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词条 Lebouder Autoplane
释义

  1. Design and development

  2. Specifications

  3. References

  4. External links

name=Autoplane image= caption=

}}{{Infobox Aircraft Type

type=Two seat roadable aircraft national origin=France manufacturer= designer=Robert Lebouder first flight= before July 1973 introduced= retired=1977 status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Lebouder Autoplane was a French amateur built modular roadable aircraft, with a car-like component that could be separated from its aeronautical parts. The sole Autoplane flew and drove successfully in the early 1970s.

Design and development

From a distance or in flight, the two seat Autoplane appeared to be a conventional, single engined, high wing braced monoplane with a fixed tail wheel undercarriage. On the ground the front part of the fuselage was seen to be a seriously modified Vespa 400 micro-car, a common, small, four wheeled, open top two seater powered by an {{convert|18|hp|kW|abbr=on|0|order=flip}} motorcycle engine. For road use this had lights and direction indicators mounted on a nose grille, a forward bumper and, inside, a standard steering wheel but also a set of flight instruments and engine controls. The Autoplane's roadable component also had both the aircraft's {{convert|100|hp|kW|abbr=on|0|order=flip}} Continental air-cooled flat four under the bonnet and the original engine which powered it on the road at up to {{convert|70|km/h|mph|abbr=on|0}}.[1][2]

The Autoplane had a rectangular plan wing. Its rear fuselage, open at the front until the car/forward fuselage was inserted, was attached to the wing underside from about half chord and tapered rearwards to a conventional tail with a triangular dorsal fillet leading to a large rectangular fin and rudder. The horizontal tail, also rectangular in plan, was attached to the fuselage bottom.[1][2]

Joining these two parts into an aircraft took two people a little over half an hour. The steering wheel stowed in the car and the bumper in the rear fuselage, then the car was backed into the fuselage opening and linked to the wings by attaching on each side a single lift strut to a bracket on the lower car body. This positioned the windscreen at the wing leading edge and the side windows enclosed the cabin. Entry was via standard car-type, forward hinged doors. Removing the grille revealed a propeller boss and the propeller was bolted on. The Vespa 400 had been modified so that the front wheels could be swung downward and forward on V struts, forming the Autoplanes's narrow track main undercarriage. Its rear suspension was also modified to allow the wheels to be retracted upwards into the body. After a flight, this procedure was reversed, releasing the car to the road.[1][2]

The date of the first flight is uncertain but it was before 13 July 1973 when the Autoplane received its Certificate of Airworthiness.[1] Later in 1973 it appeared at two RSA meetings, at Montdidier and Montargis, winning four prizes.[2] Lebouder flew it until it was damaged in an accident in 1975. The damage was chiefly confined to the undercarriage and propeller but the Autoplane never flew again, though the road vehicle survived.

Specifications

{{Aircraft specs
|ref=Gaillard (1991), p.121[1]
|prime units?=met


|genhide=
|capacity=Two
|length m=6.4
|length note=
|span m=9.67
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=13.8
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=470
|empty weight note=
|gross weight kg=750
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Continental
|eng1 type=air-cooled flat-four
|eng1 hp=100
|eng1 note=only for use in aircraft mode
|power original=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=200
|max speed note=
|cruise speed kmh=180
|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=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control 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=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
}}

References

1. ^{{cite book |title=Les Avions Francais de 1965 à 1990|last=Gaillard|first=Pierre|year=1991|publisher=Éditions EPA|location=Paris|isbn=2 85120 392 4|pages=121}}
2. ^{{cite book |title= Jane's All the World's Aircraft 1975-76|last= Taylor |first= John W R |coauthors= |edition= |year=1975|publisher=Jane's Yearbooks |location= London|isbn=0 531 03250 7|page= }}
[1][2]
}}

External links

  • Conversion and flight
{{Flying cars}}

4 : Roadable aircraft|French sport aircraft 1970–1979|High-wing aircraft|Aircraft first flown in 1973

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