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词条 Continental IO-360
释义

  1. History

  2. Variants

     IO-360  TSIO-360  LTSIO-360 

  3. Applications

  4. Specifications (IO-360-A)

  5. See also

  6. References

     Notes  Bibliography 

  7. External links

{{for|a similarly named and broadly similar engine by another manufacturer|Lycoming O-360}}
name=IO-360image=Continental IO360D.JPGcaption=Continental IO-360-D

}}{{Infobox Aircraft Engine

type=Piston aero-enginenational origin=United Statesmanufacturer=Teledyne Continental Motorsfirst run=1962major applications=Cirrus SR20
Cessna 172
Ilyushin Il-103
Cessna Skymaster
Piper PA-34 Seneca
Cessna O-2 Skymaster
Cessna T-41 Mescalero
}}

The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010.[1][2]

The engine is available in both normally aspirated, fuel injected IO-360 model and a turbocharged TSIO-360 versions. It is also available in both left and right hand rotation versions for use on twin-engined aircraft.[3]

There was no carbureted version of this engine, which would have been designation O-360, therefore the base model is the IO-360.[4][5]

History

The IO-360 was first certified by the Federal Aviation Administration on 15 May 1962 to the CAR 13 certification standard, effective June 15, 1956, as amended by 13-1 thru 13-3. The engine is produced by Continental under Production Certificate No. 508.[4]

The turbocharged TSIO-360 series was first certified on 11 October 1966 to the Federal Aviation Regulations Part 33 standard effective February 1, 1965, as amended by 33-1. This series is manufactured under Production Certificate No. 7, except the TSIO-360-D which is under Production Certificate No. 508.[5]

Variants

IO-360

IO-360-A

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Base IO-360 model: a six-cylinder air-cooled, horizontally opposed direct drive, fuel injected engine. Uses a TCM 639230A3 fuel injector. The crankshaft has two 6th order dampers.[4]

IO-360-AB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639230A3 fuel injector. Same as the IO-360-A except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-AF

{{convert|180|hp|kW|0|abbr=on}}, designed to run on lower octane fuels such as the proposed 94UL avgas. The designation of "AF" stands for alternative fuel. The version incorporates lower-compression pistons, giving a 7.5 to 1 compression ratio and a revised fuel injection system.[6]

IO-360-B

{{convert|180|hp|kW|0|abbr=on}} at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 6.0:1. Uses a TCM 639230A3 or 6006 fuel injector. Same as IO-360-A except for reduced compression ratio and rated power. The crankshaft has two 6th order dampers.[4]

IO-360-C

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for accessory drive provisions. The crankshaft has two 6th order dampers.[4]

IO-360-CB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-C except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-D

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-A except for power rating and oil cooled pistons. The crankshaft has two 6th order dampers.[4]

Rolls-Royce Continental IO-360-D

Licence production in the United Kingdom by Rolls-Royce

IO-360-DB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-E

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for oil sump and suction tube. The crankshaft has two 6th order dampers.[4]

IO-360-ES

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Same as the IO-360-HB except for the modified spider induction system and the use of a TCM 639289A95 fuel injector. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-G

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-C except for crankshaft counterweight tuning. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-GB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-G except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-H

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-D except for crankshaft counterweight tuning. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-HB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-H except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-J

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-H except for power rating. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-JB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-J except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-K

{{convert|195|hp|kW|0|abbr=on}} at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-H except for power rating. The crankshaft has one 6th and one 4½ order damper.[4]

IO-360-KB

{{convert|195|hp|kW|0|abbr=on}} at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.5:1. Uses a TCM 639231A3 fuel injector. Same as the IO-360-K except for modified crankshaft. The crankshaft has one 6th and one 4½ order damper.[4]

TSIO-360

TSIO-360-A

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Base TSIO-360 model: a six-cylinder air-cooled, horizontally opposed direct drive, fuel injected, tuned induction, turbocharged engine with internal piston cooling oil jets.[5]

