Renault 12R
{{short description|1930s French piston aircraft engine}}
{{Infobox aircraft begin
|name = Renault 12R |image = File:Paris - Retromobile 2012 - Moteur Renault 12R - 1915 - 001.jpg |caption = 12R at Retromobile in 2012 }} {{Infobox aircraft engine |type = Air cooled in-line |national origin = France |manufacturer = Renault |designer = |first run = 1935 |major applications = Caudron C.714 |status = |produced = |number built = 325 |program cost = |unit cost = |developed from = |variants with their own articles = |developed into = }} |
The Renault 12R was an air-cooled inverted V12 aircraft engine developed by the French engineering company Renault in the 1930s. The design was based on mounting two 6Q six-cylinder engines on a single crankshaft. In production, the engine was rated between {{convert|450|and|500|hp|kW|abbr=on}}, although a high performance version built for the sole Caudron C.712 racing special produced {{convert|730|hp|kW|abbr=on}}. More than one third of production went to power the Caudron C.714 light fighter that fought in the early stages of World War II for the French and Polish Air Forces.
Design and development
The 12R was developed by Renault in the 1930s.{{sfn|Gunston|1998|page=135}} The design was derived from the successful Renault Bengali, using the same construction techniques and being of essentially steel construction.{{sfn|Grey|Bridgman|1938}}{{sfn|Wilkinson|1945|page=58}} It was based on the 4.46, a test engine developed by mounting two 6Q six-cylinder engines on the same crankshaft.{{sfn|Ailes Anciennes Le Bourget}} The engine retained the bore and stroke of the smaller engine.{{sfn|Wilkinson|1945|pages=245–247}} The cylinders and pistons were made of forged steel and connected in pairs to an eight bearing crankshaft. The crankcase was made of aluminium alloy coated with magnesium. A centrifugal supercharger was mounted to the rear.{{sfn|Angle|1941|page=120}} The engine was produced in both right handed and left handed versions, the difference being the direction of propeller rotation.{{sfn|Wilkinson|1945|page=247}}
Designed to be fitted to a range of aircraft, both civil and military, the engine was originally rated at {{convert|450|hp|kW|lk=on}} when first introduced in 1935. However, the majority manufactured, 290 out of a total production of 325, were the {{convert|500|hp|kW|abbr=on|adj=on}} 12Rc introduced in 1939.{{sfn|Hartman|2015|page=31}} Of these, 120 powered the Caudron C.714 light fighter which served in World War II.{{sfn|Hartman|2015|page=32}} In addition to examples of the aircraft ordered the French Air Force, thirty-five were delivered to the Polish Air Force in France and a further six to the Finnish Air Force, although the latter were not used in combat.{{sfn|Angelucci|Matricardi|Cosentino|Tatangelo|1978|page=258}} The most powerful version was the 12R Spécial of 1937 which produced {{convert|730|hp|kW|abbr=on}} at 3250 rpm and powered the single C.712 racing aircraft derived from the fighter.{{sfn|Ailes Anciennes Le Bourget}}
Variants
;Renault 12R:{{convert|450|hp|kW|abbr=on}}{{sfn|Hartman|2015|page=22}}
;Renault 12Rb:{{convert|470|-|480|hp|kW|abbr=on}}{{sfn|Hartman|2015|page=31}}
;Renault 12Rc:{{convert|500|hp|kW|abbr=on}}{{sfn|Hartman|2015|page=31}}
;Renault 12Rm:{{convert|480|hp|kW|abbr=on}}{{sfn|Hartman|2015|page=32}}
;Renault 12Ro:{{convert|450|hp|kW|abbr=on}}{{sfn|Hartman|2015|page=22}}
;Renault 12R-00:{{convert|500|hp|kW|abbr=on}} LH rotation{{sfn|Wilkinson|1945|page=247}}
;Renault 12R-01:{{convert|500|hp|kW|abbr=on}} RH rotation{{sfn|Wilkinson|1945|page=247}}
;Renault 12R-02:{{convert|500|hp|kW|abbr=on}}{{sfn|Hauet|2002|page=202}}
;Renault 12R-03:{{convert|500|hp|kW|abbr=on}}{{sfn|Ailes Anciennes Le Bourget}}
;Renault 12R-09:{{convert|500|hp|kW|abbr=on}}{{sfn|Hauet|2002|page=229}}
;Renault 12R Spécial:{{convert|730|hp|kW|abbr=on}}{{sfn|Hartman|2015|page=32}}
Applications
