Piaggio P.XI
Appearance
| Company type | Aircraft engine |
|---|---|
| Industry | Aerospace |
| Predecessor | Gnome-Rhône Mistral Major 14K (licensed design) |
| Products | 14-cylinder radial aircraft engines |
The Piaggio P.XI was an Italian 14-cylinder radial engine designed for aircraft use. This engine was produced under license in Italy, based on the French Gnome-Rhône Mistral Major 14K design.
Subsequent enhancements resulted in the creation of the P.XIX, which featured a higher compression ratio—increasing from 6:1 to 7:1—and an elevated maximum rpm from 2,400 to 2,600.
Variants
- P.XI
- P.XIbis
- P.XI R.C.15
- (geared, optimized for altitude 1,500 m (4,900 ft))
- P.XI R.C.30
- (geared, optimized for altitude 3,000 m (9,800 ft))
- P.XI R.C.40D
- [1]
- P.XI R.C.40S
- 740 kW (1,000 PS) (geared, optimized for altitude 4,000 m (13,000 ft)), counter-rotating relative to 40D.
- P.XI R.C.40bis
- (geared, optimized for altitude 4,000 m (13,000 ft))
- P.XI R.2C.40
- 740 kW (1,000 PS), (geared, optimized for altitude 4,000 m (13,000 ft)), equipped with a two-speed supercharger.
- P.XI C.40
- (direct drive, optimized for altitude 4,000 m (13,000 ft))
- P.XI R.C.44
- (geared, optimized for altitude 4,400 m (14,400 ft))
- P.XI R.C.50
- (geared, optimized for altitude 5,000 m (16,000 ft))
- P.XI R.C.60
- (geared, optimized for altitude 6,000 m (20,000 ft))
- P.XI R.C.72
- (geared, optimized for altitude 7,200 m (23,600 ft))
- P.XI R.C.100
- P.XI R.C.100/2v
- (geared, optimized for altitude 10,000 m (33,000 ft))
Applications
- Breda Ba.65
- Breda Ba.88
- CANT Z.516
- CANT Z.1007
- Caproni Ca.135
- Caproni Ca.161
- Reggiane Re 2000
- Saab 17C
- (Savoia-Marchetti SM.79B)
- Savoia-Marchetti SM.84
Specifications (P.XI R.C.40)
{{pistonspecs| |ref=Italian Civil & Military Aircraft 1930-1945 and Aircraft Engines of the World 1945. |type=14-cylinder radial engine |bore =146 mm (5.7 in) |stroke =165 mm (6.5 in) |displacement =38.6 L (2,360 cu in) |length=1,700 mm (67 in) |diameter=1,328 millimetres (52.3 in)*
See also
References
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Notes
- ↑ Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value). :740 kW (1,000 PS) (geared, optimized for altitude 4,000 m (13,000 ft))
Bibliography
- Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
- Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
- Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
- Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9