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词条 Teichfuss LT.12 Biposto
释义

  1. Design and development

  2. Operators

  3. Specifications

  4. References

name=LT.12 Biposto image= caption=

}}{{Infobox Aircraft Type

type=Training glider national origin=Italy manufacturer=F.A.L. Teichfuss (Fabrica Alianti Teichfuss), la Aie, Pavulla designer=Luigi Teichfluss first flight=1933 introduced= retired= status= primary user= more users= produced= number built=3 program cost= unit cost= developed from= variants with their own articles=
}}

The Teichfuss LT.12 Biposto ({{lang-en|two-seat}}) was an Italian tandem seat primary glider designed by Luigi Teichfuss and flown in 1933.

Design and development

Before World War II, most glider pilots made their first flights solo on low cost single seat aircraft like the Zögling, even though those starting to fly powered aircraft flew with an instructor in a dual control machine.[1] Luigi Teichfuss saw the advantages of ab initio dual control training early in the 1930s and began the design of his LT.12 in 1932. It was intended to be simple and robust.

The LT.12 was a braced high-wing monoplane, with a wing that was rectangular in plan out to very near the blunt tips where the chord reduced slightly. The wing was held high over the fuselage on two plywood covered pillars like a cut-away pedestal, forward and aft of the rear, underwing, open cockpit. The forward cockpit was ahead of the leading edge. Two parallel faired struts braced the wing on each side from about mid-span to the lower fuselage longerons. The fuselage was a deep sided, almost rectangular hexagonal, plywood skinned wooden structure which tapered to the tail. The LT.12's tailplane was mounted on top of the fuselage, with a straight, swept leading edge and carrying balanced elevators, the balances reducing the leading edge sweep outboard. The small fin was triangular, carrying a broad balanced rudder which moved in an elevator cut-out. The LT.12 had both a standard landing skid from nose to below the wing trailing edge combined with a rudder protecting tail bumper and a narrow track wheeled undercarriage, attached to the skid on half axles and with trailing struts.

At least one LT.12 was used for pilot training by the Pavulla club and some of the three built were sold to other aero clubs.[5]

Operators

  • Pavulla training school

Specifications

{{Aircraft specs
|ref= Pedrielli (2011) pp.40-1
|prime units?=met


|genhide=
|crew=Two
|length m=8.22
|length note=
|span m=15.40
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=28
|wing area sqft=
|wing area note=
|aspect ratio=8.50
|airfoil=
|empty weight kg=331
|empty weight note=
|gross weight kg=481
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|more general=


|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=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=16:1 at {{convert|65|km/h|mph|abbr=on|0}}[5]
|sink rate ms= 1.05
|sink rate note=minimum[5]
|lift to drag=
|wing loading kg/m2=17
|wing loading lb/sqft=
|wing loading note=
|more performance=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

1. ^{{cite book |title=Sailplanes 1920-1945 |last=Simons |first=Martin |edition=2nd revised |year=2006|publisher= EQIP Werbung & Verlag GmbH|location=Königswinter |isbn=3 9806773 4 6|pages=47–9}}
2. ^{{cite web |url=http://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/planeur-fiche_0int.php?code=1523|title= Teichfuss LT-12 Biposto|accessdate=22 November 2013}}
[1][2]
}}{{Teichfuss aircraft}}

1 : Italian sailplanes 1930–1939

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