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  2. Gnome Monosoupape - Wikipedia

    en.wikipedia.org/wiki/Gnome_Monosoupape

    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.

  3. Le Rhône - Wikipedia

    en.wikipedia.org/wiki/Le_Rhône

    In 1915 around 45% of all Le Rhône engines manufactured in France were exported to Great Britain, Italy and Russia. Le Rhône series engines proved to be far more popular with aircraft manufacturers than Gnome et Rhône's other major engine series, the Gnome Monosoupape mainly due to the Rhône’s lower fuel and lube oil consumption. [2]

  4. Gnome et Rhône - Wikipedia

    en.wikipedia.org/wiki/Gnome_et_Rhône

    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 ...

  5. Rotary engine - Wikipedia

    en.wikipedia.org/wiki/Rotary_engine

    Castor oil was the lubricant of choice, as its lubrication properties were unaffected by the presence of the fuel, and its gum-forming tendency was irrelevant in a total-loss lubrication system. An unfortunate side-effect was that World War I pilots inhaled and swallowed a considerable amount of the oil during flight, leading to persistent ...

  6. Caudron Type G - Wikipedia

    en.wikipedia.org/wiki/Caudron_Type_G

    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 ...

  7. Le Rhône 9C - Wikipedia

    en.wikipedia.org/wiki/Le_Rhône_9C

    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 ...