SNECMA 14R
http://dbpedia.org/resource/SNECMA_14R an entity of type: AircraftEngine102687423
The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War.
rdf:langString
rdf:langString
SNECMA 14R
xsd:integer
33237355
xsd:integer
1111487863
xsd:double
0.292
xsd:double
31.85
rdf:langString
Gear-driven 2-speed supercharger at 6.5:1 and 9.0:1 ratios
rdf:langString
Single inlet and exhaust valves operated by rockers and pushrods
rdf:langString
*Take-off: at 2,600 rpm at Hg boost with 100 octane fuel
**Military, low: at 2,600 rpm at
**Military, high: at 2,600 rpm at
**Normal, low: at 2,400 rpm at
**Normal, high: at 2,400 rpm at
xsd:integer
14
rdf:langString
The SNECMA 14R was a 14-cylinder two-row air-cooled radial engine developed in France just prior to the start of World War II from the Gnome-Rhône 14N. The 14N radial engine was itself an improved version of the popular pre-war Gnome-Rhône 14K Mistral Major series; designed and manufactured by Gnome et Rhône, a major French aircraft engine manufacturer whose origins pre-date the First World War. The improved 14R was initially known as the Gnome-Rhône 14P and then the Gnome-Rhône 14R. There were several improvements such as the introduction of a longer crankshaft and crankcase with a centre bearing, an increase in cylinder capacity, and a two-speed compressor. These changes allowed the engine to deliver 1,400hp at take-off and 1,300hp at 1,500m (1st gear) and 1200hp at 4000m (2nd gear). This came at the cost of a much increased total weight. It was expected that further development, such as the introduction of higher grade fuels, would lead to a power output of 1,660hp at low altitude. With the Fall of France, engine development was stopped under the occupation. After the war, development recommenced; however production of this engine after 1945 was transferred to the newly formed SNECMA and the engine was renamed the SNECMA 14R.
rdf:langString
Starter: Air equipment electric inertia starter
* Ignition: 2 x R.B. magnetos, 2 x short reach spark plugs per cylinder fed by a shielded ignition harness.
xsd:double
6.8
rdf:langString
Air-cooled with baffles
xsd:integer
1
xsd:integer
92
rdf:langString
Frontal Area:
rdf:langString
* List of aircraft engines
xsd:double
0.0067
rdf:langString
Pressure fed at
xsd:integer
14
xsd:double
1.494
rdf:langString
Planetary / epicyclic bevel reduction gearing at 0.67:1 ratio
xsd:nonNegativeInteger
6466