释义 |
- Variants O-300 O-315 (6A3)
- Applications Direct drive Geared drive Supercharged
- Specifications (6AC-298)
- See also
- References
name= O-300/6AC-298 | image = | caption = }}{{Infobox Aircraft Engine | type= Piston aircraft engine | national origin = United States | manufacturer= Franklin Engine Company | first run= 1941 | major applications= | number built = | program cost = | unit cost = | developed from = | developed into = | variants with their own articles = }} |
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 {{convert|300|cuin|L|abbr=on|0}}. The power output ranged between {{convert|130|hp|kW|abbr=on|0}} and {{convert|175|hp|kW|abbr=on|0}} 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. VariantsO-300- 6AC-298
- 6AC-298-F3 (O-300-1)
- {{convert|130|hp|kW|abbr=on|0}} at 2,600 rpm
- 6ACT-298
- {{convert|150|hp|kW|abbr=on|0}} at 3,000 rpm
- 6ACT-298-J4 (O-300-3)
- {{convert|150|hp|kW|abbr=on|0}} at 2,930 rpm
- 6ACT-298-35 (O-300-11)
- {{convert|150|hp|kW|abbr=on|0}} at 2,930 rpm
- 6ACG-298-P5 (O-300-9)
- Geared propeller drive 0.63:1, {{convert|160|hp|kW|abbr=on|0}} at 3,200 rpm
- 6ACTS-298
- Supercharged, {{convert|160|hp|kW|abbr=on|0}} at 3,200 rpm
- 6ACTS-298-K4 (O-300-7)
- Supercharged, {{convert|175|hp|kW|abbr=on|0}} at 3,000 rpm
- 6ACV-298
- Vertical installation for helicopters,{{convert|160|hp|kW|abbr=on|0}} at 3,250 rpm
O-315 (6A3)- 6AL-315
- {{convert|175|hp|kW|abbr=on|0}}
- 6ALG-315
- {{convert|175|hp|kW|abbr=on|0}}
ApplicationsDirect drive- Aeronautical Products A-1
- Aeronautical Products A-3
- CNNA HL-6
- Culver XPQ-9
- Culver XPQ-14, YPQ-14A, XPQ-15
- Bell 30
- Bellanca T-14
- Erco XPQ-13
- Fleetwings 33
- Hockaday Comet
- Piper P-1
- Troy A
- Zodiac Libra-Det
Geared drive- Culver PQ-14 Cadet
- Republic RC-1 Thunderbolt (O-315)
Supercharged- Northwestern XPG-1 (Waco CG-4 twin-engine conversion)
Specifications (6AC-298){{pistonspecs | |ref={{fact|date=December 2017}} |type=6-cylinder air-cooled horizontally opposed aircraft piston engine |bore=4.25 in (108 mm) |stroke=3.5 in (88.9 mm) |displacement=297.9 in³ (4.88 L) |length= |diameter= |width= |height= |weight=260 lb (118 kg) |valvetrain= |supercharger= |turbocharger= |fuelsystem= |fueltype= |oilsystem= |coolingsystem=Air-cooled |power=130 hp (97 kW) at 2,600 rpm |specpower= |compression= |fuelcon= |specfuelcon= |oilcon= |power/weight= }}See also{{aircontent |see also= |related= |similar engines= |similar aircraft= |lists= }}References{{Commons category|Franklin aircraft engines}}- Notes
- Bibliography
{{refbegin}}- Gunston, Bill. (1986) World Encyclopedia of Aero Engines. Patrick Stephens: Wellingborough. p. 57
{{refend}}{{Franklin aeroengines}}{{US military piston aeroengines}} 3 : Franklin aircraft engines|Aircraft piston engines 1940–1949|Boxer engines |