Piaggio P.XIX

Piaggio P.XIX
Type	Air cooled radial
National origin	Italy
Manufacturer	Piaggio
First run	1940
Major applications	Reggiane Re.2002
Developed from	Piaggio P.XI

The Piaggio P.XIX was an Italian aircraft engine produced by Rinaldo Piaggio S.p.A. during World War II and used to power aircraft of the Regia Aeronautica.

Development edit

The engine was part of a line of 14-cylinder radial engines developed from Piaggio based on the Gnome-Rhône Mistral Major, which was itself loosely based on the Bristol Jupiter.^[1] It was derived from the earlier P.XI but with a higher compression ratio.

Variants edit

P.XIX R.C.45 Turbine: Geared, rated altitude 4,500 m (14,800 ft)
P.XIX R.C.50: Geared

Applications edit

The engine was also fitted experimentally to single versions of the IMAM Ro.57 and Savoia-Marchetti SM.82 (serial number MM.60591).^[2]

Specifications (R.C. 45 Turbine) edit

Data from ^{[citation needed]}

General characteristics

Type: 14-cylinder, two row, air cooled radial engine
Bore: 146 mm (5+3⁄4 in)
Stroke: 165 mm (6+1⁄2 in)
Displacement: 38.6 L (2,356 in³)
Diameter: 1,274 mm (50+1⁄4 in)

Components

Valvetrain: 2 x overhead valves per cylinder operated by rockers and pushrods
Supercharger: Centrifugal compressor
Fuel type: 92 Octane petrol
Cooling system: Air-cooled

Performance

Power output:
- Take-off: 1,085 hp (809 kW) at 2400 rpm
- Cruise: 1,144 hp (853 kW) at 2400 rpm at 4,500 m (14,764 ft)
Compression ratio: 7.0:1
Specific fuel consumption: 235 g/(kW•h) (0.38 lb/(hp•h))

References edit

^ Gunston, Bill (1986). World Encyclopedia of Aero Engines. London: Guild Publishing. p. 125.
^ Lopez, Aymeric (2016). "Savoia Marchetti S.82 "Marsupiale"". Italie 1939-1945 (in French). Retrieved 28 August 2018.

External links edit

Re.2002 manual entry for the P.XIX

[1] Gunston, Bill (1986). World Encyclopedia of Aero Engines. London: Guild Publishing. p. 125.

[2] Lopez, Aymeric (2016). "Savoia Marchetti S.82 "Marsupiale"". Italie 1939-1945 (in French). Retrieved 28 August 2018.

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