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
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
- P.XIX R.C.45 Turbine
- Geared, rated altitude 4,500 m (14,800 ft)
- P.XIX R.C.50
- Geared
Applications
- CANT Z.1007ter
- Macchi MC.200bis prototype
- Reggiane Re.2002
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)
Data from
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))
See also
Comparable engines
- Alfa Romeo 135
- Bristol Taurus
- Fiat A.74
- Gnome-Rhône 14N
- Mitsubishi Kinsei
- Nakajima Sakae
- Pratt & Whitney R-1830 Twin Wasp
- Shvetsov ASh-82
- Tumansky M-88
Related lists
References
- ↑ 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
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