| 词条 | Rotax 275 | ||||||||||||||
| 释义 |
The Rotax 275 is a {{convert|24|hp|kW|0|abbr=on}}, single-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in Self-launched Gliders.[1] DesignThe Rotax 275 is a single-cylinder two-stroke engine with an air-cooled cylinder head and cylinder. It has a single magneto ignition with a gear driven propeller. It was certified in Austria in November 1988.[1] Applications
Specifications (275){{pistonspecs||ref=EASA Type Certificate[1] |type=two-stroke air-cooled aeroengine |bore=72 mm (2.83 in) |stroke=66 mm (2.60 in) |displacement=268.7 cc (16.40 cu in) |length= |diameter= |width= |height= |weight=25 kg (complete with muffler and starter) |valvetrain= |supercharger= |turbocharger= |fuelsystem= |fueltype=two-stroke mixture |oilsystem= |coolingsystem=free air |power=17.6 kW (26 hp) at 7000 l/min |specpower= |compression= |fuelcon= |specfuelcon= |oilcon= |power/weight= |designer= |reduction_gear= |general_other= |components_other= |performance_other= }}{{aircontent |see also= |related= |similar aircraft= |lists= }} References1. ^1 2 [https://www.easa.europa.eu/system/files/dfu/TCDS%20E.210_issue%2003%2020160509_1.0.pdf EASA Type-Certificate Data Sheet No E.210 for Rotax 275 series engines (Issue 03 Dated 5 September 2016)] {{Rotax aeroengines}} 3 : Air-cooled aircraft piston engines|Rotax engines|Two-stroke aircraft piston engines |
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