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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. Rotary engine - Wikipedia

    en.wikipedia.org/wiki/Rotary_engine

    In 1913 the Seguin brothers introduced the new Monosoupape ("single valve") series, which replaced inlet valves in the pistons by using a single valve in each cylinder head, which doubled as inlet and exhaust valve. The engine speed was controlled by varying the opening time and extent of the exhaust valves using levers acting on the valve ...

  4. Le Rhône - Wikipedia

    en.wikipedia.org/wiki/Le_Rhône

    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 ...

  5. Gnome et Rhône - Wikipedia

    en.wikipedia.org/wiki/Gnome_et_Rhône

    The Gnome used a unique valve system with only one rod-operated exhaust valve, and a "hidden" intake valve located on the piston head. 160 hp Gnome 9N Monosoupape of 1917. On 6 June 1905 Louis Seguin and his brother Laurent formed the Société Des Moteurs Gnome [4] (the Gnome Motor Company) to produce automobile engines. They soon started ...

  6. 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 .

  7. 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 ...

  8. Category:Gnome-Rhône aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Gnome-Rhône...

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  9. Monosoupape engine - Wikipedia

    en.wikipedia.org/?title=Monosoupape_engine&...

    This page was last edited on 21 December 2012, at 00:13 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.