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词条 Renault 6P
释义

  1. Design and development

  2. Variants

  3. Applications

  4. Specifications (Renault 6Pdi)

  5. See also

  6. References

  7. Further reading

name = 6Pimage =caption =

}}{{Infobox Aircraft Engine

type=Air-cooled 6-cyl inverted in-line piston enginemanufacturer=Renaultnational origin=Francefirst run=major applications=number built =program cost =unit cost =developed from =developed into =variants with their own articles =
}}

The Renault 6P, also called the Renault Bengali, was a series of air-cooled 6-cylinder inverted in-line aero engines designed and built in France from the late 1920s, which produced from {{convert|abbr=on|180|hp|kW|disp=flip}} to {{convert|abbr=on|270|hp|kW|disp=flip}}.

Design and development

Charles Lindbergh's Atlantic Ocean crossing in 1927 inspired Renault to enter the light aero-engine market to diversify the range of engines they offered. To complement the 4P four-cylinder engines, Renault developed the 6P series, with {{convert|abbr=on|115|mm|in}} bore and {{convert|abbr=on|140|mm|in}} stroke; by adding two cylinders of the same bore and stroke.

Developed by Charles-Edmond Serre, the {{convert|9.5|l|cuin|abbr=on|2}} 6P evolved to give {{convert|abbr=on|180|to|270|hp|kW}}, using {{convert|abbr=on|120|mm|in}} bore steel cylinder liners, aluminium alloy cylinder heads attached by long studs to the crankcase, Duralumin connecting rods and magnesium alloy crankcase.

The 6P was also produced in the USSR, as the MV-6, (Motor Vozdushniy / Motor Voronezhskiy - air-cooled engine / Voronezh built engine {correct interpretation is unclear}).

Variants

Renault 6Pdi
inverted 6 in-line
Renault 6Pdis
with supercharger
Renault 6Pfi
{{convert|170|hp|kW|abbr=on|disp=flip}}
Voronezh MV-6
licence production in the USSR

Applications

  • Caudron C.630 Simoun
  • Caudron C.684
  • Morane-Saulnier MS.350 (Pei)

Specifications (Renault 6Pdi)

{{pistonspecs|
|ref=Renault 1907-1934:27 Ans d'Aviation[1]
|type=6-cylinder naturally aspirated air-cooled inverted in-line piston aircraft engine
|bore={{convert|120|mm|in|abbr=on}}
|stroke={{convert|140|mm|in|abbr=on}}
|displacement={{convert|9.5|L|in3|abbr=on|2}}
|length=
|diameter=
|width=
|height=
|weight={{convert|205|kg|lb|abbr=on}}
|valvetrain=Pushrod-actuated, single intake and single exhaust valve per cylinder
|supercharger=
|turbocharger=
|fuelsystem=
|fueltype= 80 Octane gasoline
|oilsystem=Pressure fed, {{convert|3.0|kg/cm2|lb/in2|abbr=on}}, dry sump
|coolingsystem=Air
|power={{convert|180|hp|kW|abbr=on}} at 2,000 rpm @ sea-level normal
|specpower=
|compression=5.75:1
|fuelcon=
|specfuelcon=0.335 kg/kW.hr (0.551 lb/hp.hr)
|oilcon=
|power/weight=0.654 kW/kg (0.398 hp/lb)
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
  • List of aircraft engines

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

}}

References

1. ^{{cite book|title=Renault 1907-1934:27 Ans d'Aviation|date=1934|publisher=Usines Renault|location=Billancourt|pages=31–41|url=http://dev.museesafran.com/wp-content/uploads/2012/10/1350047209-livres-espace-patrimoine-saf2012_0048840.pdf|accessdate=12 October 2014|language=French|deadurl=yes|archiveurl=https://web.archive.org/web/20141017012427/http://dev.museesafran.com/wp-content/uploads/2012/10/1350047209-livres-espace-patrimoine-saf2012_0048840.pdf|archivedate=17 October 2014|df=}}

Further reading

  • {{cite web |last=HARTMANN |first=Gérard |title=LES MOTEURS D’AVIATION RENAULT |url=http://hydroretro.netudegh/renault.pdf |work=hydroretro.net |accessdate=9 July 2013 }}{{dead link|date=March 2018 |bot=InternetArchiveBot |fix-attempted=yes }}
{{Renault aeroengines}}

2 : Aircraft piston engines 1920–1929|Renault aircraft engines

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