| 词条 | Agusta GA.40 | |||||||||||||||
| 释义 |
The Agusta GA.40 was a 2-cylinder, air-cooled, horizontally opposed engine developed in Italy by Agusta for light aircraft use. It was intended for use in motorgliders. The engine was produced in the 1950s and 1960s.[2] Specifications{{pistonspecs|ref=Jane's All the World's Aircraft 1962-63[3] |type=2-cylinder air-cooled horizontally opposed aircraft piston engine |bore={{convert|100|mm|in|abbr=on|2}} |stroke={{convert|95|mm|in|abbr=on|2}} |displacement={{convert|1.492|l|cuin|abbr=on|2}} |length={{convert|613|mm|in|abbr=on|2}} |diameter= |width={{convert|785|mm|in|abbr=on|2}} |height={{convert|450|mm|in|abbr=on|2}} |weight={{convert|56|kg|lb|abbr=on|0}} dry |valvetrain=pushrod operated overhead valve, 1x inlet + 1x exhaust per cylinder |supercharger= |turbocharger= |fuelsystem=Stromberg NAS 3A1 carburettor |fueltype=80/87 octane |oilsystem=Pressure lubrication with a gear driven pump |coolingsystem=Air-cooled |power={{convert|42|hp|kW|abbr=on|2|disp=flip}} at 2,700rpm |specpower=20.99 kW/l (0.46 hp/cuin) |compression= |fuelcon= |specfuelcon= |oilcon= |power/weight=0.559 kW/kg (0.34 hp/lb) |designer=M. Ginnini |reduction_gear= |general_other= |components_other= |performance_other= }} Applications
Notes1. ^{{cite journal|title=none|magazine=Sport Aviation|date=July 1958}} 2. ^{{cite journal|title=none|magazine=Flight|date=July 1957}} 3. ^{{cite book|last=Taylor|first=John W.R. FRHistS. ARAeS|title=Jane's All the World's Aircraft 1962-63|year=1962|publisher=Sampson, Low, Marston & Co Ltd|location=London}} References{{commons category|Agusta}}{{refbegin}}
3 : Aircraft piston engines 1950–1959|Boxer engines|Agusta aircraft engines |
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