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词条 Yuneec International ETrike
释义

  1. Design and development

  2. Specifications (ETrike)

  3. References

name=ETrike image= caption=

}}{{Infobox Aircraft Type

 type=Ultralight trike national origin=China manufacturer=Yuneec International designer= first flight= introduced= retired= status=Prototypes only primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Yuneec International ETrike is a Chinese electric ultralight trike that was designed and produced by Yuneec International of Kunshan, Jiangsu. The aircraft was originally intended to be supplied complete and ready-to-fly, but does not seem to have progressed beyond a few prototypes.[1]

By 2013 the ETrike was not offered for sale by either Yuneec International or its North American licensee, GreenWing International.[2][3]

Design and development

The ETrike airframe is based upon the Avio Delta Thruster and designed to comply with the American FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}. It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit without a cockpit fairing, tricycle landing gear and a single electric motor 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 {{convert|14|hp|kW|0|abbr=on}} Yuneec Power Drive 10 electric motor.[1]

Specifications (ETrike)

{{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=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=12.3
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=200
|gross weight lb=
|gross weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Yuneec Power Drive 10
|eng1 type=electric aircraft engine
|eng1 kw=
|eng1 hp=14
|prop blade number=2
|prop name=composite
|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=
|cruise speed mph=
|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. ^1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 224. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}}
2. ^{{cite web|url=http://www.yuneec.com/ |title=Yuneec International |publisher=Yuneec.com |date= |accessdate=2013-09-24}}
3. ^{{cite web|url=http://greenwing.aero/ |title=GreenWing International; Electric Aviation |publisher=Greenwing.aero |date= |accessdate=2013-09-24}}
{{Yuneec International aircraft}}

5 : Chinese sport aircraft 2000–2009|Chinese ultralight aircraft 2000–2009|Single-engined pusher aircraft|Electric aircraft|Ultralight trikes
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