Franklin O-300 Explained
The Franklin O-300 (company designation 6AC-298) was an American air-cooled aircraft engine of the early 1940s. The engine was of six-cylinder, horizontally-opposed layout and displaced 300abbr=onNaNabbr=on. The power output ranged between 130abbr=onNaNabbr=on and 175abbr=onNaNabbr=on depending on variant. The 6ACG-298 featured a geared propeller drive.
An enlarged displacement version was known as the O-315, 6A3 or 6AL-315.
Variants
O-300
- 6AC-298:
6AC-298-F3 (O-300-1):130abbr=onNaNabbr=on at 2,600 rpm
- 6ACT-298:150abbr=onNaNabbr=on at 3,000 rpm
6ACT-298-J4 (O-300-3):150abbr=onNaNabbr=on at 2,930 rpm
6ACT-298-35 (O-300-11):150abbr=onNaNabbr=on at 2,930 rpm
- 6ACG-298-P5 (O-300-9):Geared propeller drive 0.63:1, 160abbr=onNaNabbr=on at 3,200 rpm
- 6ACTS-298:Supercharged, 160abbr=onNaNabbr=on at 3,200 rpm
6ACTS-298-K4 (O-300-7):Supercharged, 175abbr=onNaNabbr=on at 3,000 rpm
- 6ACV-298:Vertical installation for helicopters,160abbr=onNaNabbr=on at 3,250 rpm
O-315 (6A3)
- 6AL-315:175abbr=onNaNabbr=on
- 6ALG-315:175abbr=onNaNabbr=on
Applications
Direct drive
Geared drive
Supercharged
References
- Notes
Bibliography
- Gunston, Bill. (1986) World Encyclopedia of Aero Engines. Patrick Stephens: Wellingborough. p. 57