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词条 Dyn'Aéro R180
释义

  1. Design and development

  2. Operational history

  3. Specifications (R180)

  4. See also

  5. References

name= R180 image= caption=

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 type=Amateur-built aircraft national origin=France manufacturer=Dyn'Aéro designer= first flight= introduced= retired= status=Production completed (2017) primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
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The Dyn'Aéro R180 is a France amateur-built aircraft that was designed and produced by Dyn'Aéro of Darois. When it was available the aircraft was supplied as plans and as a kit for amateur construction.[1]

As of March 2017 the design is no longer advertised as available by the company.[2]

Design and development

The R180 was designed for competition aerobatics and also as a military trainer. It features a cantilever low-wing, low-mounted tailplane, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed conventional landing gear with wheel pants and a single engine in tractor configuration. A tricycle landing gear version was also designed.[1]

The aircraft is made from wood and carbon fibre. Its {{convert|8.72|m|ft|1|abbr=on}} span wing has an area of {{convert|8.31|m2|sqft|abbr=on}}, mounts full-span ailerons and lacks flaps and winglets. The standard engine specified is the {{convert|180|hp|kW|0|abbr=on}} Lycoming O-360 four-stroke aircraft engine.[1]

Operational history

Reviewers Roy Beisswenger and Marino Boric described the design in a 2015 review as having better control harmony than the Mudry CAP 10.[1]

Specifications (R180)

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


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=8.72
|span ft=
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|wing area sqm=8.31
|wing area sqft=
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|aspect ratio=
|airfoil=
|empty weight kg=470
|empty weight lb=
|empty weight note=
|gross weight kg=750
|gross weight lb=
|gross weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Lycoming O-360
|eng1 type=four cylinder, air-cooled, four stroke aircraft engine
|eng1 kw=
|eng1 hp=180
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=342
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=301
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=93
|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=8
|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=90.3
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

See also

  • List of aerobatic aircraft

References

1. ^1 2 3 4 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 96. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
2. ^{{cite web|url = http://www.dynaero.com/en/|title = Aircraft|accessdate = 30 March 2017|author=Dyn'Aéro|work = dynaero.com/ |year=2014}}
{{Dyn'Aéro aircraft}}

2 : Homebuilt aircraft|Single-engined tractor aircraft
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