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词条 NHI H-3 Kolibrie
释义

  1. Design

  2. Production

  3. Commercial failure

  4. Production list

  5. Survivors

  6. Specifications (H-3 Kolibrie)

  7. See also

  8. References

name=NHI H-3 Kolibrieimage=File:NHI H-3 Kolibrie PH-NHI AMS 14.03.67 edited-2.jpglong caption=The seventh Kolibrie (manufacturers number 3007) on display at the Aviodrome museum at Schiphol Airport, Amsterdam, in 1967. Actually registered PH-NGV, it wears 'PH-NHI' markings.

}}{{Infobox aircraft type

type = Helicopternational origin = manufacturer = Nederlandse Helikopter Industriedesign group = designer = builder =first flight = introduction =introduced = retired = status = primary user = more users = produced = number built = program cost = unit cost = developed from = variants with their own articles = developed into =
}}

The NHI H-3 Kolibrie (Dutch for "Hummingbird") was a small helicopter developed in the Netherlands in the 1950s by Nederlandse Helikopter Industrie.

Design

The H-3 was a two seat general purpose helicopter. It has a duraluminium tube superstructure, an open cockpit and an undergear of metal skids. The design is distinctive because it is ramjet powered. Two ramjets, one at the tip of each rotor blade, power the helicopter. The small tail rotor is powered by the motion of the main rotor. The ramjets could run at any given fuel, which gave the helicopter a certain versatility.

The ramjets made a complex engine and gear box unnecessary. Kromhout designed and built the ramjets. Each engine generated 196 N thrust. The last models had an improved engine, built by Aviolanda, generating 226 N thrust.

In order to start the ramjets, a small 2 hp auxiliary power unit set the main rotor in motion. At a rotor-speed of 70 rpm, the ramjets would be ignited.

Variants with ski’s, floating devices and medical evacuation stretchers were developed and tested, but these versions were never produced. A version as crop duster was developed, and in due time, the H-3 was mainly marketed as crop dusting helicopter.

Production

The H-3 was assembled at Aviolanda. Subassembly took place at Aviolanda which built the fuselage and at Kromhout which built the engines. Fokker, a subcontractor to NHI, built the rotorblades. Final assembly took place at the newly opened Rotterdam Airport.

The initial production run counted ten helicopters of which the first three were used for development, testing and airworthiness tests. The second production run of ten helicopters was undertaken by Aviolanda after Kromhout left the joint venture. This second production run was to be equipped with an uprated ramjet. It is unsure whether the improved ramjet was ever produced.

Commercial failure

Although the H-3 was considered to be technical success, it never was a commercial success. Despite its low acquisition price, the project became a failure. Several factors contributed to this failure. Firstly, the Hiller OH-23 Raven was provided to the Royal Netherlands Air Force by the United States free of charge, under the Mutual Defense Assistance Pact (MDAP). Secondly, NHI's two most important designers, Jan M. Drees and Gerard F. Verhage, left the company, which never recovered. Thirdly, the ramjets, at the tips of the rotorblades, required a great deal of development to make them acceptable for production, with potential buyers regarding the ramjets as unsafe. Fourthly, the extraordinary fuel consumption of the two ramjets made the helicopter uneconomical to operate, flight time and flight range were quite limited making the helicopter unattractive for commercial or military use.

Production list

Overall, nine H-3’s were built between 1958 and 1959 by NHI at Rotterdam Airport when Kromhout was still a parent company. After Kromhout left, Aviolanda built another two H-3’s at their Papendrecht plant.

The few production models were mainly exported to Israel, Germany, the UK and Netherlands New Guinea. A few models stayed in the Netherlands.

Survivors

The remaining examples that are known of are to be found at the aerospace museum Aviodrome. Aviodrome has one H-2 and one H-3 on display.

Specifications (H-3 Kolibrie)

{{Aircraft specs
|ref=Jane's All The World's Aircraft 1961–62[1]
|prime units?=met


|genhide=
|crew=1
|capacity=1
|length m=4.32
|length ft=
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|height m=2.75
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|wing area sqm=
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|swept area sqm=
|swept area sqft=
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|volume m3=
|volume ft3=
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|aspect ratio=
|airfoil=
|empty weight kg=276
|empty weight lb=
|empty weight note=
|gross weight kg=650
|gross weight lb=
|gross weight note=[2]
|max takeoff weight kg=700
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=400 L (88 Imp Gallons)
|more general=


|eng1 number=2
|eng1 name=NHI TJ-5
|eng1 type=ramjet
|eng1 kn=
|eng1 lbf=51
|eng1 note=
|power original=
|thrust original=
|rot number=1
|rot dia m=9.95
|rot dia ft=
|rot dia in=
|rot area sqm=79.2
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=116
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=100
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|range km=75
|range miles=
|range nmi=
|range note=
|endurance=65 min
|ceiling m=1600
|ceiling ft=
|ceiling note=
|climb rate ms=
|climb rate ftmin=680
|climb rate note=
|time to altitude=
|more performance=
|avionics=
}}

See also

  • Fairey Rotodyne - a gyrodyne (jet tipped rotor driven at take off and landing only)
  • Rotary Rocket - with rocket tipped rotor blades
  • Hiller YH-32 Hornet - another helicopter with ramjet powered rotorblades

References

{{commons category|NHI H-3 Kolibrie at Aviodrome Lelystad}}
1. ^Taylor 1961, p. 117.
2. ^Apostolo 1984, p. 124.
  • Taylor, John W. R. Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company, 1961.
  • Apostolo, Giorgio. The Illustrated Encyclopedia of Helicopters. New York: Bonanza Books, 1984. {{ISBN|0-517-439352}}.

3 : Dutch civil utility aircraft 1950–1959|Dutch helicopters 1950–1959|Tipjet-powered helicopters

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