“Schönleber Vento”的意思、由来-开放百科全书

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Schönleber Vento

释义

Design and development
Specifications (Vento)
References

name=Vento

image=

caption=

}}{{Infobox Aircraft Type

type=Ultralight trike

national origin=Germany

manufacturer=Schönleber Metallbau GbR

designer=

first flight=

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retired=

status=In production (2015)

primary user=

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produced=

number built=

program cost=

unit cost= €18,500 (2015)

developed from=

variants with their own articles=
}}

The Schönleber Vento ({{lang-en|italic=yes|Wind}}) is a German ultralight trike designed and produced by Schönleber Metallbau GbR of Schönaich and formerly located in Regensburg. The aircraft is supplied complete and ready-to-fly.^[1]

Design and development

The company has been producing ultralight trikes since the 1990s, mostly to supply local customers and without advertising. The company's main business is metal fabrication.^[1]

The Vento was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|450|kg|lb|0|abbr=on}}. The aircraft has a maximum gross weight of {{convert|400|kg|lb|0|abbr=on}}.^[1]

The aircraft design features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with an optional cockpit fairing, tricycle landing gear and a single engine in pusher configuration.^[1]

The aircraft is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. Its {{convert|9.5|m|ft|1|abbr=on}} span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, liquid-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine, equipped with a 4:1 belt reduction drive to reduce the aircraft's noise signature.^[1]

The aircraft has an empty weight of {{convert|160|kg|lb|0|abbr=on}} and a gross weight of {{convert|400|kg|lb|0|abbr=on}}, giving a useful load of {{convert|240|kg|lb|0|abbr=on}}. With full fuel of {{convert|60|l}} the payload is {{convert|197|kg|lb|0|abbr=on}}.^[1]

A number of different wings can be fitted to the basic carriage, including a special wing for hang glider towing.^[1]

Specifications (Vento)

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

|genhide=
|crew=one
|capacity=one passenger
|length m=
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|empty weight kg=160
|empty weight lb=
|empty weight note=
|gross weight kg=400
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|60|l}}
|more general=

|perfhide=
|max speed kmh=120
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=95
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=50
|stall speed mph=
|stall speed kts=
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|never exceed speed kmh=
|never exceed speed mph=
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|never exceed speed note=
|range km=
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|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
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|glide ratio=
|climb rate ms=3.2
|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=30.8
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|avionics=
}}

References

1. ^¹²³⁴⁵⁶⁷Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 239. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

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