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Aero HC-2 Heli Baby

The Aero HC-2 Heli Baby is a two-seat general-purpose light utility helicopter, designed by engineer Jaroslav Šlechta, and produced by the Czechoslovak company Aero Vodochody in the 1950s. It has a three-blade main rotor, and a two-blade tail rotor. The helicopter has an entirely metal frame and cockpit, and windows made of Plexiglas. It was the first and the only Czechoslovak-designed helicopter to be produced.[2]

Aero HC-2 Heli Baby
HC-2 in flight
Role Light helicopter
National origin Czechoslovakia
Manufacturer Aero Vodochody
Designer Jaroslav Šlechta
First flight December 3, 1954
Introduction 1955
Produced 1958-1962[1]
Number built 23 (including 2 prototypes)

Design and development edit

The helicopter was designed by engineer Jaroslav Šlechta.[3] Construction of the prototype began in 1951, and testing commenced in 1954. The first flight occurred on December 3, 1954, and the helicopter was introduced to the public in 1955 at the Brno Industries Fair.[4] Production was slated to begin in 1957, however, engine problems delayed it. The initial run produced 200 of these helicopters.[5] The Czechoslovak Air Force was a user of the HC-2, as was the Czechoslovak People's Army. The Heli Baby is capable of carrying a pilot and 220 pounds of cargo at the speed of 62 mph, while using 4.85 gallons of fuel.[6] In 1959, it was one of the world's lightest two-seated helicopters.[7] Initially powered by an 83 hp (62 kW) Praga DH engine, the more powerful 105 hp (78 kW) Avia M 110H engine, designed specifically for use in helicopters, replaced it after approximately six years.[8][9] The Heli Baby can be used for transport, training, and various "other duties in military and civil service".[10] Cargo space is situated behind the helicopter's two seats. The non-retractable undercarriage has three wheels in a tricycle configuration.

Operators edit

  Czechoslovakia

Specifications edit

General characteristics

  • Crew: 1
  • Capacity: 1 passenger or 220 lbs. payload
  • Length: 10.5 m (34 ft 5 in)
  • Height: 2.3 m (7 ft 7 in)
  • Empty weight: 370 kg (816 lb)
  • Gross weight: 585 kg (1,290 lb)
  • Max takeoff weight: 580 kg (1,279 lb)
  • Powerplant: 1 × Praga DH four-cylinder, air-cooled, horizontally-opposed, 62 kW (83 hp)
or 1x Avia M 110H 4-cylinder air-cooled piston engine rated at 78.3 kW (105 hp)
  • Main rotor diameter: 3 × 8.8 m (28 ft 10 in)
  • Main rotor area: 60.83 m2 (654.8 sq ft)

Performance

  • Maximum speed: 126 km/h (78 mph, 68 kn)
  • Cruise speed: 100 km/h (62 mph, 54 kn)
  • Range: 150 km (93 mi, 81 nmi)
  • Service ceiling: 3,030 m (9,940 ft)

References edit

Notes
  1. ^ . Národní technické muzeum (in Czech). Archived from the original on 2018-09-30. Retrieved 2018-09-30.
  2. ^ Taylor, John William Ransom (1968). Helicopters and VTOL aircraft. Doubleday.
  3. ^ Lambermont, Paul Marcel; Anthony Pirie (1970). Helicopters and autogyros of the world. Barnes. p. 35.
  4. ^ International Aeronautic Federation (1959). "Interavia". 14. Interavia: 64. {{cite journal}}: Cite journal requires |journal= (help)
  5. ^ Jane, Frederick Thomas; Charles Grey Grey; Leonard Bridgman; Leonard Howard-Flanders (1959). Jane's all the world's aircraft 1959-1960. S. Low Marston & company. p. 112.
  6. ^ United Service and Royal Aero Club (Great Britain) and Royal Aero Club of the United Kingdom (1960). "Flight International". 77. IPC Transport Press Ltd.: 714. {{cite journal}}: Cite journal requires |journal= (help)
  7. ^ United Service and Royal Aero Club (Great Britain) and Royal Aero Club of the United Kingdom (1959). "Flight International". 75. IPC Transport Press Ltd.: 683. {{cite journal}}: Cite journal requires |journal= (help)
  8. ^ Jane, Frederick Thomas (1966). Jane's all the world's aircraft. S. Low Marston & company. p. 478.
  9. ^ United Service and Royal Aero Club (Great Britain) and Royal Aero Club of the United Kingdom (1962). "Flight International". 81. IPC Transport Press Ltd.: 894. {{cite journal}}: Cite journal requires |journal= (help)
  10. ^ Underwood, John W., ed. (1961). World Aircraft Illustrated. 1. Aero Publishers.{{cite journal}}: CS1 maint: untitled periodical (link)
Bibliography
  • Beneš, Ladislav. (In Czech) Československé vrtulníky známé i neznámé. Votobia, 1998. ISBN 978-80-7198-326-2.

