Franklin O-150
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Template:Short description Template:Use dmy dates Template:Use American English
Template:Infobox Aircraft EngineThe Franklin O-150 (company designation 4AC-150) was an American air-cooled aircraft engine of the late 1930s. The engine was of four-cylinder, horizontally-opposed layout and displaced Script error: No such module "convert".. The power output was nominally Script error: No such module "convert"..
Applications
- Aeronca 50 Chief
- Bartlett Zephyr
- Clutton-Tabenor FRED
- Fetterman Chickadee
- Payne MC-7 pusher
- Piper J-3 Cub
- Rose Parakeet
- Taylorcraft BF-65
- Taylorcraft L-2
Engines on display
- Aerospace Museum of California - Franklin 0-150 (4AC-150)
Specifications (4AC-150)
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Data from Jane's all the World's Aircraft 1938.[1]
General characteristics
- Type: 4-cylinder air-cooled horizontally opposed aircraft piston engine
- Bore: Script error: No such module "convert".
- Stroke: Script error: No such module "convert".
- Displacement: Script error: No such module "convert".
- Length: Script error: No such module "convert".
- Width: Script error: No such module "convert".
- Height: Script error: No such module "convert".
- Dry weight: Script error: No such module "convert".
Components
- Valvetrain: Pushrod and rocker operated overhead valves. One intake, one exhaust
- Fuel system: Stromberg NA-S2 updraught carburetor
- Fuel type: 70 Octane gasoline
- Oil system: Wet sump full pressure system
- Cooling system: Air-cooled
Performance
- Power output: Script error: No such module "convert". at 1,875 rpm
- Compression ratio: 6.66:1
- Fuel consumption: Script error: No such module "convert".
- Specific fuel consumption: 0.54 lb/hp/h
See also
Comparable engines
Related lists
References
- Notes
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- ↑ Script error: No such module "citation/CS1".
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- Bibliography
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- Gunston, Bill. (1986) World Encyclopedia of Aero Engines. Patrick Stephens: Wellingborough. p. 57
Template:Franklin aeroengines Template:US military piston aeroengines