FIAT A 80 RC 41 Nembo
1935 - primi anni '40
Description
The FIAT A 80 is a twin-row, radial aircraft engine with 18 cylinders, with a max. power of 1000 hp. Before the 1930’s FIAT mainly developed liquid-cooled aircraft engines so the FIAT A 74 and the FIAT A 80 have been the first high power air-cooled airplane engines produced by FIAT. These engines, produced in vaious versions, have been derived from a Pratt and Whitney model and have been then developed by FIAT with several original design improvements. Despite they have been produced in a large number up to the first part of the 1940’s, due to several reasons, only few specimen survived up to nowadays. These engines have been widely used for many Italian military aircrafts up to the 1940’s. The FIAT A 80 was also employed by the Japanese imperial army that used the FIAT B.R.20 bombers during the Second Sino-Japanese War (1937-1945). Before the war few exemples have been also used in some liner aircrafts.
Technical specifications
Manufacturer | FIAT Aviazione, Turin, Italy, from 1935 up to early 1940s |
Type | A 80 RC 41 Nembo |
Description | twin-row 18-cylinder radial engine, crankcase, heads and pistons made of aluminium-alloy, streel-made cylinders screwed into the heads, hemispherical combustion chambers, crankshaft composed of two parts connected by bolts |
Stroke | 165 mm |
Bore | 140 mm |
Displacement | 45720 cm³ |
Compression ratio | 6.70 |
Power | 1000 hp (standard output) at 2100 rpm, at 4100 m with an absolute intake manifold pressure of 0.98 bar |
Specific fuel consumption | 270 g/hp/h at maximum power; 220-230 g/hp/h at 6/10 of maximum power |
Specific power | 21.9 CV/litre |
Valvetrain system | 2 overhead valves per cylinder, operated by pushrods and rocker arms, with exhaust sodium-cooled valves |
Fuel feeding system | with one twin-barrel gasoline FIAT carburetor, placed upstream of the compressor and equipped with pressure limiter and air-fuel mixture preheating |
Supercharging system | with a single-stage centrifugal compressor, driven by the crankshaft by means of a spur gears drive with a speed ratio of 9.37:1, for a full-throttle height of 4100 m |
Ignition system | two spark plugs per cylinder fed by two independent Marelli MF 18 magneto distributors |
Cooling system | air-fed |
Lubrication system | forced by gear pumps |
Starting system | compressed air type with a 12 litres tank at a max. pressure of 15 bar (sufficient for 2 starts) and a Garelli air compressor for re-charging |
Diameter | 1335 mm |
Length | 1620 mm |
Weight | 725 kg |
Mass-to-power ratio | 0.73 kg/hp |
Propeller speed ratio | 0.625:1 by means of a Farman-type bevel gear epicyclic reducer |
Application
Airplanes Aeronautica Umbra Trojani AUT.18 (fighter)
Breda Ba.65 Kite (ground attack aircraft)
Breda Ba.82 (bomber)
CANT Z.509 (seaplane postal and passenger transport)
Caproni Ca.135 (bomber)
Fiat B.R.20 Cicogna (bomber)
FIAT G.18 V (airliner)
Savoia-Marchetti SM79 Sparviero (bomber and torpedo bomber)
Savoia-Marchetti S.M.87 (seaplane airliner)
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