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Страна : Великобритания

Год : 1938

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M.Simons The World's Vintage Sailplanes 1908-45

THE KIRBY PETREL

  In 1938 the speedway rider Frank Charles visited Slingsby’s factory and asked the firm to build for him an improved version of the Rhoenadler. The design was not to be altered fundamentally but the wing was to be given the ‘gull’ form. By cranking the wing down toward the centre, the roots could be faired neatly into the streamlined fuselage at shoulder level. For the cockpit canopy Charles returned to an older idea. The canopy was made wholly of plywood with large portholes. He believed the airflow would be smoother, even with the holes, than over the wooden-framed transparent type.
  The Petrel made its first flight in December, 1938. Orders for eight were received but they were to be fitted with transparent canopies and some were to have fixed tailplanes with elevators. Two Petrels entered the British National Competitions in 1939. Saturday 12th July was tragic, and gave the Petrel a dubious place in the history of soaring. Charles took oil on a winch launch in conditions of low cloud and occasional rain showers. As he climbed he entered cloud and the winch driver reduced power, expecting the glider to release the cable. Charles emerged from the cloud, and turned downwind, cable still on. The winch driver was unable to cut the cable in time, the glider was pulled up sharply at the end of its tether, and dived vertically to the ground. Charles was killed instantly. The accident was witnessed by John Furlong, who, with his friend Leonard Ottley, later developed the OTTFUR safety release for sailplanes. Many lives have been saved since then, and now no sailplane is launched by winch or car tow without either an OTTFUR or some equivalent type of ‘back release'.
  Only three Petrels were completed by the Slingsby works. One was wrecked in the accident: the other two still survive and fly regularly in Britain. One has a pendulum elevator and the other has a fixed tailplane with hinged elevator.

  Technical data:
  Petrel: Span. 17.34 m. Wing area. 16.72 sq m. Aspect ratio. 17.9. Empty weight. 199.5 kg. Flying weight. 289.5 kg. Wing loading. 17.5 kg/sq m. Wing section. Goettingen 652 modified (as on Rhoenadler) at the roots, tapering to Clark YH with washout at the tips.

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Описание:

  • M.Simons The World's Vintage Sailplanes 1908-45
  • M.Hardy. Gliders & Sailplanes of the world
  • Фотографии