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词条 GyroTec DF02
释义

  1. Design and development

  2. Specifications (DF02)

  3. References

  4. External links

name=DF02 image= caption=

}}{{Infobox Aircraft Type

type=Autogyro national origin=Germany manufacturer=GyroTec Michael Obermaier designer= first flight= introduced= retired= status=In production (2013) primary user= more users= produced= number built= program cost= unit cost= €33,500 (assembled, 2011) developed from= variants with their own articles=
}}

The GyroTec DF02 is a German autogyro, designed and produced by GyroTec Michael Obermaier of Wörth am Rhein. The DF02 is supplied as complete ready-to-fly-aircraft.[1]

Design and development

The DF02 features a single main rotor, a single-seat enclosed cockpit with an optional bubble canopy, tricycle landing gear and a twin cylinder, liquid-cooled, two-stroke, dual-ignition, fuel-injected {{convert|70|hp|kW|0|abbr=on}} Hirth 3503 engine in pusher configuration.[1]

The aircraft uses a {{convert|7.45|m|ft|1|abbr=on}} diameter, high-inertia Averso Aviation rotor, with a chord of {{convert|21.6|cm|in|1|abbr=on}}. The rotor head was designed by GyroTec and includes a disc-style rotor brake, pre-rotator and integral articulation stops. The DF02 has an empty weight of {{convert|175|kg|lb|0|abbr=on}} and a gross weight of {{convert|300|kg|lb|0|abbr=on}}, giving a useful load of {{convert|125|kg|lb|0|abbr=on}}.[1]

The bubble canopy can be removed for flight in warm weather. In 2009 the canopy size was increased to accommodate taller pilots.[1]

Specifications (DF02)

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


|genhide=
|crew=one
|capacity=
|length m=
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|width m=
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|airfoil=
|empty weight kg=175
|empty weight lb=
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|gross weight kg=300
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|62|l}}
|more general=


|eng1 number=1
|eng1 name=Hirth 3503
|eng1 type=twin cylinder, liquid-cooled, two-stroke, dual-ignition, fuel-injected aircraft engine
|eng1 kw=
|eng1 hp=70
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=1
|rot dia m=7.45
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=180
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=120
|cruise speed mph=
|cruise speed kts=
|cruise 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=5.5
|climb rate ftmin=
|climb rate note=
|time to altitude=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 180. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

  • {{Official website|http://www.gyrotec.de/}}

2 : German sport aircraft 2000–2009|Single-engined pusher autogyro

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