aero, heli, baby, seat, general, purpose, light, utility, helicopter, designed, engineer, jaroslav, Šlechta, produced, czechoslovak, company, aero, vodochody, 1950s, three, blade, main, rotor, blade, tail, rotor, helicopter, entirely, metal, frame, cockpit, wi. The Aero HC 2 Heli Baby is a two seat general purpose light utility helicopter designed by engineer Jaroslav Slechta and produced by the Czechoslovak company Aero Vodochody in the 1950s It has a three blade main rotor and a two blade tail rotor The helicopter has an entirely metal frame and cockpit and windows made of Plexiglas It was the first and the only Czechoslovak designed helicopter to be produced 2 Aero HC 2 Heli BabyHC 2 in flightRole Light helicopterNational origin CzechoslovakiaManufacturer Aero VodochodyDesigner Jaroslav SlechtaFirst flight December 3 1954Introduction 1955Produced 1958 1962 1 Number built 23 including 2 prototypes Contents 1 Design and development 2 Operators 3 Specifications 4 ReferencesDesign and development editThe helicopter was designed by engineer Jaroslav Slechta 3 Construction of the prototype began in 1951 and testing commenced in 1954 The first flight occurred on December 3 1954 and the helicopter was introduced to the public in 1955 at the Brno Industries Fair 4 Production was slated to begin in 1957 however engine problems delayed it The initial run produced 200 of these helicopters 5 The Czechoslovak Air Force was a user of the HC 2 as was the Czechoslovak People s Army The Heli Baby is capable of carrying a pilot and 220 pounds of cargo at the speed of 62 mph while using 4 85 gallons of fuel 6 In 1959 it was one of the world s lightest two seated helicopters 7 Initially powered by an 83 hp 62 kW Praga DH engine the more powerful 105 hp 78 kW Avia M 110H engine designed specifically for use in helicopters replaced it after approximately six years 8 9 The Heli Baby can be used for transport training and various other duties in military and civil service 10 Cargo space is situated behind the helicopter s two seats The non retractable undercarriage has three wheels in a tricycle configuration Operators edit nbsp CzechoslovakiaCzechoslovak Air ForceSpecifications editGeneral characteristics Crew 1 Capacity 1 passenger or 220 lbs payload Length 10 5 m 34 ft 5 in Height 2 3 m 7 ft 7 in Empty weight 370 kg 816 lb Gross weight 585 kg 1 290 lb Max takeoff weight 580 kg 1 279 lb Powerplant 1 Praga DH four cylinder air cooled horizontally opposed 62 kW 83 hp or 1x Avia M 110H 4 cylinder air cooled piston engine rated at 78 3 kW 105 hp dd Main rotor diameter 3 8 8 m 28 ft 10 in Main rotor area 60 83 m2 654 8 sq ft Performance Maximum speed 126 km h 78 mph 68 kn Cruise speed 100 km h 62 mph 54 kn Range 150 km 93 mi 81 nmi Service ceiling 3 030 m 9 940 ft References edit nbsp Wikimedia Commons has media related to Aero HC 2 Heli Baby Notes Vrtulnik HC 2 VR 2 Heli Baby Narodni technicke muzeum in Czech Archived from the original on 2018 09 30 Retrieved 2018 09 30 Taylor John William Ransom 1968 Helicopters and VTOL aircraft Doubleday Lambermont Paul Marcel Anthony Pirie 1970 Helicopters and autogyros of the world Barnes p 35 International Aeronautic Federation 1959 Interavia 14 Interavia 64 a href Template Cite journal html title Template Cite journal cite journal a Cite journal requires journal help Jane Frederick Thomas Charles Grey Grey Leonard Bridgman Leonard Howard Flanders 1959 Jane s all the world s aircraft 1959 1960 S Low Marston amp company p 112 United Service and Royal Aero Club Great Britain and Royal Aero Club of the United Kingdom 1960 Flight International 77 IPC Transport Press Ltd 714 a href Template Cite journal html title Template Cite journal cite journal a Cite journal requires journal help United Service and Royal Aero Club Great Britain and Royal Aero Club of the United Kingdom 1959 Flight International 75 IPC Transport Press Ltd 683 a href Template Cite journal html title Template Cite journal cite journal a Cite journal requires journal help Jane Frederick Thomas 1966 Jane s all the world s aircraft S Low Marston amp company p 478 United Service and Royal Aero Club Great Britain and Royal Aero Club of the United Kingdom 1962 Flight International 81 IPC Transport Press Ltd 894 a href Template Cite journal html title Template Cite journal cite journal a Cite journal requires journal help Underwood John W ed 1961 World Aircraft Illustrated 1 Aero Publishers a href Template Cite journal html title Template Cite journal cite journal a CS1 maint untitled periodical link BibliographyBenes Ladislav In Czech Ceskoslovenske vrtulniky zname i nezname Votobia 1998 ISBN 978 80 7198 326 2 Retrieved from https en wikipedia org w index php title Aero HC 2 Heli Baby amp oldid 1168692921, wikipedia, wiki, book, books, library,

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