- Source: Gnome Lambda
The Gnome 7 Lambda was a French designed, seven-cylinder, air-cooled rotary aero engine that was produced under license in Britain and Germany. Powering several World War I-era aircraft types it was claimed to produce 80 horsepower (60 kW) from its capacity of 12 litres (730 cubic inches) although recorded figures are lower.
Just under 1,000 units were produced in Britain, the majority (967) by the Daimler Company of Coventry. A 14-cylinder variant was known as the Gnome 14 Lambda-Lambda.
In Germany Motorenfabrik Oberursel license-built the seven-cylinder engine as the Oberursel U.0 and later copied the 14-cylinder design and designated it as the Oberursel U.III.
Variants
Gnome 7 Lambda
Seven-cylinder, single-row rotary engine.
Gnome 7 Lambda (long stroke)
Increased stroke of 145 mm (5.71 in) to raise the compression ratio to 3.87:1, and total displacement to 12.26 litres (748 cu in).
Gnome 14 Double Lambda
14-cylinder, two-row rotary engine using Lambda cylinders. 160 hp (120 kW).
Motorenfabrik Oberursel U.0
German production of the Gnome 7 Lambda – had a 124 mm (4.88 in) cylinder bore and 140 mm (5.51 in) piston stroke for a total displacement of 11.52 litres (703 cu in), external diameter of 1.020 metres (40.16 in).
Motorenfabrik Oberursel U.III
German production of the Gnome 14 Double Lambda
Applications
List from Lumsden
= Gnome 7 Lambda
== Gnome 14 Lambda-Lambda
=Survivors
An original Gnome 7 Lambda engine is installed in the Sopwith Tabloid replica aircraft on display in the Grahame-White hall of the Royal Air Force Museum London.
Specifications (Gnome 7 Lambda)
Data from Lumsden.
= General characteristics
=Type: 7-cylinder, single-row, rotary engine
Bore: 124 mm (4.9 in)
Stroke: 140 mm (5.5 in)
Displacement: 11.8 L (720 cu in)
Length: 112 cm (44 in)
Diameter: 93 cm (37 in)
Dry weight: 96 kg (212 lb)
= Components
=Valvetrain: Automatic centre-piston inlet valve, overhead exhaust valve (one each per cylinder)
Cooling system: Air-cooled
Reduction gear: Direct drive, right-hand tractor, left-hand pusher
= Performance
=Power output: 50.3 kW (67.5 hp) at 1,250 rpm (maximum power)
Compression ratio: 3.75:1
See also
Comparable engines
Clerget
Le Rhône
Related lists
List of aircraft engines
References
= Notes
== Bibliography
=Kata Kunci Pencarian:
- Fokker M.5
- Gnome Lambda
- Gnome et Rhône
- Rotary engine
- Farman HF.20
- Sopwith Tabloid
- Gnome Monosoupape
- Motorenfabrik Oberursel
- Bristol Scout
- Fokker M.5
- Avro 504
