Lorraine Pétrel
12H Pétrel | |
---|---|
Type | Upright water-cooled V-12, supercharged and geared aeroengine
|
National origin | France |
Manufacturer | Société Lorraine, Argenteuil |
First run | 1932[1] |
Major applications | Potez 542
|
The Lorraine 12H Pétrel was a French V-12
Design and development
During the 1930s
The Pétrel was an upright V-12 engine with two banks of six cylinders, arranged at 60° to each other, driving a common
Steel cylinder liners were screwed into the heads, with their lower parts projecting into the crankcase. Steel seats for valves and sparking plugs were shrunk into the heads. The pistons were forged from
The Pétrel had four overhead valves per cylinder, two exhaust and two inlet, in bronze valve guides. Each bank had its own
Engine lubrication was by forcing pressurized oil through the crankshaft, with sump scavenging. The supercharger had its own lubrication system.[2]
First run in 1932, the early Pétrels produced only 370 kW (500 hp) but by 1938 the engine had been developed into the 12Hars model which gave 640 kW (860 hp). This variant was used by the Koolhoven F.K.55 fighter, where it drove a pair of counter-rotating, twin-bladed propellers.[1]
Operational history
Like the Koolhoven F.K.55, many of the aircraft types to use the Pétrel were one-offs, testing the Lorraine against better known engines from Hispano-Suiza and Rolls-Royce but the
Variants
- 12H Pétrel
- Initial power 370 kW (500 hp).[1]
- 12Ha
- 370 kW (500 hp)
- 12Hars
- 477 kW (640 hp).[1]
- 12Hdr
- 370 kW (500 hp) at 2300 rpm
- 12Hdrs
- 536 kW (719 hp) at 2300 rpm
- 12Hfrs Normale
- 536 kW (719 hp).[2]
- 12Hfrs Chasse
- Designed for fighter aircraft produced higher powers, 567 kW (760 hp) at 2,800 rpm and 4,000 m (13,000 ft).[2]
- 12Hgrs
- 608 kW (815 hp) at 2800 rpm
Applications
- Breguet Br.19.10
- Fokker D.XVII
- Hawker Fury
- Hawker Hart
- Koolhoven F.K.55
- Nieuport-Delage NiD 82
- Potez 39
- Potez 542
- P.Z.L. P.8/II
- Renard R-31
- Société Aérienne Bordelaise AB-21
- French Motor Torpedo Boat Prototype 40K
Engines on display
- A Pétrel is on display in the aircraft section of the Musée Royal de l'Armée, Brussels.
Specifications (12Hfrs, Normale)
Data from Jane's all the World's aircraft 1938 [2]
General characteristics
- Type: Supercharged upright water-cooled 60° V-12 piston engine
- Bore: 145 mm (5.71 in)
- Stroke: 145 mm (5.71 in)
- Displacement: 28.73 L (1,753 cu in)
- Length: 1,858 mm (73.15 in)
- Width: 707 mm (27.83 in)
- Height: 795 mm (31.30 in)
- Dry weight: with accessories 475 kg (1,047 lb)
Components
- Valvetrain: 4 spring-loaded valves per cylinder, driven in pairs via T-shaped tappets by cams on overhead camshafts, one per block
- epicyclic gears; independent lubrication with dedicated pressure and scavenge pumps
- Fuel system: single or double barrelled Lorraine carburettor at supercharger inlet, supplied by 2 A.M. fuel pumps
- Ignition system: 2 plugs per cylinder; 2 magnetos
- Fuel type: petrol
- Oil system: 1 pressure pump supplies oil via crankshaft, removed from sump by 2 scavenge pumps. Operating pressure 0.49 Mpa (71 psi)
- Cooling system: water
- Reduction gear: 17:11
Performance
- Power output: 536 kW (720 hp) rated at 2,650 rpm and 4,000 m (13,000 ft)
- Compression ratio: 6:1
- Specific fuel consumption: 315 g/(kW.h) (8.0 oz/(hp.h))
- Oil consumption: cruise 12±1 g/(kW.h) (0.33± 0.05 oz/(hp.h))
References
- ^ ISBN 1-85260-163-9.
- ^ ISBN 0-7153-5734-4.