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GIL BŻ-4 Żuk

The BŻ-4 Żuk ("Beetle" in Polish), formerly known as GIL-4, was a Polish four-seat light helicopter built in the 1950s. Although it pioneered a novel rotor and transmission system, it never entered series production.

Design and development

Work on the GIL-4 began at the Główny Instytut Lotnictwa - Main Aviation Institute (GIL), in Warsaw in 1953, under the leadership of Dipl. Ing. Bronisław Żurakowski, who had earlier designed the experimental BŻ-1 GIL helicopter, the first successful rotating-wing aircraft built in Poland. Progress was slow. The main object was to produce a simple and inexpensive general use light helicopter and to further development of the novel rotor and transmission system, which eliminates vibration and improves control.[1]

The BŻ-4 Żuk was based on a single main three-blade rotor powered by an indigenous 240 kW (320 hp) Narkiewicz WN-4 piston engine in a fuselage made of a steel frame, behind a cabin section.[1] It had an open frame rear boom structure and a fixed four-wheel undercarriage. Main rotor was atypical, for it had a smaller upper steering rotor and was fitted with an automatic stabilization system, of the Hiller principle. The cabin had four doors with two front seats and a rear bench. There were two fuel tanks, 220 L in total.

Four main variants were planned: a passenger version accommodating a pilot and three passengers, an ambulance variant carrying pilot, one stretchers and an attendant, an agricultural variant carrying pilot and spraying or dusting equipment and a dual control trainer.

Testing and evaluation

The first prototype of the BŻ-4 Żuk four-seat helicopter was manufactured and displayed publicly in the Polish Aviation Day Exhibition in August 1956. Due to a long program of ground testing and fixing faults, it flew first only on 10 February 1959 and completed 17 flights for a total of 3 hrs, 40 minutes. The Żuk was still in the development stage when further work was cancelled in favor of the licence production of the Mil Mi-1, that had already started in WSK PZL-Świdnik. The prototype was damaged during landing on 31 August 1959 and despite being repaired, was not used again. Two additional prototypes were not completed.

BŻ-4 prototype in the Polish Aviation Museum

One damaged and incomplete prototype is preserved in the Polish Aviation Museum in Kraków.

Specifications (BŻ-4)

Data from Jane's All the World's Aircraft 1958-59 [2]

General characteristics

Performance

See also

Related development

Aircraft of comparable role, configuration, and era

References

Notes

  1. ^ a b Cynk 1959, p. 72.
  2. ^ Bridgman, Leonard, ed. (1958). Jane's All the World's Aircraft 1958-59. London: Jane's All the World's Aircraft Publishing Co. Ltd. p. 211.

Bibliography

External links