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词条 Guerpont Autoplum
释义

  1. Design and development

  2. Specifications (Autoplum)

  3. References

  4. External links

name=Autoplum image= caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft national origin=France manufacturer=Roland Mangeard (plans) designer=Maurice Guerpont first flight= introduced= retired= status=Plans available (2015) primary user= more users= produced= number built= program cost= unit cost= €230 (plans only, 2015) developed from= variants with their own articles=
}}

The Guerpont Autoplum is a French ultralight aircraft that was designed by Maurice Guerpont. Plans are supplied by one of the first builders of the type, Roland Mangeard of Pulnoy. The aircraft is supplied as plans only for amateur construction.[1][2]

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under an aircraft canopy with gull winged doors for access, fixed conventional landing gear and a single engine in tractor configuration.[1][2]

The aircraft is made from wood, with its flying surfaces covered in doped aircraft fabric. The Autoplum's tailplane is 50% the area of the main wing, which provides a wide centre of gravity range and a high degree of pitch dampening. Its {{convert|8.60|m|ft|1|abbr=on}} span wing, has an area of {{convert|17.50|m2|sqft|abbr=on}}. Earlier examples were fitted with a {{convert|51|hp|kW|0|abbr=on}} Rotax 462 two-stroke engine, with later ones using the {{convert|64|hp|kW|0|abbr=on}} Rotax 582 two-stroke powerplant or other engines.[1][2]

Specifications (Autoplum)

{{Aircraft specs
|ref=Bayerl and Tacke[1][2]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=8.60
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=17.50
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=230
|empty weight lb=
|empty weight note=
|gross weight kg=420
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|50|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 462
|eng1 type=two cylinder, air-cooled, two stroke aircraft engine
|eng1 kw=
|eng1 hp=52
|prop blade number=2
|prop name=composite, ground adjustable
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=150
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=140
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=50
|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=4
|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=24.0
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 57. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 60. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

External links

  • Photo of a Guerpont Autoplum

3 : French ultralight aircraft 2000–2009|Homebuilt aircraft|Single-engined tractor aircraft

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