Klimov TV2-117: Difference between revisions
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{{short description|1960s Soviet turboshaft aircraft engine}} |
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{|{{Infobox |
{|{{Infobox aircraft begin |
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|name= TV2-117 |
|name= TV2-117 |
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|image = File:Isotow TV-2-117A.jpg |
|image = File:Isotow TV-2-117A.jpg |
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|caption = |
|caption = |
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}} |
}} |
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{{Infobox |
{{Infobox aircraft engine |
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|type= [[Turboshaft]] |
|type= [[Turboshaft]] |
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|national origin = |
|national origin = |
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|manufacturer= [[Klimov]] |
|manufacturer= [[Klimov]] |
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|first run= |
|first run=1962 |
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|major applications= [[Mil Mi-8]]. |
|major applications= [[Mil Mi-8]]. |
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|number built = 23,000 |
|number built = 23,000 |
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|program cost = |
|program cost = |
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|unit cost = |
|unit cost = |
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|developed from = [[Klimov TV3-117]] |
|developed from = |
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|developed into = [[Klimov TV3-117]] |
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|developed into = |
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|variants with their own articles = |
|variants with their own articles = |
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}} |
}} |
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|} |
|} |
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The '''Klimov TV2-117''' (initially '''Isotov TV2-117''') is a Soviet gas-turbine [[turboshaft]] engine intended for helicopter use. Designed in the early 1960s by the [[Isotov Design Bureau]] the engine was later produced by [[Klimov]], |
The '''Klimov TV2-117''' (initially '''Isotov TV2-117''') is a Soviet gas-turbine [[turboshaft]] engine intended for helicopter use. Designed in the early 1960s by the [[Isotov Design Bureau]] the engine became the first purpose built gas turbine engine for helicopter use by the Soviet Union with previous helicopter turbines being adapted aeroplane powerplants. It was later produced by [[Klimov]], production ending in 1997.<ref name="Klimov">[http://en.klimov.ru/production/helicopter/TV2-117/ Klimov TV2-117 product page] {{webarchive|url=https://web.archive.org/web/20130307012729/http://en.klimov.ru/production/helicopter/TV2-117/ |date=2013-03-07 }} Retrieved: 24 May 2012</ref> |
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The TV2-117 is claimed to be the most popular helicopter powerplant worldwide and has accumulated over 100 million hours in service. |
The TV2-117 is claimed to be the most popular helicopter powerplant worldwide and has accumulated over 100 million hours in service. |
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''Source:Klimov.''<ref name="Klimov"/> |
''Source:Klimov.''<ref name="Klimov"/> |
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;TV2-117 |
;TV2-117 |
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:Base variant. |
:Base variant. |
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;TV2-117A |
;TV2-117A |
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;TV2-117TG |
;TV2-117TG |
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: |
:Multi-fuel variant, adapted to run on liquid petroleum gas and other fuels (gasoline or diesel fuel) and for use in cold climates. |
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==Applications== |
==Applications== |
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* [[Mil Mi-14]] |
* [[Mil Mi-14]] |
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==Specifications ( |
==Specifications (TV2-117A)== |
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{{jetspecs |
{{jetspecs |
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|ref=World Encyclopaedia of Aero Engines,<ref name=Gunston>{{cite book |last=Gunston |first=Bill |title=World Encyclopaedia of Aero Engines |year=1989 |publisher=Patrick Stephens Limited |location=Cambridge, England |isbn=978-1-85260-163-8 |edition=2nd |page=81}}</ref> World Encyclopaedia of Aero Engines,<ref name="Gunston"/> Aircraft engines of the World 1970<ref name=Wilkinson70>{{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1970 |year=1970 |publisher=Paul H. Wilkinson |location=Washington D.C. |edition=21st |page=214 }}</ref> |
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|ref=''Gunston''.<ref>Gunston 1989, p. 81.</ref> |
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|type=Turboshaft |
|type=Turboshaft |
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|length= |
|length={{cvt|2390|mm}} |
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|diameter= |
|diameter={{cvt|400|mm}}<br/> |
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*'''Frontal area:''' {{cvt|0.12|m2}} |
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|weight=330 |
|weight={{cvt|330|kg}} (minus accessories) |
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|compressor=Ten-stage axial flow |
|compressor=Ten-stage axial flow |
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|combustion=Eight-chamber cannular |
|combustion=Eight-chamber cannular |
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|turbine=Two-stage compressor turbine, two-stage power turbine |
|turbine=Two-stage compressor turbine, two-stage power turbine |
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|fueltype= |
|fueltype=Aviation [[Kerosene]] such as [[JP-4]] |
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|oilsystem=Pressure spray at {{cvt|50|psi|bar}} with return |
