| 词条 | Armstrong Siddeley Panther | ||||||||||||||
| 释义 |
The Armstrong Siddeley Panther was a 27-litre 14-cylinder twin-row air-cooled radial aero engine developed by Armstrong Siddeley. It was originally named the Jaguar Major.[1] Applications
Specifications (Panther VII){{pistonspecs| |ref=[2] |type=14-cylinder twin-row air-cooled radial engine |bore=5.25 in (133.4 mm) |stroke=5.5 in (139.7 mm) |displacement=1,667 cu in (27.3 L) |length=64 in (1.63 m) |diameter=46.45 in (1.18 m) |width= |height= |weight=1,047 lb (475 kg) |valvetrain=Overhead valve |supercharger=Centrifugal |turbocharger= |fuelsystem=Carburettor |fueltype= |oilsystem= |coolingsystem=Air-cooled |power=638 hp (478 kW) at 2,400 rpm with 0.5 psi (3.5 kPa) boost |specpower= |compression=5.1:1 |fuelcon= |specfuelcon= |oilcon= |power/weight= 0.61 hp/lb (1.01 kW/kg) }} See also{{aircontent|see also= |related=
|similar aircraft= |lists=
|similar engines= }} ReferencesNotes1. ^Lumsden 2003, p.72. 2. ^Lumsden 2003, p.73. Bibliography{{refbegin}}
3 : Radial engines|Armstrong Siddeley aircraft engines|Aircraft piston engines 1920–1929 |
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