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词条 Avio Delta Thruster
释义

  1. Design and development

  2. Specifications (Delta Thruster)

  3. References

  4. External links

name=Delta Thruster image= caption=

}}{{Infobox Aircraft Type

type=Ultralight trike national origin=Bulgaria manufacturer=Avio Design designer= first flight= introduced= retired= status=In production (2013) primary user= more users= produced= number built= program cost= unit cost= €6,642 (carriage only, 2011) developed from= variants with their own articles=Yuneec International ETrike
}}

The Avio Delta Thruster is a Bulgarian ultralight trike, designed and produced by Avio Design of Kazanlak. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

Design and development

The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|115|kg|lb|0|abbr=on}}. It is German DULV certified and can be flown with any suitable cable-braced hang glider high-wing. The aircraft features weight-shift controls, a single-seat open cockpit, tricycle landing gear and a single engine in pusher configuration. The hang glider wing can be replaced with a paraglider wing and requires ten minutes to convert.[1]

The aircraft is intended to be quickly folded into a package small enough to fit into a car for ground transport.[1]

The aircraft is made from bolted-together aluminum tubing, with its single or double surface wing covered in Dacron sailcloth. A number of different hang glider and paraglider wings can be fitted to the basic carriage. A typical hang gider wing used would have a {{convert|9.5|m|ft|1|abbr=on}} span and would be supported by a single tube-type kingpost and use an "A" frame weight-shift control bar. The carriage front wheel is adjustable to allow for different pilot leg lengths.[1]

The powerplant is a single cylinder, air-cooled, two-stroke, {{convert|28|hp|kW|0|abbr=on}} Simonini Mini 2 engine. Without the wing, the aircraft has an empty weight of {{convert|32|kg|lb|0|abbr=on}} and a gross weight of {{convert|200|kg|lb|0|abbr=on}}. The fuel tank holds {{convert|10|l}}.[1]

An electric version was under development in 2011.[1]

Specifications (Delta Thruster)

{{Aircraft specs
|ref=Bayerl[1]
|prime units?=met


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=9.5
|span ft=
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|height note=
|wing area sqm=12.3
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=32
|empty weight lb=
|empty weight note=carriage only
|gross weight kg=200
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|10|l}}
|more general=


|eng1 number=1
|eng1 name=Simonini Mini 2
|eng1 type=single cylinder, air-cooled, two stroke aircraft engine
|eng1 kw=
|eng1 hp=28
|prop blade number=2
|prop name=wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
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|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=16.3
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 206. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

  • {{Official website|http://www.avio-delta.com/index.php/en/trikes/8-en/trikes/19-delta-truster}}
{{Avio Design aircraft}}

5 : Bulgarian sport aircraft 2000–2009|Bulgarian ultralight aircraft 2000–2009|Single-engined pusher aircraft|Ultralight trikes|Avio Design aircraft

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