PZL P.6: Difference between revisions

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|type = [[fighter aircraft|Fighter]]
|type = [[fighter aircraft|Fighter]]
|manufacturer =[[PZL]]
|manufacturer =[[PZL]]
|image =
|image = Image:Pzl p-6.jpg
|caption =
|caption =
|designer =
|designer =Zygmunt Puławski
|first flight = August [[1930 in aviation|1930]]
|first flight = August [[1930 in aviation|1930]]
|introduced =
|introduced =
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==Design and development==
==Design and development==
The history of PZL P.6 started in 1928, when a talented designer, Zygmunt Puławski designed an all-metal metal-covered monoplane fighter [[PZL P.1]]. It introduced a high [[gull wing]], giving a pilot an optimal view. The P.1 was powered with an inline engine, and developed a speed of 302 km/h, but remained a prototype, because it was decided, that a fighter for the [[Polish Air Force]] should be powered with a [[radial engine]], licence produced in Poland. Therefore, the next model '''PZL P.6''', was powered with the [[Bristol Jupiter]] VI FH radial engine. It was flown in August [[1930 in aviation|1930]] by [[Bolesław Orliński]]. It had a very similar wing, but a fuselage was thoroughly redesigned - it introduced modern semi-[[monocoque]] design, oval in cross-section, a tail changed as well. As a result, the plane was over 200 kg lighter. The P.6, just like the P.1, met with a huge interest in the world. Their wing design was called the "Polish wing" or "Pulawski wing". During a presentation at the [[Paris Air Show]] in Le Bourget in December [[1931 in aviation|1931]], an aviation press, like ''L'Air'', ''The Aeroplane'', ''Flight'', ''Die Luftwacht'', recognized P.6 as one of the world's top fighters. Then, the prototype P.6, piloted by Orliński, won the American [[National Air Races]] in 29 August-7 September 1931.
The history of PZL P.6 started in 1928, when a talented designer, Zygmunt Puławski designed an all-metal metal-covered monoplane fighter [[PZL P.1]]. It introduced a high [[gull wing]], giving a pilot an optimal view. The P.1 was powered with an inline engine, and developed a speed of 302 km/h, but remained a prototype, because it was decided, that a fighter for the [[Polish Air Force]] should be powered with a [[radial engine]], licence produced in Poland. Therefore, the next model '''PZL P.6''', was powered with the [[Bristol Jupiter]] VI FH radial engine.


The PZL P.6 was flown for the first time in August [[1930 in aviation|1930]] with test pilot [[Bolesław Orliński]] at the controls. It had a very similar wing to the P.1, but the fuselage was completely redesigned with a modern semi-[[monocoque]] configuration introduced that was oval in cross-section, as well, the tail was also changed. As a result of the modifications, the aircraft was over 200 kg lighter.
The PZL P.6 did not enter production, because at the same time the next improved variant [[PZL P.7]] was developed. The first P.7 prototype was basically the P.6 with a stronger engine Bristol Jupiter VII F. Thanks to a charger, it showed better performance on higher altitudes.

The P.6 prototype crashed on 11 October 1931 near [[Częstochowa]] because of a propeller break, resulting in tearing apart of engine. Its pilot, who was Bolesław Orliński, bailed out successfully.


==Technical description==
==Technical description==
All-metal braced high-wing [[monoplane]], [[duralumin]]-covered. The fuselage was framed in in a front section and semi-monocoque in mid and tail sections, oval in cross-section. Two-spar wing of trapezoid shape, thinner by the fuselage, covered with a rimmed Wibault type duralumin sheet, supported with two struts on either side. Pilot's cockpit was open, with a windshield. A fuel tank in a fuselage could be dropped in case of fire emergency. A fixed [[undercarriage]] with a rear skid. radial engine in front, with a [[Townend ring]], two-blade propeller.
The PZL P.6 was an all-metal [[duralumin]]-covered, braced, high-wing [[monoplane]]. The fuselage was framed in a front section and semi-monocoque in mid and tail sections with an oval cross-section. The two-spar wing of trapezoid shape, thinner by the fuselage, covered with a rimmed Wibault type duralumin sheet, was supported by two struts on either side. The pilot's cockpit was open, with a windshield. The [[Bristol Jupiter]] VI FH radial engine mounted in front was fitted with a [[Townend ring]] and used a two-blade propeller. The fixed [[undercarriage]] with a rear skid was mainly conventional and typical of the period. An unusual feature was a fuselage fuel tank that could be dropped in case of a fire emergency.

==Testing and evaluation==
The P.6, just like the P.1, garnered a great deal of interest worldwide. Their wing design was called the "Polish wing" or "Puławski wing". During a presentation at the [[Paris Air Show]] in Le Bourget in December [[1931 in aviation|1931]], the aviation press, such as ''L'Air'', ''The Aeroplane'', ''Flight'' and ''Die Luftwacht'' acknowledged the P.6 as one of the world's top fighter designs. Significantly, the P.6 prototype, piloted by Orliński, won the American [[National Air Races]] in 29 August-7 September 1931.

