Lorraine Pétrel

12H Pétrel
Type	Upright water-cooled V-12, supercharged and geared aeroengine
National origin	France
Manufacturer	Société Lorraine, Argenteuil
First run	1932
Major applications	Potez 542

The Lorraine 12H Pétrel was a French V-12 supercharged, geared piston aeroengine initially rated at 370 kW (500 hp), but later developed to give 640 kW (860 hp). It powered a variety of mostly French aircraft in the mid-1930s, several on an experimental basis.

Design and development

During the 1930s Société Lorraine, which in 1937 was nationalised into the Société Nationale de Construction de Moteurs (SNCM), continued its tradition of building large water-cooled aeroengines. These later engines were named after birds: Eider, Courlis (en:curlew), Pétrel and Sterna. The last two remained in production in 1938.^[2]

The Pétrel was an upright V-12 engine with two banks of six cylinders, arranged at 60° to each other, driving a common crankshaft. The cylinder blocks were bolted onto the crankcase, all light alloy parts. The crankcase came in two pieces, with seven crankshaft bearings in the upper section. Roller bearings were used at the crankshaft ends; the remaining five were plain. The upper crankcase section also had integrally cast water channels as part of the cooling system.^[2]

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 alugir, with three compression and one scraper ring and floating bronze bushes for the gudgeon pins. The twelve pistons were connected to the six crankpins in pairs, each with a master and an auxiliary connecting rod. The master rods had forked big ends with white metal bearings; the auxiliary rod ends ran between the forks on bronze bushes.^[2]

The Pétrel had four overhead valves per cylinder, two exhaust and two inlet, in bronze valve guides. Each bank had its own overhead camshaft and each cam operated a pair of valves through T-shaped tappets, the stem of the T moving in a guide to avoid sideways force on the valve stems. There were two sparking plugs per cylinder and twin magnetos. A carburettor fed the mixture into the intake of the supercharger, at the rear of the engine. The Pétrel's output could be left or right handed; a Lorraine patent planet gearset, with six satellite gears, provided an 11:17 reduction of propeller shaft speed.^[2]

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 Potez 542 version of the Potez 540 family were built in numbers, with 74 of these twin-engined, multi-role (bomber, reconnaissance and transport) aircraft supplied to the French and Spanish air forces.

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

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
Supercharger: centrifugal, driven at 8.8 crankshaft speed via 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

^ ^a ^b ^c ^d Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2 ed.). Wellingborough: Patrick Stephens Ltd. p. 95. ISBN 1-85260-163-9.
^ ^a ^b ^c ^d ^e ^f ^g ^h Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. pp. 47d–48d. ISBN 0-7153-5734-4.

[Gun-1] Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2 ed.). Wellingborough: Patrick Stephens Ltd. p. 95. ISBN 1-85260-163-9.

[JAWA38-2] ^ ^a ^b ^c ^d ^e ^f ^g ^h Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. pp. 47d–48d. ISBN 0-7153-5734-4.

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