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Kinney HRH

The Kinney HRH (Hot Rod Helicopter) is an American helicopter that was designed by Robert Kinney and produced by Vortech, Inc in the form of plans for amateur construction. The aircraft was first shown at Sun 'n Fun in 2002.[1][2]

HRH
Role Helicopter
National origin United States
Manufacturer Vortech, Inc
Designer Robert Kinney
First flight 2001
Introduction 2002
Status Plans available (2013)
Number built one

Design and development

The HRH was designed to comply with the US experimental – amateur-built rules. It features a single main rotor, a single-seat enclosed cockpit with a windshield, skid-type landing gear and a four-cylinder, air-cooled, four-stroke, 165 hp (123 kW) Subaru EJ25 automotive engine. It is the high power to weight ratio that gives the aircraft its name.[1][2]

The aircraft fuselage is made from a mix of welded 4130 steel tube and bolted-together aluminum tubing, with a composite cabin shell. Its 25 ft (7.6 m) diameter two-bladed Waitman composite rotor has a chord of 8 in (20 cm). The tail rotor has a 46 in (117 cm) diameter. The aircraft has an empty weight of 1,000 lb (454 kg) and a gross weight of 1,350 lb (612 kg), giving a useful load of 350 lb (159 kg). With full fuel of 18.5 U.S. gallons (70 L; 15.4 imp gal) the payload is 239 kg (527 lb). The HRH can hover in ground effect at 7,000 ft (2,134 m) and out of ground effect at 5,000 ft (1,524 m)[1][2]

Operational history

By January 2013 there was one example, the 2001 prototype, registered in the United States with the Federal Aviation Administration.[3]

Specifications (HRH)

Data from Bayerl and Vortech[1][2]

General characteristics

  • Crew: one
  • Length: 20 ft 0 in (6.10 m)
  • Width: 5.55 ft (1.69 m)
  • Height: 7 ft 3 in (2.21 m)
  • Empty weight: 1,000 lb (454 kg)
  • Gross weight: 1,350 lb (612 kg)
  • Fuel capacity: 18.5 U.S. gallons (70 L; 15.4 imp gal)
  • Powerplant: 1 × Subaru EJ25 four cylinder, air-cooled, four stroke automotive engine, 165 hp (123 kW)

Performance

  • Maximum speed: 103 mph (166 km/h, 90 kn)
  • Cruise speed: 90 mph (140 km/h, 78 kn)
  • Never exceed speed: 115 mph (185 km/h, 100 kn)
  • Endurance: 2 hours
  • Service ceiling: 10,000 ft (3,000 m)
  • Rate of climb: 790 ft/min (4 m/s)

References

  1. ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 192. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^ a b c d Vortech, Inc (2003). "Kinney HRH – Hot Rod Helicopter". Retrieved February 4, 2013.
  3. ^ Federal Aviation Administration (February 4, 2013). "Make / Model Inquiry Results". Retrieved February 4, 2013.

External links

  • Official website

kinney, helicopter, american, helicopter, that, designed, robert, kinney, produced, vortech, form, plans, amateur, construction, aircraft, first, shown, 2002, hrhrole, helicopternational, origin, united, statesmanufacturer, vortech, incdesigner, robert, kinney. The Kinney HRH Hot Rod Helicopter is an American helicopter that was designed by Robert Kinney and produced by Vortech Inc in the form of plans for amateur construction The aircraft was first shown at Sun n Fun in 2002 1 2 HRHRole HelicopterNational origin United StatesManufacturer Vortech IncDesigner Robert KinneyFirst flight 2001Introduction 2002Status Plans available 2013 Number built one Contents 1 Design and development 2 Operational history 3 Specifications HRH 4 References 5 External linksDesign and development EditThe HRH was designed to comply with the US experimental amateur built rules It features a single main rotor a single seat enclosed cockpit with a windshield skid type landing gear and a four cylinder air cooled four stroke 165 hp 123 kW Subaru EJ25 automotive engine It is the high power to weight ratio that gives the aircraft its name 1 2 The aircraft fuselage is made from a mix of welded 4130 steel tube and bolted together aluminum tubing with a composite cabin shell Its 25 ft 7 6 m diameter two bladed Waitman composite rotor has a chord of 8 in 20 cm The tail rotor has a 46 in 117 cm diameter The aircraft has an empty weight of 1 000 lb 454 kg and a gross weight of 1 350 lb 612 kg giving a useful load of 350 lb 159 kg With full fuel of 18 5 U S gallons 70 L 15 4 imp gal the payload is 239 kg 527 lb The HRH can hover in ground effect at 7 000 ft 2 134 m and out of ground effect at 5 000 ft 1 524 m 1 2 Operational history EditBy January 2013 there was one example the 2001 prototype registered in the United States with the Federal Aviation Administration 3 Specifications HRH EditData from Bayerl and Vortech 1 2 General characteristicsCrew one Length 20 ft 0 in 6 10 m Width 5 55 ft 1 69 m Height 7 ft 3 in 2 21 m Empty weight 1 000 lb 454 kg Gross weight 1 350 lb 612 kg Fuel capacity 18 5 U S gallons 70 L 15 4 imp gal Powerplant 1 Subaru EJ25 four cylinder air cooled four stroke automotive engine 165 hp 123 kW Performance Maximum speed 103 mph 166 km h 90 kn Cruise speed 90 mph 140 km h 78 kn Never exceed speed 115 mph 185 km h 100 kn Endurance 2 hours Service ceiling 10 000 ft 3 000 m Rate of climb 790 ft min 4 m s References Edit a b c d Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 192 WDLA UK Lancaster UK 2011 ISSN 1368 485X a b c d Vortech Inc 2003 Kinney HRH Hot Rod Helicopter Retrieved February 4 2013 Federal Aviation Administration February 4 2013 Make Model Inquiry Results Retrieved February 4 2013 External links EditOfficial website Retrieved from https en wikipedia org w index php title Kinney HRH amp oldid 1065244498, wikipedia, wiki, book, books, library,

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