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词条 Renault 6Q
释义

  1. Design and development

  2. Operational history

  3. Variants

  4. Applications

  5. Engines on display

  6. Specifications (post-war unsupercharged)

  7. See also

  8. References

name= Renault 6Qimage= File:Nord 1101-moteur (MAA).jpgcaption=Renault 6Q 10 in a Nord Ramier I

}}{{Infobox Aircraft Engine

type=6-cylinder inverted air-cooled inlinemanufacturer=Renaultdesigner=national origin=Francefirst run=c.1932major applications=produced=number built=>3360program cost=unit cost=developed from=variants with their own articles=
}}

The Renault 6Q is an air-cooled six-cylinder, inverted piston engine, producing about {{convert|220|hp|kW|abbr=on|-1|order=flip}} continuous power. It was designed and built in France and produced for more than ten years after its homologation in 1936, with large numbers built during World War II.[1][2]

Design and development

The six-cylinder Renault 6Q and the four-cylinder Renault 4P, both from the early 1930s, shared the same bore, stroke and pistons.[3]

The 6Q was built in both unsupercharged and supercharged forms. The centrifugal supercharger was added at the back of the engine, driven off the crankshaft via step-up gearing. It added {{convert|13|kg|lb|abbr=on|0}} to the weight and {{convert|242|mm|in|abbr=on|1}} to the length but boosted the performance at altitude to a continuous power of {{convert|237|hp|kW|0|abbr=on|order=flip}} at 2,500 rpm and {{convert|2200|m|ft|-1|abbr=on}}. Two pre-war models were optimised to different altitudes, the 02/03 right- and left-handed pair to {{convert|2000|m|ft|-1|abbr=on}}, with 7.61:1 gearing and the 04/05 pair to {{convert|4000|m|ft|-1|abbr=on}}, with 12.274 gearing.

Operational history

The 6Q was homologated in 1936; 1700 were built before the war and 1660 during it.[2] Post-war, production was resumed.[3] The majority of pre-war 6Qs were used in Caudron C.440 Goélands, during the war in Goélands and post-war in Nord's Messerschmitt Bf 108 derived Nord Pingouin, in the Nord Noralpha and Ramier Bf 108 developments.

Variants

Even sub-type numbers rotate clockwise, odd numbers anti-clockwise as seen from engine.

Renault 6Q-00/01
Unsupercharged LH/RH rotation
Renault 6Q-02/03
{{convert|220|hp|kW|abbr=on}} Supercharged to {{convert|2000|m|abbr=on}} LH/RH rotation
Renault 6Q-04/05
{{convert|240|hp|kW|abbr=on}} Supercharged to {{convert|4000|m|abbr=on}} LH/RH rotation
Renault 6Q-06/07
{{convert|233|hp|kW|abbr=on}} LH/RH rotation
Renault 6Q-08/09
{{convert|240|hp|kW|abbr=on}} LH/RH rotation
Renault 6Q-10/11
{{convert|230|hp|kW|abbr=on}} LH/RH rotation
Renault 6Q-18/19
LH/RH rotation
Renault 6Q-20/21
{{convert|300|hp|kW|abbr=on}} LH/RH rotation

Applications

  • Caudron C.440 Goéland
  • Caudron C.631-5 Simoun
  • Caudron C.640 Typhon
  • Caudron C.690
  • Caudron C.860
  • Dewoitine HD.730
  • Farman F.430
  • Hanriot H.230
  • Morane-Saulnier MS.350
  • Morane-Saulnier MS.501
  • Nord 1101/2 Noralpha/Ramier
  • Nord Pingouin
  • Potez 661
  • Rey R.1
  • SNCASE SE-700
  • SNCASE SE-1210

Engines on display

  • Ailes Anciennes, Toulouse: Renault 6Q 10 in a Nord 1101 Ramier I.[8]

Specifications (post-war unsupercharged)

{{pistonspecs|
|ref=Jane's All the World's Aircraft 1948, p.55d[3]
|type=6-cylinder inverted air-cooled inline
|bore={{convert|120|mm|in|2|abbr=on}}
|stroke={{convert|140|mm|in|2|abbr=on}}
|displacement={{convert|9.5|l|cuin|0|abbr=on}}
|length={{convert|1600|mm|in|1|abbr=on}}
|width={{convert|510|mm|in|1|abbr=on}}
|height={{convert|920|mm|in|1|abbr=on}}
|weight={{convert|240|kg|lb|0|abbr=on}} dry
|valvetrain=One inlet and one exhaust valve per cylinder with Austenitic, driven via tappets, rocker arms and pushrods from a camshaft in the crankcase.
|fuelsystem=Twin Zenith carburetters and SEV ignition magnetos; two sparking plugs per cylinder.
|fueltype=
|oilsystem=Dry sump with pump to crankshaft, camshaft and big ends. Cylinders and pistons splash lubricated.
|coolingsystem=Air
|power=Take-off {{convert|233|hp|kW|0|abbr=on|order=flip}} at 2,500 rpm; normal {{convert|218|hp|kW|0|abbr=on|order=flip}} at 2,500 rpm and {{convert|500|m|ft|0|abbr=on}}
|specpower=
|compression=6:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=
|designer=
|reduction_gear=
|general_other=
|components_other= Cylinders: Steel barrels with machined fins aluminium heads with cast fins and hemispherical combustion chamber.
  • Pistons: Aluminium alloy forged with four piston rings and floating gudgeon pins. Duralumin connecting rods with white metal big-end bearings and bronze little-end bushes.
  • Crankshaft: Forged steel with six throws and seven bearings.
  • Crankcase: Aluminium, with magnesium cover and main bearing in crankcase extension.

|performance_other=
}}

See also

{{aircontent
|see also=
|related=
  • Renault 4P
  • Renault 6P

|similar aircraft=
|lists=
  • List of aircraft engines

|similar engines=
  • Alfa Romeo 115
  • Argus As 17
  • de Havilland Gipsy Queen
  • de Havilland Gipsy Six
  • Isotta Fraschini Beta
  • Menasco Buccaneer

}}

References

{{commons category}}
1. ^{{cite book |title= Jane's All the World's Aircraft 1948|last= Bridgman |first= Leonard |coauthors= |edition= |year=1948|publisher=Sampson, Low, Marston and Co. Ltd|location= London|isbn=|page=55d }}
2. ^{{cite book |title= World Encyclopaedia of Aero Engines|last=Gunston|first=Bill|edition=2| year=1989|volume= |publisher=Patrick Stephens Ltd |location=Wellingborough |isbn=1-85260-163-9|page=135}}
3. ^{{cite book |title=Aviation Museums and Collections of Mainland Europe |last= Ogden |first=Bob |coauthors= |edition= |year=2009|publisher= Air Britain (Historians) Ltd|page=125 |isbn=978 0 85130 418 2}}
4. ^{{cite web |url=http://www.hydroretro.net/etudegh/renault.pdf|title=Les Moteurs d'Aviation Renault |author=Gerard Hartmann |page=24 |work= |publisher= |accessdate=14 March 2014}}
[1][2][3][4]
}}{{Renault aeroengines}}

4 : Air-cooled aircraft piston engines|Inverted aircraft piston engines|Aircraft piston engines 1930–1939|Renault aircraft engines

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