“Airbridge Fregat-Hydro”的意思、由来-开放百科全书

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Airbridge Fregat-Hydro

释义

Design and development
Specifications (Fregat-Hydro)
References
External links

name=Fregat-Hydro

image=

caption=

}}{{Infobox Aircraft Type

type=Ultralight trike

national origin=Russia

manufacturer=Airbridge

designer=

first flight=

introduced=

retired=

status=In production (2013)

primary user=

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variants with their own articles=
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The Airbridge Fregat-Hydro is a Russian seaplane ultralight trike, designed and produced by Airbridge of Moscow. The aircraft is supplied as a complete ready-to-fly-aircraft.^[1]

Design and development

The Fregat-Hydro was designed to comply with the Fédération Aéronautique Internationale microlight category. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, twin inflatable floats and a single engine in pusher configuration.^[1]

The Fregat-Hydro is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. Its {{convert|9.28|m|ft|1|abbr=on}} span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. On the more recent models the powerplant is a modified liquid-cooled, four-stroke, {{convert|80|hp|kW|0|abbr=on}} Suzuki automotive engine. The aircraft has an empty weight of {{convert|230|kg|lb|0|abbr=on}} and a gross weight of {{convert|500|kg|lb|0|abbr=on}}, giving a useful load of {{convert|270|kg|lb|0|abbr=on}}. With full fuel of {{convert|33|l}} the payload is {{convert|246|kg|lb|0|abbr=on}}.^[1]

Specifications (Fregat-Hydro)

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

|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=9.28
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=16.5
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=230
|empty weight lb=
|empty weight note=
|gross weight kg=500
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|33|l}}
|more general=

|perfhide=
|max speed kmh=130
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=100
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=60
|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=6.5
|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=27.3
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 203. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

{{Official website|http://www.veter50.ru/delt/}}

5 : Russian sport aircraft 2000–2009|Russian ultralight aircraft 2000–2009|Single-engined pusher aircraft|Ultralight trikes|Airbridge aircraft

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