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词条 Dorna Parandeh Abi
释义

  1. Design and development

  2. Operational history

  3. Specifications (Parandeh Abi)

  4. See also

  5. References

  6. External links

name=Prandeh Abi image= caption=

}}{{Infobox Aircraft Type

type=Two-seat light aircraft and trainer national origin=Iran manufacturer=H F Dorna Company, Tehran designer=Mohammad Hassan Karami first flight=27 July 1998 introduced= retired= status= primary user= more users= produced= number built=28+ program cost= unit cost= €120,000 (2015)[1] developed from= variants with their own articles=
}}

The Dorna D-139 Parandeh Abi ({{lang-en|italic=yes|Blue Bird}}) is a low-wing single-engine monoplane built from composite materials in Iran. It is a recreational and training aircraft with side-by-side seating.

Design and development

The design of the Parandeh Abi, Blue Bird in English, was begun in 1994 and the first flight was on 27 July 1998. It is a conventionally laid out low wing single-engine monoplane, built entirely from composite materials and seating two side-by-side. Its two spar wings and single spar horizontal tail are rectangular in plan. The wing carries 2.5° of dihedral and the tips are slightly upturned. Plain flaps fill the trailing edges inboard of the ailerons. The elevators are horn balanced, as is the rudder. Together, the fin and rudder are straight tapered, with a small dorsal fillet.

The Parandeh Abi is powered by a Rotax 914 F3 horizontally opposed four-cylinder engine driving a thee-bladed propeller. Its fixed, self-sprung steel cantilever tricycle undercarriage is attached to the fuselage. All wheels have speed fairings. In early production aircraft, access to the cabin was via the top hinged, upward opening canopy, but later examples have forward hinged doors reaching down almost to the wing. The doors contain a framed window, though the total cabin transparency is noticeably reduced. All models have a pair of small, fixed windows in the tapering fuselage behind the seats, where there is a baggage compartment. The aircraft can be equipped with either a stick or yoke for primary control. Other differences between early and later production models include improved engine cooling with the addition of chin and cheek air intakes, enlarged rudder horn balances, tailplane root fillets and fluted skinning on the ailerons and rudder.

The design was type certified to JAR-VLA standards.[1]

Dorna are also developing a version to meet US LSA requirements, called the Parandeh Sefid or White Bird in English. This differs from the Parandeh Abi chiefly in its engine, which may be either an 84.5 kW (113.3 hp) Rotax 914 UL or a 60 kW (80 hp) Rotax 912 UL. Estimated performance with the 914 UL is similar to that of the Parandeh Abi, though the range is less as a result of a lower fuel capacity.

By the end of 2012 the company's website was gone and the domain was for sale.[2] The company may no longer be in business.

Operational history

Production of the Parandeh Abi began in 2001 with orders for 5 from Iranian flying clubs.

By March 2006 Dorna had orders for 14 and options on another 30 and by November 2008 28 had been built. As well as supplying clubs and training centres, Parandeh Albis also went to the Iranian Police and to the Civil Aviation Organisation.

In 2005 it seemed possible that the aircraft might enter the South African or wider markets. Aviation Advantage of Gauteng sought to buy some complete and to obtain a licence for local manufacture or assembly.[8]

Specifications (Parandeh Abi)

{{Aircraft specs
|ref=Jane's All the World's Aircraft 2010-11
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=6.17
|length ft=
|length in=
|length note=
|span m=9.45
|span ft=
|span in=
|span note=
|height m=2.70
|height ft=
|height in=
|height note=
|wing area sqm=11.06
|wing area sqft=
|wing area note=gross
|aspect ratio=
|airfoil=NACA 63-215
|empty weight kg=490
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=750
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=120 L (26.4 Imp gal, 31.7 US gal)
|more general=


|eng1 number=1
|eng1 name=Rotax 914 F3
|eng1 type=turbocharged flat four, air- and water-cooled
|eng1 kw=
|eng1 hp=
|prop blade number=3
|prop name=MT-Propeller MTV-6-A/172-8
|prop dia m=1.72
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=282
|max speed mph=
|max speed kts=
|max speed note=at 4,267 m (14,000 ft)
|max speed mach=
|cruise speed kmh=161
|cruise speed mph=
|cruise speed kts=
|cruise speed note=economical, at 3,658 m (12,000 ft)
|stall speed kmh=83
|stall speed mph=
|stall speed kts=
|stall speed note=sea level, flaps down
|never exceed speed kmh=321
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=1094
|range miles=
|range nmi=
|range note=with maximum fuel
|endurance=
|ceiling m=4265
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=3.8
|climb rate ftmin=
|climb rate note=at sea level
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

See also

{{aircontent
|see also=
  • Dorna Free Bird, light sport aircraft

|related=
|similar aircraft=
|lists=
}}

References

1. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 152. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
2. ^{{cite web|url = http://www.maplesystems.co.uk/Reserved-Web-Page-pg93.html?domain=www.hfdorna.com|title = Domains for Sale Page|accessdate = 20 December 2012|last = Maple Systems|year = 2012|deadurl = yes|archiveurl = https://web.archive.org/web/20131021185207/http://www.maplesystems.co.uk/Reserved-Web-Page-pg93.html?domain=www.hfdorna.com|archivedate = 21 October 2013|df = }}
3. ^{{cite journal|last=|first=|authorlink=|coauthors=|year=|month=|title=Another new trainer heads for South Africa.|journal=World Airnews|volume=|issue=January 2005|page=51|id=|url=http://www.hfdorna.com/news_media.htm|archive-url=https://web.archive.org/web/20060311030149/http://www.hfdorna.com/news_media.htm|dead-url=yes|archive-date=2006-03-11|accessdate=2011-02-25|quote=}}
[3]
}}

External links

  • {{Official website|http://www.hfdorna.com/}}
  • [https://web.archive.org/web//http://www.hfdorna.com Website archives] on Archive.org

2 : Iranian civil aircraft 1990–1999|Dorna aircraft

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