagues from the Avro Canada
Avro Canada
Commonly known as Avro Canada, this company started in 1945 as an aircraft plant and became within thirteen years the third-largest company in Canada, one of the largest 100 companies in the world, and directly employing over 50,000...

 company specifically to build a modern autogyro.

The Gyroplane was a two seat autogyro without wings, with a ducted fan pusher propeller driven by a 200 hp (150kW) Lycoming IO-360 piston engine. It had a three bladed rotor
Helicopter rotor
A helicopter main rotor or rotor system is a type of fan that is used to generate both the aerodynamic lift force that supports the weight of the helicopter, and thrust which counteracts aerodynamic drag in forward flight...

, formed from bonded aluminium. There were flapping hinges but no drag hinges. In normal flight the rotor was undriven, but the design team were keen to enable vertical jump starts, an autogyro technique which spins up the rotor before take off without forward movement over the ground. The first prototype used conspicuous tip jets fed directly with compressed air from a fuselage mounted cylinder.

The fuselage was built on a light alloy box beam which carried the cabin, engine mounting, rotor pylon and propeller duct. The well glazed cabin seated two in tandem in front of the engine. Entry was via a starboard side door; dual controls were fitted. Yaw
Yaw
The word yaw can refer to:* Yaw angle, one of the Tait-Bryan angles, describing the heading of a vehicle or machine, and some other related elements:**Yaw system, component responsible for the orientation of a wind turbine towards the wind....

 was controlled with a rudder mounted within the propeller duct, enhancing its low speed effectiveness. The Gyroplane had a fixed tricycle undercarriage. The main wheels were mounted on steel cantilever legs and the nosewheel castored.

Development

The Gyroplane prototype first flew in Spring 1960. It was later lost in a crash. The compressed air jump start system was not a success, so the second prototype used the engine, connected via a belt, clutch and gear box. This aircraft was also made lighter than the first with more use of aluminium and fibreglass, increasing cruising speed by 25%. It was followed by three pre-production aircraft. By the end of 1963 more than 300 flying hours were completed. In December 1964 Avian received a $540,000 Canadian government contract to build a modified Gyroplane that would take the type to Certification. This was achieved late in 1968.

In 1970 Avian Ltd went into receivership. Although there were later hopes of a revival, nothing came of them. In 1972 some assets of Avian, including three Gyroplanes, were put up for sale, but no purchase is recorded. However, in 2002 one surviving Gyroplane and its certification rights were sold to Pegasus Rotorcraft Ltd, who renamed it the Pegasus III.

Specifications (certification aircraft)

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