- Caudron C-446{{sfn|Hartman|2015|page=32}}
- Caudron C.560{{sfn|Hartman|2015|page=32}}
- Caudron C.581{{sfn|Hartman|2015|page=32}}
- Caudron C.710{{sfn|Hartman|2015|page=32}}
- Caudron C.712{{sfn|Hartman|2015|page=32}}
- Caudron C.714{{sfn|Green|Swanborough|1994|page=111}}
- Caudron C.870{{sfn|Hauet|2002|page=229}}
- Dewoitine D.720{{sfn|Green|1967|page=22}}
- Dewoitine D.750{{sfn|Green|1967|page=25}}
- Hanriot H.220 (prototype only){{sfn|Green|Swanborough|1994|page=280}}
- Romano R.110{{sfn|Green|Swanborough|1994|page=503}}
Specifications (12R-00)
{{pistonspecs|
|ref=Aircraft Engines of the World {{sfn|Wilkinson|1945|page=247}}
|type= 12-cylinder, air cooled V12 engine
|bore= {{convert|120|mm|in|abbr=on}}
|stroke= {{convert|140|mm|in|abbr=on}}
|displacement= {{convert|19|L|in3|0|abbr=on}}
|length= {{convert|2072|mm|in|abbr=on}}
|diameter=
|width= {{convert|680|mm|in|abbr=on}}
|height= {{convert|929|mm|in|abbr=on}}
|weight={{convert|439|kg|lb|abbr=on}}
|valvetrain= 2 x overhead valves per cylinder operated by pushrods
|supercharger= Single speed centrifugal compressor
|turbocharger=
|fuelsystem=
|oilsystem=
|coolingsystem= Air-cooled
|power=
- Take-off: {{convert|500|hp|kW|0|abbr=on}} at 2,500 rpm
- Cruise: {{convert|300|hp|kW|0|abbr=on}} at 2,500 rpm at {{convert|4000|m|ft|abbr=on}}
- Military: {{convert|450|hp|kW|0|abbr=on}} at 2,100 rpm at {{convert|4000|m|ft|abbr=on}}
|specpower=
|compression= 6.4:1
|fuelcon= 225 g/(hp•h) (0.50 lb/(hp•h))
|specfuelcon=
|oilcon= 10 g/(hp•h) (0.022 lb/(hp•h))
|power/weight=
|designer=
|reduction_gear=
|general_other=
|components_other=
|performance_other=
}}
See also
{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
|similar engines=
- Alfa Romeo 122
- Argus As 410
- de Havilland Gipsy Twelve
- Isotta Fraschini Gamma
- Junkers Jumo 210
- Ranger V-770
- Walter Sagitta
}}
References
{{Commons category}}
=Citations=
{{reflist}}
=Bibliography=
- {{cite web|author=Ailes Anciennes Le Bourget|url=http://aalebourget.fr/moteur-caudron-cr-714/|title=Le moteur du Caudron CR.714|language=fr|access-date=29 May 2019}}
- {{cite book|last1=Angelucci|first1=Enzo|last2=Matricardi|first2=Paolo|last3=Cosentino|first3=Vincenzo|last4=Tatangelo|first4=Claudio|title=World War II Airplanes|location=Chicago|publisher=Rand McNally|year=1978|isbn=978-0-52888-170-1}}
- {{cite book|last=Angle|first=Glen D.|title=Modern Aircraft Engines|location=New York City|publisher=Aircraft Publications|year=1941|url=https://babel.hathitrust.org/cgi/pt?id=mdp.39015006075827|oclc=658901703}}
- {{cite book|last=Green|first=William|title=War Planes of the Second World War: Volume 8 Bombers and Reconnaissance Aircraft|publisher=MacDonald|location=London|year=1967|oclc=1064406192}}
- {{cite book|last1=Green|first1=William|last2=Swanborough|first2=Gordon|title=The Complete Book of Fighters|year=1994 |publisher=Salamandar|location=London|isbn=978-0-86101-643-3}}
- {{cite book|last1=Grey|first1=C.G.|last2=Bridgman|first2=Leonard|title=Jane's All the World's Aircraft 1938|publisher=Sampson, Low & Martin Company Limited|location=London|year=1938}}
- {{cite book|last=Gunston|first=Bill|title=World Encyclopedia of Aero Engines|location=London|publisher=P. Stephens|year=1998|isbn=978-1-85260-597-1}}
- {{cite web|last=Hartman|first=Gerard|title=Les Moteurs d'Aviation Renault|website=hydroretro.net|url=http://www.hydroretro.net/etudegh/les_moteurs_d_aviation_renault.pdf|date=2015|access-date=29 May 2019|language=Fr}}
- {{cite book|last=Hauet|first=André|title=Les Avions Caudron|volume=2|location=Le Vigen|publisher=Lela Presse|year=2002|isbn=978-2-91401-709-1|language=Fr}}
- {{cite book|last=Wilkinson|first=Paul Howard|title=Aircraft Engines of the World|publisher=Paul H. Wilkinson|location=New York|year=1945|isbn=978-0-91171-024-3|url=https://archive.org/details/in.ernet.dli.2015.205335|access-date=29 May 2019}}
{{Renault aeroengines}}
Category:1930s aircraft piston engines