词条 | Walter Bora | ||||||||||||||
释义 |
The Walter Bora was a Czechoslovakian nine-cylinder, air-cooled radial engine for powering light aircraft that was developed in the 1930s by Walter Aircraft Engines.[1] Variants
Direct drive engine
Geared engine, reduction ratio 0.666:1 Applications
Engines on displayA preserved example of the Walter Bora engine is on display at the following museum:
Specifications (Bora II-R){{pistonspecs| |ref=Flight[2] |type=9-cylinder radial piston engine |bore=105 mm (4.1 in) |stroke=120 mm (4.7 in) |displacement= |length= |diameter= |width= |height= |weight= 172 kg (379 lb) |valvetrain=One intake and one exhaust valve per cylinder |supercharger= |turbocharger= |fuelsystem=Carburettor |fueltype=Petrol |oilsystem= |coolingsystem=Air-cooled |power= 183 kW (245 hp) at 2,400 rpm |specpower= |compression=6.3:1 |fuelcon= |specfuelcon= |oilcon= |power/weight= 1 kW/kg (0.65 hp/lb) }} See also{{aircontent|see also= |related= |similar aircraft= |lists=
|similar engines=
}} References{{Commons category}}Notes1. ^Gunston 1989, p. 174. 2. ^Flight - Walter engines - November 1936 Retrieved: 19 October 2010 Bibliography{{refbegin}}
3 : Aircraft piston engines 1930–1939|Walter aircraft engines|Radial engines |
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