The PZL P.6 did not enter production, because at the same time the next improved variant, the [[PZL P.7]] was being developed. The first P.7 prototype was basically the P.6 with a more powerful Bristol Jupiter VII F engine. With the provision of a supercharger, it achieved better performance at higher altitudes.

The P.6 prototype crashed on [[11 October]] [[1931]] near [[Częstochowa]] due of a propeller breaking apart, resulting in the engine tearing apart. Its pilot, who was Bolesław Orliński, bailed out successfully.


==Operators==
==Operators==
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}}
}}
==Reference==
==References==
{{Reflist}}
{{reflist}}
* Glass, Andrzej. ''Polskie konstrukcje lotnicze 1893-1939 (Polish aviation constructions 1893-1939)''. Warsaw: WKiŁ, 1977. (Polish language, no ISBN)

* Kopański, Tomasz J. ''PZL P.7: Cz.2''. Gdańsk, Poland: AJ Press, 2001. ISBN 83-7237-081-8.
*Andrzej Glass: "Polskie konstrukcje lotnicze 1893-1939" (''Polish aviation constructions 1893-1939''), WKiŁ, Warsaw 1977 (Polish language, no ISBN)


==External links==
==External links==

Revision as of 03:26, 1 August 2007

Template:Infobox Aircraft The PZL P.6 was a Polish fighter, designed by the engineer Zygmunt Puławski, manufactured by PZL state-owned factor. It remained a prototype.

Design and development

The history of PZL P.6 started in 1928, when a talented designer, Zygmunt Puławski designed an all-metal metal-covered monoplane fighter PZL P.1. It introduced a high gull wing, giving a pilot an optimal view. The P.1 was powered with an inline engine, and developed a speed of 302 km/h, but remained a prototype, because it was decided, that a fighter for the Polish Air Force should be powered with a radial engine, licence produced in Poland. Therefore, the next model PZL P.6, was powered with the Bristol Jupiter VI FH radial engine.

The PZL P.6 was flown for the first time in August 1930 with test pilot Bolesław Orliński at the controls. It had a very similar wing to the P.1, but the fuselage was completely redesigned with a modern semi-monocoque configuration introduced that was oval in cross-section, as well, the tail was also changed. As a result of the modifications, the aircraft was over 200 kg lighter.

Technical description

The PZL P.6 was an all-metal duralumin-covered, braced, high-wing monoplane. The fuselage was framed in a front section and semi-monocoque in mid and tail sections with an oval cross-section. The two-spar wing of trapezoid shape, thinner by the fuselage, covered with a rimmed Wibault type duralumin sheet, was supported by two struts on either side. The pilot's cockpit was open, with a windshield. The Bristol Jupiter VI FH radial engine mounted in front was fitted with a Townend ring and used a two-blade propeller. The fixed undercarriage with a rear skid was mainly conventional and typical of the period. An unusual feature was a fuselage fuel tank that could be dropped in case of a fire emergency.

Testing and evaluation

The P.6, just like the P.1, garnered a great deal of interest worldwide. Their wing design was called the "Polish wing" or "Puławski wing". During a presentation at the Paris Air Show in Le Bourget in December 1931, the aviation press, such as L'Air, The Aeroplane, Flight and Die Luftwacht acknowledged the P.6 as one of the world's top fighter designs. Significantly, the P.6 prototype, piloted by Orliński, won the American National Air Races in 29 August-7 September 1931.

The PZL P.6 did not enter production, because at the same time the next improved variant, the PZL P.7 was being developed. The first P.7 prototype was basically the P.6 with a more powerful Bristol Jupiter VII F engine. With the provision of a supercharger, it achieved better performance at higher altitudes.

The P.6 prototype crashed on 11 October 1931 near Częstochowa due of a propeller breaking apart, resulting in the engine tearing apart. Its pilot, who was Bolesław Orliński, bailed out successfully.

Operators

 Poland

Specifications

General characteristics

  • Crew: 1

Performance Armament

References

  • Glass, Andrzej. Polskie konstrukcje lotnicze 1893-1939 (Polish aviation constructions 1893-1939). Warsaw: WKiŁ, 1977. (Polish language, no ISBN)
  • Kopański, Tomasz J. PZL P.7: Cz.2. Gdańsk, Poland: AJ Press, 2001. ISBN 83-7237-081-8.

External links

Related content

Related development PZL P.1 - PZL P.7 - PZL P.8 - PZL P.11 - PZL P.24 Aircraft of comparable role, configuration, and era Dewoitine D.371 - Loire 46 - Ikarus IK-2 - Polikarpov I-15 Related lists List of fighter aircraft