TSIO-360-AB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-A except for a modified crankshaft.[5]

TSIO-360-B

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-A except for accessory drive provisions.[5]

TSIO-360-BB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-B except for modified crankshaft and different dampers.[5]

TSIO-360-C

{{convert|225|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-A except for rating, crankshaft dampers provision for cabin pressurization.[5]

TSIO-360-CB

{{convert|225|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-C except for a modified crankshaft.[5]

TSIO-360-D

{{convert|225|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-C except for cabin pressurization.[5]

TSIO-360-DB

{{convert|225|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-D except for a modified crankshaft.[5]

TSIO-360-E

{{convert|215|hp|kW|0|abbr=on}} at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-C except for rating, engine mounted turbocharger, freon compressor drive and cabin pressurization.[5]

TSIO-360-EB

{{convert|215|hp|kW|0|abbr=on}} at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for a modified crankshaft.[5]

TSIO-360-F

{{convert|200|hp|kW|0|abbr=on}} at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for the power output rating and the exhaust system configuration.[5]

TSIO-360-FB

{{convert|200|hp|kW|0|abbr=on}} at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-F except for a modified crankshaft.[5]

TSIO-360-G

{{convert|210|hp|kW|0|abbr=on}} at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for the power output rating and the exhaust system configuration.[5]

TSIO-360-GB

{{convert|210|hp|kW|0|abbr=on}} at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-G except for a modified crankshaft.[5]

TSIO-360-H

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-G except for rating and cabin pressurization.[5]

TSIO-360-HB

{{convert|210|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-H except for a modified crankshaft.[5]

TSIO-360-JB

{{convert|225|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-HB except for the increased power output rating.[5]

TSIO-360-KB

{{convert|220|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-EB except for the increased power output rating.[5]

TSIO-360-LB

{{convert|210|hp|kW|0|abbr=on}} at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-GB but with a larger throttle body, larger induction elbows, relocated overboost valve, magneto pressurization and an exhaust muffler.[5]

TSIO-360-MB

{{convert|210|hp|kW|0|abbr=on}} at 36" mp and 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-LB except for intercooler, wastegate controller, maximum manifold pressure, and cluster manifold.[5]

TSIO-360-NB

{{convert|210|hp|kW|0|abbr=on}} at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-LB except for an intercooler.[5]

TSIO-360-PB

{{convert|200|hp|kW|0|abbr=on}} at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-MB but not equipped with an intercooler.[5]

TSIO-360-RB

{{convert|220|hp|kW|0|abbr=on}} at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, RH95/130 or B95/130 CIS, compression ratio 7.50:1. Same as the TSIO-360-KB except the manifold pressure is controlled with a wastegate controller, an intercooler is installed in the induction system, and uses a Precision Airmotive RSA-5AD2 fuel injection servo.[5]

TSIO-360-SB

{{convert|220|hp|kW|0|abbr=on}} at 39" mp and 2600 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-MB except for the manifold pressure, RPM, and power output rating.[5]

LTSIO-360

LTSIO-360-E

{{convert|215|hp|kW|0|abbr=on}} at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the TSIO-360-E except for direction of rotation.[5]

LTSIO-360-EB

{{convert|215|hp|kW|0|abbr=on}} at 2575 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the LTSIO-360-E except for a modified crankshaft.[5]

LTSIO-360-KB

{{convert|220|hp|kW|0|abbr=on}} at 2800 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 7.50:1. Same as the LTSIO-360-EB except for the increased power output rating.[5]

LTSIO-360-RB

{{convert|220|hp|kW|0|abbr=on}} at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, RH95/130 or B95/130 CIS, compression ratio 7.50:1. Same as the TSIO-360-RB except for direction of rotation.[5]

