Lycoming O-360
aeronewsline :: Accueil :: Histoire :: Moteurs
Page 1 sur 1
Lycoming O-360
Le Lycoming O-360 vu sur Wikipedia.en Merci
[Vous devez être inscrit et connecté pour voir ce lien]
------------------------------------------------------------------------------------------------------------------------------------------------------------------
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines.
Engines in the O-360 series produce between 145 and 225 horsepower (109 to 168 kW).
Design and development
There are 167 different models within the O-360 family of engines, with 12 different prefixes.
[Vous devez être inscrit et connecté pour voir ce lien]
------------------------------------------------------------------------------------------------------------------------------------------------------------------
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines.
Engines in the O-360 series produce between 145 and 225 horsepower (109 to 168 kW).
Design and development
There are 167 different models within the O-360 family of engines, with 12 different prefixes.
SUNSITE- CLUB
- Messages : 1253
Re: Lycoming O-360
O-360 carbureted horizontally opposed engine series
HO-360 vertically mounted engine series for helicopter installation
LO-360 identical to the same model O-360, but with the crankshaft rotating in the opposite direction for use on twin-engined aircraft to eliminate the problem of having one engine that is the critical engine.
HO-360 vertically mounted engine series for helicopter installation
LO-360 identical to the same model O-360, but with the crankshaft rotating in the opposite direction for use on twin-engined aircraft to eliminate the problem of having one engine that is the critical engine.
SUNSITE- CLUB
- Messages : 1253
Re: Lycoming O-360
TO-360 turbocharged engine series
LTO-360 turbocharged left-hand rotation engine series
LTO-360 turbocharged left-hand rotation engine series
SUNSITE- CLUB
- Messages : 1253
Re: Lycoming O-360
IO-360 fuel-injected horizontally opposed engine series
LIO-360 identical to the same model IO-360, but with the crankshaft rotating in the opposite direction
LIO-360 identical to the same model IO-360, but with the crankshaft rotating in the opposite direction
SUNSITE- CLUB
- Messages : 1253
Re: Lycoming O-360
AIO-360 inverted mount, fuel-injected engine series
AEIO-360 aerobatic, fuel-injected engine series
HIO-360 vertically mounted, fuel-injected engine series for helicopter installation
LHIO-360 left-hand rotation, fuel-injected, vertically-mounted helicopter engine.
AEIO-360 aerobatic, fuel-injected engine series
HIO-360 vertically mounted, fuel-injected engine series for helicopter installation
LHIO-360 left-hand rotation, fuel-injected, vertically-mounted helicopter engine.
SUNSITE- CLUB
- Messages : 1253
Re: Lycoming O-360
The O-360 series all have a displacement of 361 cubic inches (5.9 liters).
Bore and stroke are 5.125 and 4.375 inches (130 and 111 mm) respectively.
The O-360 has a factory rated TBO (Time Between Overhaul) of 2000 hours.
Engines that do not accumulate 2000 hours are recommended to be overhauled in the twelfth year.
They have been installed in thousands of aircraft including Cessna 172s, Piper Cherokees/Archers, Grumman Tigers and many home-built aircraft.
By increasing the cylinder bore of the O-360 by 3⁄16 inches, the engine was developed into the 210 hp (157 kW) Lycoming IO-390.[
The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2.
Bore and stroke are 5.125 and 4.375 inches (130 and 111 mm) respectively.
The O-360 has a factory rated TBO (Time Between Overhaul) of 2000 hours.
Engines that do not accumulate 2000 hours are recommended to be overhauled in the twelfth year.
They have been installed in thousands of aircraft including Cessna 172s, Piper Cherokees/Archers, Grumman Tigers and many home-built aircraft.
By increasing the cylinder bore of the O-360 by 3⁄16 inches, the engine was developed into the 210 hp (157 kW) Lycoming IO-390.[
The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2.
SUNSITE- CLUB
- Messages : 1253
Sujets similaires
» Lycoming T53
» Lycoming IO-580 & GSO-580
» Lycoming ( Honeywell ) T55
» Lycoming ALF 502 ( Honeywell )
» Lycoming IO-580 & GSO-580
» Lycoming ( Honeywell ) T55
» Lycoming ALF 502 ( Honeywell )
aeronewsline :: Accueil :: Histoire :: Moteurs
Page 1 sur 1
Permission de ce forum:
Vous ne pouvez pas répondre aux sujets dans ce forum
|
|