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词条 CWL WZ.X
释义

  1. Development

  2. Description

  3. Variants

  4. Specifications (WX.X/I)

  5. See also

  6. References

  7. External links

name =WZ.Ximage =CWL WZ-X.jpgcaption =CWL WZ.X prototype, 1926

}}{{Infobox Aircraft Type

type =Reconnaissance aircraftmanufacturer =CWLdesigner =first flight = August 1926introduced = 1928retired = 1939status =primary user = Polish Air Forcemore users =produced = 1926-1927number built = 4unit cost =developed from =variants with their own articles =
}}

The WZ.X was the Polish reconnaissance aircraft designed in the mid-1920s and manufactured in the Centralne Warsztaty Lotnicze (CWL) - Central Aviation Workshops in Warsaw. It was the first combat aircraft of own design built in Poland, in a small series.

Development

The aircraft was designed by Władysław Zalewski, as his tenth design (Zalewski had already constructed aircraft for the Russian Air Force during the World War I). Work started in 1923, and the first prototype was flown in August 1926. Another airframe was built for static trials. Flight trials were successful: its performance was at least as good as the Breguet 19, and better than the Potez 25. However, maintenance was more difficult.

In 1927, two pre-series aircraft were built (designated WZ.X/II, WZ.X/III), powered by {{cvt|450|hp|order=flip}} Lorraine-Dietrich 12Eb used by the prototype, with a fourth (WZ.X/IV) powered by a {{cvt|530|hp|order=flip}} Gnome et Rhône 9A Jupiter radial engine with four-blade propeller.

The WZ.X did not enter serial production, because Poland had already bought many Breguet 19 aircraft from France, and started production under licence of the Potez 25 of the same class. Three WZ.Xs were given to aviation schools, where one or two survived in Dęblin until 1939.

Description

Wooden construction braced biplane, conventional in layout. A fuselage was semi-monocoque, elliptical in cross-section, plywood-covered. Rectangular two-spar wings, covered with canvas and plywood (in front), of equal span, slightly staggered. Ailerons on both wings, joined with struts. Strutted empennage, covered with plywood (stabilizers) and canvas (rudder and elevators). Crew of two, sitting in tandem in open cockpits, the first with a windshield. Conventional fixed landing gear, with a rear skid, the main gear with a common axle. Inline engine in front, driving two-blade tractor wooden propeller, with two round Lamblin radiators under the fuselage (in the WZ.X/IV - radial engine, with four-blade propeller and no radiators). Fuel tank in the fuselage.

The pilot had two fixed 7.7 mm Vickers machine guns with an interrupter gear, the observer had twin 7.7 mm Lewis machine guns on a ring mounting. Bomb load: unknown.

Variants

WZ.X/I
First prototype powered by a {{cvt|450|hp|order=flip}} Lorraine-Dietrich 12Eb
WZ.X/II
Pre-series aircraft essentially similar to the WZ.X/I
WZ.X/III
Pre-series aircraft essentially similar to the WZ.X/I
WZ.X/IV
Pre-series aircraft powered by a {{cvt|530|hp|order=flip}} Gnome et Rhône 9A Jupiter driving a four-bladed propeller

Specifications (WX.X/I)

{{Aircraft specs
|ref=Jane's all the World's Aircraft 1928[1], Polskie konstrukcje lotnicze 1893-1939[2], Polish Aircraft 1893–1939[3]
|prime units?=met


|crew=2
|length m=8.21
|span m=11.31
|height m=3.07
|wing area sqm=33.2
|aspect ratio=
|airfoil=St. Cyr
|empty weight kg=1246
|gross weight kg=1915
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Lorraine-Dietrich 12Eb
|eng1 type=W-12 water-cooled piston engine
|eng1 hp=450
|prop blade number=2
|prop name=fixed-pitch wooden propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|max speed kmh=206
|max speed note=fully loaded; {{cvt|220|km/h|mph kn}} lightly loaded
|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=
|range km=800
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=6325
|g limits=
|roll rate=
|climb rate ms=5.5
|time to altitude=
|wing loading kg/m2=57.7
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|0,1064|hp/lb|kW/kg|order=flip}}
|more performance=


|guns=

2x fixed front-firing {{cvt|7.7|mm|3}} Vickers machine-guns

2x movable {{cvt|7.7|mm|3}} Lewis machine-guns


|bombs=light bombs
|avionics=
}}

See also

{{aircontent|
|related=
|similar aircraft=

Breguet 19 -

Potez 15 -

Potez 25 -

Aero A.32
|lists=
|see also=*WZ-III - WZ-IV - CWL WZ-VIII - CWL WZ-IX
}}

References

1. ^{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |page=178c}}
2. ^{{cite book|last1=Glass|first1=Andrzej|title=Polskie konstrukcje lotnicze 1893-1939|date=1977|publisher=WKiŁ|location=Warsaw|pages=122-123|language=Polish}}
3. ^{{cite book |last=Cynk |first=Jerzy B. |title=Polish Aircraft 1893–1939 |year=1971 |publisher=Putnam |location=London |isbn=978-0-370-00085-5|pages=108-113}}

External links

{{commons category|CWL WZ-X}}
  • Photos and drawings at Ugolok Neba site

4 : Polish military reconnaissance aircraft 1920–1929|Biplanes|Single-engined tractor aircraft|Aircraft first flown in 1926

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