Applications

{{columns-list|colwidth=30em|
  • Aero Boero AB-210
  • AVE Mizar
  • Beriev Be-103
  • Cessna 160
  • Cessna R172K Hawk XP
  • Cessna Skymaster and military O-2 Skymaster
  • Cirrus SR20
  • Cierva CR Twin
  • Flight Design C4
  • Goodyear GZ-20
  • Ilyushin Il-103
  • Irkut A-002
  • Maule M-4
  • Maule M-5
  • Mooney M20
  • PAC CT/4
  • Piper PA-28R-201T Turbo Arrow
  • Piper PA-28-201T Turbo Dakota
  • Piper PA-34 Seneca
  • PZL M-20 Mewa
  • Reims FR172J Reims Rocket
  • Ryan XV-8
  • Sasin Spraymaster
  • T-41 Mescalero
  • White Lightning WLAC-1

}}

Specifications (IO-360-A)

{{pistonspecs|
|type=6-cylinder, fuel injected, horizontally opposed, piston engine
|ref=TYPE CERTIFICATE DATA SHEET NO. E1CE[4]
|bore=4.438 (112 mm)
|stroke=3.875 (98 mm)
|displacement=360 in³ (5.90 L)
|length=
|diameter=
|width=
|height=
|weight=294 lb (133 kg)
|valvetrain=
|supercharger=
|turbocharger=
|fuelsystem=
|fueltype=minimum 100LL Avgas
|oilsystem=
|coolingsystem=
|power=195 hp (145 kW) at 2,800 rpm continuous, 210 hp (157 kW) at 2,800 rpm for take-off
|specpower=
|compression=8.5:1
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=0.71 hp/lb
}}

See also

  • List of aircraft engines

References

Notes

1. ^{{Cite news|url = http://www.avweb.com/avwebflash/news/TeledyneContinentalMotors_SoldToTechnify_AVICInternational_China_203788-1.html |title = Teledyne-Continental Bought by Chinese Interests|accessdate = 27 March 2012|last = AvWeb Staff|authorlink = |date=December 2010| work = AvWeb}}
2. ^{{Cite news|url = http://www.businesswire.com/news/home/20101214005519/en/Teledyne-Technologies-Agrees-Sell-Teledyne-Continental-Motors|title = Teledyne Technologies Agrees to Sell Teledyne Continental Motors to AVIC International|accessdate = 27 March 2012|last = Teledyne Technologies Incorporated|authorlink = |date=December 2010| work = Business Wire}}
3. ^Taylor 1976, pp. 792–793
4. ^1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 {{cite web|url =http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/A7CBDD3D1C4DDC1086257355005674B2?OpenDocument&Highlight=360|title = TYPE CERTIFICATE DATA SHEET NO. E1CE Revision 15|accessdate = 2009-07-18|last = Federal Aviation Administration|authorlink = |date=September 2007}}
5. ^1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 {{cite web|url =http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/94439E5311979D638625748E0050D3F5?OpenDocument&Highlight=tsio-360|title = TYPE CERTIFICATE DATA SHEET NO. E9CE Revision 20|accessdate = 2009-01-18|last = Federal Aviation Administration|authorlink = |date=July 2008}}
6. ^{{Cite news|url = http://www.avweb.com/news/aopa/AOPASummit2011_Continental_Low_Octane_205415-1.html|title = Continental Introduces New Lower-Octane Engine|accessdate = 14 September 2011|last = Bertorelli|first = Paul|authorlink = |date=September 2011| work = AVweb}}

Bibliography

  • Taylor, J.W.R. (ed.). Jane's All the World's Aircraft 1976-77. London: Jane's, 1976. {{ISBN|0-354-00538-3}}.

External links

{{Commons category}}
  • [https://web.archive.org/web/20110615140127/http://www.tcmlink.com/EngSpecSheetDocs/LTSIO360RB.pdf Engine specification sheet]
{{Continental aeroengines}}

2 : Aircraft piston engines 1960–1969|Continental aircraft engines
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