avia.wikisort.org - EngineThe Kinner K-5 was a popular engine for light general and sport aircraft developed by Winfield B. 'Bert' Kinner.[1] With the boom in civilian aviation after Charles Lindbergh's transatlantic flight the K-5 sold well. The K-5 was a rough running[citation needed] but reliable engine and the K-5 and its derivatives were produced in the thousands, powering many World War II trainer aircraft. The K-5 was followed by the B-5, R-5 and R-55. Military engines were designated R-370
K-5 |
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Kinner K-5 in a Fleet Model 2 |
Type |
Radial engine |
National origin |
United States of America |
Manufacturer |
Kinner Airplane & Motor Corporation |
Developed into |
Kinner B-5 |
Applications
Specifications (Kinner K-5)
Data from Jane's all the World's Aircraft 1928[2]
General characteristics
- Type: Five-cylinder, air-cooled, radial
- Bore: 4.25 in (108 mm)
- Displacement: 372.4 cu in (6.103 l)
- Length: 19 in (480 mm)
- Diameter: 43.5 in (1,100 mm)
- Dry weight: 231 lb (105 kg)
Components
- Valvetrain: 1 inlet and 1 exhaust valve per cylinder
- Fuel system: 1 Stromberg carburetor or 1 double Zenith carburetor
- Fuel type: 73 Octane
- Oil system: pressure fed through hollow crankshaft
- Cooling system: Air
- Power output:
- 100 hp (75 kW) at 1,810 rpm maximum
- 70 hp (52 kW) at 1,650 rpm cruise
- Compression ratio: 5.0:1
- Fuel consumption: 7 gal/h (5.8 imp gal/h; 26 l/h)
- Oil consumption: 0.3125 gal/h (0.2602 imp gal/h; 1.183 l/h)
- Power-to-weight ratio: 0.36 hp/lb (0.59 kW/kg) at cruise
References
Further reading
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 99–100.
External links
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Radial engines | |
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Horizontally opposed engines | |
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H (four-bank H-configuration inline) | |
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IV (inverted-V inline) | |
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L (single-bank inline) | |
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O (opposed) | |
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R (radial) | |
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V (upright-V inline) | |
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V (inverted-V inline) | |
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VG (inverted-V inline) | |
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W (three-bank W-configuration inline) | |
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- See also: X-1800
- US military gas turbine aeroengines
- Piston engine configurations
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На других языках
[de] Kinner K-5
Der Kinner K-5 ist ein Fünfzylinder-Sternmotor, der bei dem Flugzeug- und Motorenhersteller Kinner Airplane & Motor Corporation in Glendale, Kalifornien ab 1919 entwickelt und gebaut wurde. Der Konstrukteur war Winfield Bert Kinner (1882–1957).[1]
- [en] Kinner K-5
[fr] Kinner K-5
Le Kinner K-5 était un moteur cinq cylindres en étoile américain pour avions légers et avions de sport, développé par Winfield B. 'Bert' Kinner.[1]. Le K-5 s'est bien vendu en raison de l'essor de l'aviation civile après le vol transatlantique de Charles Lindbergh. C'était un moteur rugueux mais fiable[réf. nécessaire] qui a été produit avec ses dérivés à des milliers d'exemplaires, propulsant un grand nombre d'avions d'entrainement de la seconde Guerre mondiale. Le K-5 fut suivi par le B-5, R 5 et R-55. Les versions militaires furent désignées R-370.
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