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词条 Sergiuz Czerwiński glider
释义

  1. Design and development

  2. Specifications

  3. References

name= Czerwinski (1927) glider image= caption=

}}{{Infobox aircraft type

type=Basic glider national origin=Poland manufacturer= designer=Sergiuz Czerwinski first flight=1927 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Czerwinski (1927) glider was a simple, open frame, monoplane glider built in Poland to spread enthusiasm for aviation.

Design and development

Sergiuz Czerwiński, no relation of the better known glider designer Wacław Czerwiński, had designed, built and flown his first glider, a biplane, in 1917. In 1927 he, like several other Polish aircraft enthusiasts, saw that gliding offered a cheap route to flying for the young and produced a suitable aircraft, developed in an aeromodelling group he formed at the Słowacki school in Kowel.

The 1927 Czerwiński monoplane glider had a rectangular plan, two part wing, built around a single spar and fabric covered. Instead of conventional ailerons and elevators, the pilot was able to alter the angle of incidence of each half-wing separately. This control system, used by several Polish gliders between about 1924 and 1927, was underpinned by the idea that gliders could obtain lift by capturing the energy of gusts, the pilot increasing the angle of incidence of the whole wing as soon as the upward motion of the glider indicated a horizontal gust. Differential incidence movement controlled roll, like ailerons, and collective operation controlled pitch, removing the need for an elevator.[3]

The Czerwińsk had an open frame fuselage, a flat truss built from ash with I-form chords and cross-members. The pilot sat on the lower chord behind the first cross-member. At the rear the empennage was fabric covered, with a tailplane without elevators and a conventional fin and rudder.[3]

Czerwiński made some dozen successful flights in the Kowel area but felt limited by the generally flat terrain there and presented his glider to ZASPL, the aviation students association of Lviv Polytechnic, who seem to have made no use of it.[3]

Specifications

{{Aircraft specs
|ref=samoloitypl[3]
|prime units?=met


|genhide=
|crew=One
|length m=6.5
|length note=
|span m=13
|span note=
|height in=
|height note=
|wing area sqm=22
|wing area note=
|aspect ratio=7.7
|airfoil=
|empty weight kg=80
|empty weight note=
|gross weight kg=150
|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=
|endurance=
|g limits=
|roll rate=
|glide ratio=11
|sink rate ms=1.2-1
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
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|power/mass=
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}}

References

1. ^{{cite web |url=http://www.samolotypolskie.pl/samoloty/731/126/Czerwinski-szybowiec-1927 |title=Czerwiński szybowiec (1927), 1927|author= |date= |work= |publisher= |accessdate=29 August 2018}}
[1]
}}

2 : Polish sailplanes 1920–1929|Aircraft first flown in 1927

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