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Renault 6Q

The Renault 6Q, also called the Renault Bengali 6, is an air-cooled inverted in-line six-cylinder, aircraft piston engine, producing about 160 kW (220 hp) 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]

Renault 6Q
Renault 6Q on display at the Polish Aviation Museum
Type 6-cylinder inverted air-cooled inline
National origin France
Manufacturer Renault
First run c.1932
Number built >3360

Design and development edit

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 13 kg (29 lb) to the weight and 242 mm (9.5 in) to the length but boosted the performance at altitude to a continuous power of 177 kW (237 hp) at 2,500 rpm and 2,200 m (7,220 ft). Two pre-war models were optimised to different altitudes, the 02/03 right- and left-handed pair to 2,000 m (6,560 ft), with 7.61:1 gearing and the 04/05 pair to 4,000 m (13,120 ft), with 12.274 gearing.[4]

Operational history edit

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 edit

 
Renault 6Q-10A mounted on a Nord 1002 Pingouin

Even sub-type numbers rotate clockwise, odd numbers anti-clockwise as seen from engine.[4]

Renault 6Q-00/01
Unsupercharged LH/RH rotation
Renault 6Q-02/03
220 hp (160 kW) Supercharged to 2,000 m (6,600 ft) LH/RH rotation
Renault 6Q-04/05
240 hp (180 kW) Supercharged to 4,000 m (13,000 ft) LH/RH rotation
Renault 6Q-06/07
233 hp (174 kW) LH/RH rotation
Renault 6Q-08/09
240 hp (180 kW) LH/RH rotation
Renault 6Q-10/11
230 hp (170 kW) LH/RH rotation
Renault 6Q-18/19
LH/RH rotation
Renault 6Q-20/21
300 hp (220 kW) LH/RH rotation

Applications edit

Engines on display edit

  • Ailes Anciennes, Toulouse: Renault 6Q 10 in a Nord 1101 Ramier I.[5]

Specifications (post-war unsupercharged) edit

Data from Jane's All the World's Aircraft 1948, p.55d[3]

General characteristics

  • Type: 6-cylinder inverted air-cooled inline
  • Bore: 120 mm (4.72 in)
  • Stroke: 140 mm (5.51 in)
  • Displacement: 9.5 L (580 cu in)
  • Length: 1,600 mm (63.0 in)
  • Width: 510 mm (20.1 in)
  • Height: 920 mm (36.2 in)
  • Dry weight: 240 kg (529 lb) dry

Components

Performance

  • Power output: Take-off 174 kW (233 hp) at 2,500 rpm; normal 163 kW (218 hp) at 2,500 rpm and 500 m (1,640 ft)
  • Compression ratio: 6:1

See also edit

Related development

Comparable engines

Related lists

References edit

  1. ^ Gunston, Bill (1998). World Encyclopaedia of Aero Engines (4 ed.). Wellingborough: Patrick Stephens Ltd. p. 149. ISBN 1-85260-163-9.
  2. ^ a b Gerard Hartmann. "Les Moteurs d'Aviation Renault" (PDF). p. 24. Retrieved 14 March 2014.
  3. ^ a b c Bridgman, Leonard (1948). Jane's All the World's Aircraft 1948. London: Sampson, Low, Marston and Co. Ltd. p. 55d.
  4. ^ a b Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. p. 53d. ISBN 0715-35734-4.
  5. ^ Ogden, Bob (2009). Aviation Museums and Collections of Mainland Europe. Air Britain (Historians) Ltd. p. 125. ISBN 978-0-85130-418-2.

