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The Monosoupape (French for single-valve), was a rotary engine design first introduced in 1913 by Gnome Engine Company (renamed Gnome et Rhône in 1915). It used a clever arrangement of internal transfer ports and a single pushrod-operated exhaust valve to replace the many moving parts found on more conventional rotary engines, and made the Monosoupape engines some of the most reliable of the era.
The Gnome Lambda of 1911 was a larger 80 hp (60 kW) version of the Omega, followed by the 9-cylinder 100 hp (75 kW) Gnome Delta in 1914 (also called the Gnome Monosoupape as it used that type of engine design for the first time). Gnome also tried a 14-cylinder two-row version, the Double Lambda of 160 hp (120 kW), but this saw little use, even ...
When compared with the Gnome Monosoupape, the Rhône engines were of a more conventional design [2] with a carburetor mounted on the shaft and intake and exhaust valves mounted on the cylinder heads. Fuel was piped from the hollow shaft to the cylinder heads by copper tubes (mounted at the front of the 80 Horsepower 9C model and at the back on ...
Data from General characteristics Crew: 1 Length: 7.30 m (23 ft 11 in) Wingspan: 13.90 m (45 ft 7 in) Wing area: 30 m 2 (320 sq ft) Empty weight: 350 kg (772 lb) Gross weight: 625 kg (1,378 lb) Powerplant: 1 × Gnome Monosoupape 9 Type B 9-cylinder air-cooled rotary piston engine, 60 kW (80 hp) Propellers: 2-bladed fixed-pitch propeller Performance Maximum speed: 100 km/h (62 mph, 54 kn) Time ...
The Le Rhône 9C is a nine-cylinder rotary aircraft engine produced in France by Société des Moteurs Le Rhône / Gnome et Rhône. Also known as the Le Rhône 80 hp in a reference to its nominal power rating, the engine was fitted to many military aircraft types during the First World War. Le Rhône 9C engines were also produced under license ...
The 100 hp Monosoupape was built with 9 cylinders, and developed its rated power at 1,200 rpm. [15] The later 160 hp nine-cylinder Gnome 9N rotary engine used the Monosoupape valve design while adding the safety factor of a dual ignition system, and was