Engineering:Trixy Trixformer

From HandWiki
Short description: Austrian autogyro roadable aircraft
Trixformer
Role Autogyro
National origin Austria
Manufacturer Trixy Aviation Products
First flight March 2014
Status In production (2017)

The Trixy Trixformer is an Austrian roadable aircraft autogyro/electric motorcycle designed and produced by Trixy Aviation Products of Dornbirn, introduced in 2014. The vehicle is supplied complete and ready-to-fly.[1]

Design and development

The Trixformer is based upon a two-wheeled electric motorcycle chassis as a land vehicle and is designed to add modular flying components. It can be equipped and flown as an autogyro, with the plug-in gyro module. Helicopter or fixed wing aircraft modules were under development in 2015.[1]

As an autogyro, the Trixformer features a single main rotor, a two-seats-in tandem open cockpit with a windshield, tricycle landing gear, plus a tail caster and a four-cylinder, liquid and air-cooled, four stroke 130 hp (97 kW) Trixy 912 Ti engine in pusher configuration.[1]

The aircraft fuselage is made from metal tubing and composites. Its two-bladed rotor has a diameter of 8.6 m (28.2 ft). The aircraft has a typical empty weight of 350 kg (772 lb) and a gross weight of 560 kg (1,235 lb), giving a useful load of 210 kg (463 lb). With full fuel of 80 litres (18 imp gal; 21 US gal) the payload for the pilot, passenger and baggage is 153 kg (337 lb).[1]

Unlike many other autogyro builders Trixy Aviation uses a swash plate in its rotor head designs, rather than a tilt head. This makes the design more sensitive to fly and requires special type training.[1]

Specifications (Trixformer)

Data from Tacke[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Empty weight: 350 kg (772 lb)
  • Gross weight: 560 kg (1,235 lb)
  • Fuel capacity: 80 litres (18 imp gal; 21 US gal)
  • Powerplant: 1 × Trixy 912 Ti four cylinder, liquid and air-cooled, four stroke aircraft engine, 97 kW (130 hp)
  • Main rotor diameter: 8.6 m (28 ft 3 in)
  • Main rotor area: 58 m2 (620 sq ft)
  • Propellers: 3-bladed composite

Performance

  • Maximum speed: 180 km/h (110 mph, 97 kn)
  • Rate of climb: 5.6 m/s (1,100 ft/min)
  • Disk loading: 9.7 kg/m2 (2.0 lb/sq ft)

See also

References

  1. 1.0 1.1 1.2 1.3 1.4 1.5 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 200. Flying Pages Europe SARL, 2015. ISSN 1368-485X

External links