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词条 Landray GL.01
释义

  1. Design and development

  2. Specifications

  3. References

  4. External links

name=Landray GL.01 image= caption=

}}{{Infobox Aircraft Type

type=Two seat tandem-wing homebuilt aircraft national origin=France manufacturer= designer=Gilbert Landray first flight=August 1976 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Landray GL.01 is a small tandem-wing, side-by-side seat sport aircraft of the Mignet Pou-du-Ciel type. Built in the mid 1970s, the single example remains active.

Design and development

In the later 1970s Gilbert Landray began to build the first of a series of tandem-wing light aircraft in the Mignet Pou-du-Ciel tradition and closest to the Croses Criquet in implementation. Like the Criquet the GL.01 is a two-seat tractor configuration aircraft with side-by-side seating.

The forward wing of the GL.01 is a one piece structure, mounted so that its angle of incidence can be varied from 2° to 14° by the pilot.[3] The wing is held above the fuselage on two tall and slightly diverging faired struts, with pivots at their tops. Two further pivots are placed at the ends of lighter struts further out on the wing. Two vertical links from the cockpit to the rear of the wing are connected to the control column. The fixed rear wing is fabric covered and fitted with two metal flaps. Yaw stability and control are provided by a small fin and large, deep, balanced rudder, both entirely wooden and angular. Unusually, the rudder balance surface is below the fuselage.

The GL.01 has a wooden fuselage with seats enclosed under a perspex canopy. It is powered by a {{convert|90|hp|kW|abbr=on|0|order=flip}} Continental C90-8F flat four engine, driving a two blade propeller. It has a fixed tailwheel undercarriage, with spatted main wheels on arched, glass fibre, cantilever legs and a tailwheel semi-recessed into the bottom of the rudder.

The GL.01 made its first flight in August 1976.[6] It remains on the French civil aircraft register in 2014,[7] having been based at Marennes since 2003.[8]

Specifications

{{Aircraft specs
|ref=Jane's All the World's Aircraft 1981, p.487
|prime units?=met


|genhide=
|capacity=Two
|length m=5.00
|length note=
|upper span m=7.40
|upper span note=(front wing)
|lower span m=6.70
|lower span note=(rear wing)
|height m=2.10
|wing area sqm=15.50
|wing area note=
|aspect ratio=
|airfoil=NACA 23012[3]
|empty weight kg=361
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=625
|max takeoff weight note=
|fuel capacity={{convert|80|l|impgal USgal|abbr=on|0}}
|more general=


|eng1 number=1
|eng1 name=Continental C90-8F
|eng1 type=flat four
|eng1 hp=90
|eng1 shp=
|eng1 note=
|power original=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=220
|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=700
|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=
|more performance=

  • Take-off run: {{convert|300|ft|m|abbr=on|-1|order=flip}}
  • Landing speed: {{convert|80|km/h|mph kn|abbr=on|0}}
  • Landing distance: {{convert|200|ft|m|abbr=on|-1|order=flip}}

}}

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=147}}
2. ^{{cite book |title=European registers handbook 2014 |last= Partington |first=Dave |coauthors= |edition= |year=2014|publisher= Air Britain (Historians) Ltd|location= |isbn=|page=}}
3. ^{{cite web |url=http://www.aero-constructeurs-amateurs-atlantique.fr/joomla/constr-acaa/163-const-landray|title= Les constructions d'Etienne Landray.|date= |work= |publisher= |accessdate=27 November 2014}}
4. ^{{cite web |url=http://pouguide.org/avions-de-gilbert-landray|title= Les Avions de Gilbert Landray – GL 1 |author=Etienne-Claude Landray |date= |work= |publisher= |accessdate=27 November 2014}}
[1][2][3][4]
}}

External links

  • NACA 23012 airfoil
{{Landray aircraft}}

4 : Homebuilt aircraft|Tandem-wing aircraft|French sport aircraft 1970–1979|Aircraft first flown in 1976

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