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|oilsystem= |
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|power= |
|power=<br/> |
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:*'''Take-off power:''' {{cvt|1500|shp}} at 12,000 rpm (power turbine) de-rated |
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:*'''Altitude power:''' {{cvt|1800|hp|kW|order=flip}} at 12,000 rpm (power turbine) at {{cvt|1200|m}} |
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|thrust= |
|thrust= |
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|compression=6.6:1 at 21,200 rpm |
|compression=6.6:1 at 21,200 rpm |
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|bypass= |
|bypass= |
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|aircon= |
|aircon={{cvt|8.1|kg/s}} |
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|turbinetemp= |
|turbinetemp='''TIT''' {{cvt|880|C|K|order=flip}} |
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|fuelcon= |
|fuelcon= |
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|specfuelcon=0.606 |
|specfuelcon={{cvt|0.606|lb/hph|kg/kWh}} |
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|power/weight= |
|power/weight={{cvt|2.06|hp/lb|kW/kg}} |
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|thrust/weight= |
|thrust/weight= |
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}} |
}} |
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==See also== |
==See also== |
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{{Aircontent |
{{Aircontent |
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|related= |
|related= |
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==References== |
==References== |
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{{Commons category|Isotov TV2-117}} |
{{Commons category|Isotov TV2-117}} |
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;Notes |
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{{reflist}} |
{{reflist}} |
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<!--==Further reading==--> |
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<!--==External links==--> |
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;Bibliography |
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{{refbegin}} |
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* Gunston, Bill. ''World Encyclopedia of Aero Engines''. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9 |
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{{refend}} |
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{{Klimov aeroengines}} |
{{Klimov aeroengines}} |
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{{Aviation lists}} |
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{{Aeroengine-specs}} |
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| ⚫ | |||
[[Category:Turboshaft engines 1960–1969]] |
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[[Category:Klimov aircraft engines]] |
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[[ru:TB2-117]] |
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[[ |
[[Category:Klimov aircraft engines|TV2-117]] |
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[[hu:TV2–117]] |
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Latest revision as of 21:39, 9 April 2024
| TV2-117 | |
|---|---|
| |
| Type | Turboshaft |
| Manufacturer | Klimov |
| First run | 1962 |
| Major applications | Mil Mi-8. |
| Number built | 23,000 |
| Developed into | Klimov TV3-117 |
The Klimov TV2-117 (initially Isotov TV2-117) is a Soviet gas-turbine turboshaft engine intended for helicopter use. Designed in the early 1960s by the Isotov Design Bureau the engine became the first purpose built gas turbine engine for helicopter use by the Soviet Union with previous helicopter turbines being adapted aeroplane powerplants. It was later produced by Klimov, production ending in 1997.[1]
The TV2-117 is claimed to be the most popular helicopter powerplant worldwide and has accumulated over 100 million hours in service. [1]
Variants
[edit]Source:Klimov.[1]
- TV2-117
- Base variant.
- TV2-117A
- Improved engine with more durable compressor stator blades.
- TV2-117AG
- Carbon sealed shaft bearings
- TV2-117F
- Limited production of engine certified to FAA airworthiness standards for Japan.
- TV2-117TG
- Multi-fuel variant, adapted to run on liquid petroleum gas and other fuels (gasoline or diesel fuel) and for use in cold climates.
Applications
[edit]- Antonov An-24 (intended coupled turboprop application)
- Mil Mi-8
- Mil Mi-14
Specifications (TV2-117A)
[edit]Data from World Encyclopaedia of Aero Engines,[2] World Encyclopaedia of Aero Engines,[2] Aircraft engines of the World 1970[3]
General characteristics
- Type: Turboshaft
- Length: 2,390 mm (94 in)
- Diameter: 400 mm (16 in)
- Frontal area: 0.12 m2 (1.3 sq ft)
- Dry weight: 330 kg (730 lb) (minus accessories)
Components
- Compressor: Ten-stage axial flow
- Combustors: Eight-chamber cannular
- Turbine: Two-stage compressor turbine, two-stage power turbine
- Fuel type: Aviation Kerosene such as JP-4
- Oil system: Pressure spray at 50 psi (3.4 bar) with return
Performance
- Maximum power output:
- Take-off power: 1,500 shp (1,100 kW) at 12,000 rpm (power turbine) de-rated
- Altitude power: 1,300 kW (1,800 hp) at 12,000 rpm (power turbine) at 1,200 m (3,900 ft)
- Overall pressure ratio: 6.6:1 at 21,200 rpm
- Air mass flow: 8.1 kg/s (1,070 lb/min)
- Turbine inlet temperature: TIT 1,150 K (880 °C)
- Specific fuel consumption: 0.606 lb/(hp⋅h) (0.369 kg/kWh)
- Power-to-weight ratio: 2.06 hp/lb (3.39 kW/kg)
See also
[edit]Comparable engines
Related lists
References
[edit]
Wikimedia Commons has media related to Isotov TV2-117.
- ^ a b c Klimov TV2-117 product page Archived 2013-03-07 at the Wayback Machine Retrieved: 24 May 2012
- ^ a b Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2nd ed.). Cambridge, England: Patrick Stephens Limited. p. 81. ISBN 978-1-85260-163-8.
- ^ Wilkinson, Paul H. (1970). Aircraft engines of the World 1970 (21st ed.). Washington D.C.: Paul H. Wilkinson. p. 214.