Freewind Bumble B

The Freewind Bumble B (transl.Bumblebee) is a French autogyro that was designed and produced by Freewind Aviation of Vimory, introduced in about 2013. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1]

Bumble B
Role Autogyro
National origin France
Manufacturer Freewind Aviation
Status Production completed (2014)
Unit cost
41,500 (912 turbo model, assembled, 2015)

Freewind Aviation seems to have been founded about 2013 and gone out of business in 2014.[2] It is not clear how many aircraft were produced, although at least one example flew.[1]

Design and development

The Bumble B features a single main rotor, a two-seats-in tandem open cockpit with composite fairing and a windshield, tricycle landing gear and a modified four-cylinder, liquid and air-cooled, four stroke, turbocharged 122 hp (91 kW) Rotax 912 engine in pusher configuration.[1]

The aircraft has a two-bladed rotor with a diameter of 8.4 m (27.6 ft) and a chord of 21.5 cm (8.5 in). The aircraft has a typical empty weight of 258 kg (569 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 192 kg (423 lb). With full fuel of 75 litres (16 imp gal; 20 US gal) the payload for the pilot, passenger and baggage is 138 kg (304 lb).[1]

Reviewer Werner Pfaendler described the design as, "a low cost but good quality gyrocopter with excellent flight characteristics".[1]

Specifications (Bumble B 912 Supercharged)

Data from Tacke[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Empty weight: 258 kg (569 lb)
  • Gross weight: 450 kg (992 lb)
  • Fuel capacity: 75 litres (16 imp gal; 20 US gal)
  • Powerplant: 1 × modified Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, turbocharged aircraft engine, 91 kW (122 hp)
  • Main rotor diameter: 8.4 m (27 ft 7 in)
  • Main rotor area: 57 m2 (610 sq ft)
  • Propellers: 3-bladed composite

Performance

  • Maximum speed: 200 km/h (120 mph, 110 kn)
  • Cruise speed: 150 km/h (93 mph, 81 kn)
  • Rate of climb: 3.1 m/s (610 ft/min)
  • Disk loading: 7.9 kg/m2 (1.6 lb/sq ft)
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See also

References

  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 194. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. "Internet Archive Wayback Machine". archive.org. Retrieved 2 April 2017.
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