renault, also, called, renault, bengali, cooled, inverted, line, cylinder, aircraft, piston, engine, producing, about, continuous, power, designed, built, france, produced, more, than, years, after, homologation, 1936, with, large, numbers, built, during, worl. The Renault 6Q also called the Renault Bengali 6 is an air cooled inverted in line six cylinder aircraft piston engine producing about 160 kW 220 hp 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 Renault 6QRenault 6Q on display at the Polish Aviation MuseumType 6 cylinder inverted air cooled inlineNational origin FranceManufacturer RenaultFirst run c 1932Number built gt 3360 Contents 1 Design and development 2 Operational history 3 Variants 4 Applications 5 Engines on display 6 Specifications post war unsupercharged 6 1 General characteristics 6 2 Components 6 3 Performance 7 See also 8 ReferencesDesign and development editThe 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 13 kg 29 lb to the weight and 242 mm 9 5 in to the length but boosted the performance at altitude to a continuous power of 177 kW 237 hp at 2 500 rpm and 2 200 m 7 220 ft Two pre war models were optimised to different altitudes the 02 03 right and left handed pair to 2 000 m 6 560 ft with 7 61 1 gearing and the 04 05 pair to 4 000 m 13 120 ft with 12 274 gearing 4 Operational history editThe 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 Goelands during the war in Goelands and post war in Nord s Messerschmitt Bf 108 derived Nord Pingouin in the Nord Noralpha and Ramier Bf 108 developments Variants edit nbsp Renault 6Q 10A mounted on a Nord 1002 PingouinEven sub type numbers rotate clockwise odd numbers anti clockwise as seen from engine 4 Renault 6Q 00 01 Unsupercharged LH RH rotation Renault 6Q 02 03 220 hp 160 kW Supercharged to 2 000 m 6 600 ft LH RH rotation Renault 6Q 04 05 240 hp 180 kW Supercharged to 4 000 m 13 000 ft LH RH rotation Renault 6Q 06 07 233 hp 174 kW LH RH rotation Renault 6Q 08 09 240 hp 180 kW LH RH rotation Renault 6Q 10 11 230 hp 170 kW LH RH rotation Renault 6Q 18 19 LH RH rotation Renault 6Q 20 21 300 hp 220 kW LH RH rotationApplications editCaudron C 440 Goeland 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 1210Engines on display editAiles Anciennes Toulouse Renault 6Q 10 in a Nord 1101 Ramier I 5 Specifications post war unsupercharged editData from Jane s All the World s Aircraft 1948 p 55d 3 General characteristics Type 6 cylinder inverted air cooled inline Bore 120 mm 4 72 in Stroke 140 mm 5 51 in Displacement 9 5 L 580 cu in Length 1 600 mm 63 0 in Width 510 mm 20 1 in Height 920 mm 36 2 in Dry weight 240 kg 529 lb dryComponents Valvetrain One inlet and one exhaust valve per cylinder with Austenitic driven via tappets rocker arms and pushrods from a camshaft in the crankcase Fuel system Twin Zenith carburetters and SEV ignition magnetos two sparking plugs per cylinder Oil system Dry sump with pump to crankshaft camshaft and big ends Cylinders and pistons splash lubricated Cooling system Air 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 Power output Take off 174 kW 233 hp at 2 500 rpm normal 163 kW 218 hp at 2 500 rpm and 500 m 1 640 ft Compression ratio 6 1See also editRelated development Renault 4P Renault 6P Renault 12RComparable engines Alfa Romeo 115 Argus As 17 de Havilland Gipsy Queen de Havilland Gipsy Six Isotta Fraschini Beta Menasco BuccaneerRelated lists List of aircraft enginesReferences edit nbsp Wikimedia Commons has media related to Renault 6Q Gunston Bill 1998 World Encyclopaedia of Aero Engines 4 ed Wellingborough Patrick Stephens Ltd p 149 ISBN 1 85260 163 9 a b Gerard Hartmann Les Moteurs d Aviation Renault PDF p 24 Retrieved 14 March 2014 a b c Bridgman Leonard 1948 Jane s All the World s Aircraft 1948 London Sampson Low Marston and Co Ltd p 55d a b Grey C G 1972 Jane s All the World s Aircraft 1938 London David amp Charles p 53d ISBN 0715 35734 4 Ogden Bob 2009 Aviation Museums and Collections of Mainland Europe Air Britain Historians Ltd p 125 ISBN 978 0 85130 418 2 Retrieved from https en wikipedia org w index php title Renault 6Q amp oldid 1209712325, wikipedia, wiki, book, books, library,

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