CWL WZ-X

From Wikipedia, the free encyclopedia

WZ-X

CWL WZ-X prototype, 1926
Type Reconnaissance aircraft
Manufacturer CWL
Maiden flight August 1926
Introduced 1928
Retired 1939
Primary user Polish Air Force
Produced 1926-1927
Number built 4

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.

Contents

[edit] 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, three pre-series aircraft were built (designated WZ-X/II, WZ-X/III, WZ-X/IV). The first two of these were fitted with the same Lorraine-Dietrich 12Eb 478 hp W engine used by the prototype, while the other had a Gnome et Rhône Jupiter 9a 530 hp 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.

[edit] 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.

[edit] Specifications

Data from Glass, A. (1977)

General characteristics

  • Crew: 2, pilot and observer
  • Length: 8.21 m ()
  • Wingspan: 11.31 m ()
  • Height: 3.07 m ()
  • Wing area: 33.2 m² (ft²)
  • Empty weight: 1246 kg ()
  • Loaded weight: 1915 kg ()
  • Useful load: 669 kg ()
  • Max takeoff weight: 1240 kg ()
  • Powerplant: 1× Lorraine-Dietrich 12Eb water-cooled 12-cylinder inline W engine, 478 hp / 450 hp nominal power ()

Performance

Armament

  • 2 fixed front-firing 7.7 mm Vickers machineguns
  • 2 movable 7.7 mm Lewis machineguns
  • light bombs

[edit] See also

  • WZ-III - WZ-IV - CWL WZ-VIII - CWL WZ-IX

Comparable aircraft Breguet 19 - Potez 15 - Potez 25 - Aero A.32

[edit] References

  • Andrzej Glass: "Polskie konstrukcje lotnicze 1893-1939" (Polish aviation constructions 1893-1939), WKiŁ, Warsaw 1977, p. 122-123 (Polish)

[edit] External links


v • d • e
Lists relating to aviation
General
Military
Accidents/incidents
Records
Languages