| Hummingbird | |
|---|---|
| |
| Role | Helicopter |
| National origin | United States |
| Manufacturer | Vertical Aviation Technologies |
| Introduction | 1991 |
| Status | In production (2013) |
| Developed from | Sikorsky S-52 |
The Vertical Hummingbird is an American helicopter, produced by Vertical Aviation Technologies of Sanford, Florida that was introduced in 1991. The aircraft is supplied as a kit for amateur construction.[1][2]
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Design and development
The Hummingbird is a development of the certified Sikorsky S-52 that first flew in 1947, adapted to kit form. The aircraft features a single main rotor, a four-seat enclosed cabin, quadracycle landing gear and an option for skids.[1] The prototype was converted by Vertical Aviation Technologies from a Sikorsky S-52-3.[3]
The Hummingbird fuselage is made from riveted aluminum sheet. The nose section is adapted from the Bell 206. Its 33 ft (10.1 m) diameter fully articulated three-bladed main rotor employs a NACA 0015 airfoil.[4] The two-bladed tail rotor has a diameter of 5.75 ft (1.8 m). The aircraft has an empty weight of 1,790 lb (812 kg) and a gross weight of 2,800 lb (1,270 kg), giving a useful load of 1,010 lb (458 kg). With full fuel of 57 U.S. gallons (220 L; 47 imp gal) the payload is 668 lb (303 kg).[1][5]
Variants
- VAT S-52-3
- Prototype of the Hummingbird family, converted from an original Sikorsky S-52-3.[3]
- Hummingbird 260L
- Version powered by a six cylinder, air-cooled, four-stroke, dual-ignition 265 hp (198 kW) Lycoming IVO-435 engine[6]
- Hummingbird 300LS
- Version powered by an eight cylinder, liquid-cooled, four-stroke, single-ignition 325 hp (242 kW) General Motors LS7 V-8 automotive conversion engine, derated to 280 hp (209 kW)[7]
- Hummingbird 300L
- Version powered by a six cylinder, air-cooled, fuel injected IO-540 derated to 280 hp (209 kW)[5]
Specifications (Hummingbird 300L)
Data from Vertical Aviation[5]
General characteristics
- Crew: one
- Capacity: three passengers
- Width: 5 ft 0 in (1.52 m)
- Height: 8 ft 7 in (2.62 m)
- Airfoil: NACA 0015
- Empty weight: 1,790 lb (812 kg)
- Gross weight: 2,800 lb (1,270 kg)
- Fuel capacity: 57 US gallons (47 imp gal; 220 L)
- Powerplant: 1 × IO-540 six cylinder, air-cooled, four stroke fuel injected aircraft engine, 280 hp (210 kW)
- Main rotor diameter: 33 ft 0 in (10.06 m)
Performance
- Maximum speed: 110 mph (180 km/h, 96 kn)
- Never exceed speed: 110 mph (180 km/h, 96 kn)
- Range: 380 mi (610 km, 330 nmi)
- Service ceiling: 14,000 ft (4,300 m)
- Rate of climb: 950 ft/min (4.8 m/s) at 2,800 lb (1,270 kg)
References
- ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 194. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ Vertical Aviation Technologies (2013). "Home of the four passenger Hummingbird". Retrieved February 14, 2013.
- ^ a b John W.R. Taylor, ed. (1988). Jane's All the World's Aircraft 1988–89. London: Jane's Information Group. p. 495. ISBN 0-7106-0867-5.
- ^ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Retrieved October 30, 2022.
- ^ a b c "Hummingbird 300L". Retrieved October 30, 2022.
- ^ Vertical Aviation Technologies (2013). "Hummingbird 260L". Archived from the original on October 4, 2014. Retrieved February 14, 2013.
- ^ Vertical Aviation Technologies (2013). "Hummingbird 300LS". Archived from the original on January 28, 2013. Retrieved February 14, 2013.
External links
This page was last edited on 10 May 2023, at 06:27