Английская Википедия:Isotta Fraschini Delta

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Шаблон:Infobox Aircraft Engine

The Delta was a 12-cylinder inverted-V aircraft engine built by Isotta Fraschini prior to and during World War II.[1]

Design and development

The Delta is a fairly rare example of a large air-cooled inline engine, which normally have cooling problems with the rearmost cylinders. It produced about 750 hp in common versions, although others were rated up to 900 hp. The Delta was not widely used, although it could be found on a number of production aircraft and some advanced prototypes.

The engine included a number of otherwise advanced features. For instance, the valves were powered by dual overhead cams driven by power shafts at the rear of the engine. Exhaust ports were arranged to exit toward the middle of the engine, one cylinder bank being the mirror of the other, allowing the piping to be ganged below the engine nacelle.

Variants

Delta R.C.20/55 ID-IS
Delta R.C.21/60
Delta R.C.35
Delta R.C.35 I
Delta R.C.35 IS
Delta R.C.40 IS
Delta R.C.40 ID-IS
Delta R.C.48
Delta III R.C.40
Delta IV R.C.17/50

Applications

Файл:CANT z515-i.jpg
Delta-powered CANT Z.515 floatplane

Specifications (Delta RC35-IDS)

Файл:F11 Museum - Stockholm Skavsta - P1300085.JPG
Frontal view of sectioned engine

Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Commons category Шаблон:Reflist

Bibliography

Шаблон:Refbegin

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. Шаблон:ISBN
  • Jane's Fighting Aircraft of World War II. London. Studio Editions Ltd, 1989. Шаблон:ISBN
  • Wilkinson, Paul H. Aircraft engines of the World 1945. New York, Paul H. Wilkinson, 1945.

Шаблон:Refend

Шаблон:Isotta Fraschini aeroengines

  1. Gunston 1989, p.82.