CNA C.II

Last updated
C.II
Type Horizontally opposed air-cooled twin
National origin Italy
Manufacturer Compagnia Nazionale Aeronautica (CNA)
Produced1937-41

The CNA C.II was a small, air-cooled, two cylinder horizontally opposed aircraft engine designed and built in Italy in the late 1930s.

Contents

Design

The low power, unsupercharged C.II had offset cylinders with special steel barrels and light alloy cylinder heads. The pistons were light alloy castings; the connecting rods were heat treated chrome-nickel steel, with split big ends. The CN.II had a one piece chrome-nickel steel crankshaft running in two roller bearings, with a ball thrust bearing. The crankcase was a one piece light alloy casting. [1]

Applications

Data from Erickson [2]

Specifications

Data from Jane's All the World's Aircraft 1938 [1]

General characteristics

Components

Performance

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References

  1. 1 2 Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. p. 68d. ISBN   0715 35734 4.
  2. Erickson, Jack. "Horizontally Opposed Piston Aero Engines: C.N.A." Retrieved 21 March 2012.