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Shaanxi Baojii Special Vehicles Lie Ying Falcon

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Lie Ying Falcon
Role Autogyro
National origin China
Manufacturer Shaanxi Baojii Special Vehicles Manufacturing Company
Status In production (2015)

The Shaanxi Baojii Special Vehicles Lie Ying Falcon ("Semi-Open Cabin With Tandem Seats Falcon") is a Chinese autogyro that was designed and produced by the Shaanxi Baojii Special Vehicles Manufacturing Company of Baoji in Shaanxi province. The aircraft was supplied complete and ready-to-fly.[1]

The manufacturer is a well-known builder of armoured vehicles for police and military use and the aircraft was reportedly flying in 2015, but its website was taken down in late 2016 and the status of the company and the gyroplane are unclear.[1][2]

Design and development

The Falcon was designed for police and military use as a surveillance aircraft. It features a single main rotor, a two-seats-in tandem open cockpit with a windshield, tricycle landing gear and a Rotax 914 engine in pusher configuration. The Rotax engine is an Austrian-made, four-cylinder, liquid- and air-cooled, four stroke turbocharged 115 hp (86 kW) unit.[1]

The aircraft has a two-bladed rotor with a diameter of 8.4 m (27.6 ft). It has a typical empty weight of 290 kg (639 lb) and a gross weight of 560 kg (1,235 lb), giving a useful load of 270 kg (595 lb). With full fuel of 70 litres (15 imp gal; 18 US gal) the payload for the crew and mission equipment is 220 kg (485 lb).[1]

Specifications (Falcon)

Data from Tacke[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Empty weight: 290 kg (639 lb)
  • Gross weight: 560 kg (1,235 lb)
  • Fuel capacity: 70 litres (15 imp gal; 18 US gal)
  • Powerplant: 1 × Rotax 914 four cylinder, liquid and air-cooled, four stroke turbocharged aircraft engine, 75 kW (100 hp)
  • Main rotor diameter: 8.4 m (27 ft 7 in)
  • Main rotor area: 55 m2 (590 sq ft)
  • Propellers: 3-bladed composite

Performance

  • Maximum speed: 180 km/h (110 mph, 97 kn)
  • Cruise speed: 150 km/h (93 mph, 81 kn)
  • Rate of climb: 2.5 m/s (490 ft/min)
  • Disk loading: 10.2 kg/m2 (2.1 lb/sq ft)

See also

References

  1. ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 199. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ "Internet Archive Wayback Machine". archive.org. Retrieved 21 November 2017. {{cite web}}: Cite uses generic title (help)
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