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(Griffon 65)
Type: 12-cylinder supercharged
liquid-cooled 60° "Vee" piston
aircraft engine
Bore: 6 in
Stroke: 6.6 in
Displacement: 2,240 in³
Dry weight: 1,980 lb
Power output:
1,565 hp at 3,000 rpm @12,250 ft
1,390 hp at 3,000 rpm @23,500 ft
Source: Wikipedia.com
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Spitfire, Firefly, Spiteful, Seafare, Avro Shackleton
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Rolls-Royce Griffon |
The Griffon was designed prior to World War II and was originally intended as a low-altitude engine for naval aircraft such as the Fairey Firefly but a formal suggestion to fit a Griffon in a Spitfire was made by Joe Smith, who had taken over as Chief Designer at Supermarine's after Mitchell's death, in October 1939. However, work by Rolls-Royce on the engine had been halted temporarily to concentrate on the smaller 1,640 in³ (27L) Merlin which had already surpassed the output achieved with the early Griffon.
Valvetrain: Two intake and two exhaust valves per cylinder with sodium-cooled exhaust valve stems, actuated via an overhead camshaft.
Supercharger: Two-speed two-stage centrifugal type supercharger, boost pressure automatically linked to the throttle, water-air aftercooler installed between the second stage and the engine.
Fuel system: Triple-choke updraft carburetor with automatic mixture control
Oil system: Dry sump with one pressure pump and two scavenge pumps.
Cooling system: 70% water and 30% ethylene glycol coolant mixture, pressurized
Source: Wikipedia.com
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