Ivchenko AI-9: Difference between revisions
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{{Short description|1960s Soviet aircraft auxiliary power unit}} |
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{|{{Infobox Aircraft Begin|thumb|300x300px|AI9-3B |
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{|{{Infobox aircraft begin |
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| name=AI-9 |
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| caption=AI9-3B |
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}}{{Infobox aircraft engine |
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|type=[[Auxiliary Power Unit]] (APU) |
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|manufacturer=[[Ivchenko]] / [[Ivchenko-Progress]] / [[Motor Sich]] |
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|designer= |
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|national origin=[[USSR]] |
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|first run=1966 |
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The '''Ivchenko AI-9''' is an aircraft [[auxiliary power unit]] developed and produced by [[Ivchenko-Progress]] [[Motor Sich]].<ref name=":0">{{Cite web|url=http://www.motorsich.com/eng/products/aircraft/auxiliary/ai-9/|title=AI-9 - Motor Sich|last=Il'yashenko|first=Matviy|website=www.motorsich.com|access-date=2016-11-22}}</ref> |
The '''Ivchenko AI-9''' is an aircraft [[auxiliary power unit]] developed and produced by [[Ivchenko-Progress]] and [[Motor Sich]].<ref name=":0">{{Cite web|url=http://www.motorsich.com/eng/products/aircraft/auxiliary/ai-9/|title=AI-9 - Motor Sich|last=Il'yashenko|first=Matviy|website=www.motorsich.com|access-date=2016-11-22|archive-date=2017-01-10|archive-url=https://web.archive.org/web/20170110101016/http://www.motorsich.com/eng/products/aircraft/auxiliary/ai-9/|url-status=dead}}</ref> |
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<!-- ==Design and development== --> |
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== Variants == |
== Variants == |
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;AI-9: The base model which is used to supply compressed air to [[air-start system]]s. It can also be used as cabin heating if necessary.<ref name=":0" /> |
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;AI-9V: A variant of the base model that is used to supply compressed air to air-start systems and air conditioning. It also supplies electricity to on-board electrical systems with a 3 kW generator.<ref name=motorsichai9-V>{{Cite web|url=http://www.motorsich.com/eng/products/aircraft/auxiliary/ai-9v/|title=AI-9V - Motor Sich|last=Il'yashenko|first=Matviy|website=www.motorsich.com|access-date=2016-11-22|archive-date=2017-01-10|archive-url=https://web.archive.org/web/20170110101022/http://www.motorsich.com/eng/products/aircraft/auxiliary/ai-9v/|url-status=dead}}</ref> |
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;AI9-3B:The AI9-3B is used to provide air to engines and air conditioning systems and provide electricity to on-board electrical systems.<ref name=motorsichai9-3b>{{Cite web|url=http://www.motorsich.com/eng/products/aircraft/auxiliary/ai9-3b/|title=AI9-3B - Motor Sich|last=Il'yashenko|first=Matviy|website=www.motorsich.com|access-date=2016-11-22|archive-date=2017-01-12|archive-url=https://web.archive.org/web/20170112061832/http://www.motorsich.com/eng/products/aircraft/auxiliary/ai9-3b/|url-status=dead}}</ref> |
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{| class="metadata plainlinks stub" style="background:transparent" |
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|[[File:Aero-stub_img.svg|alt=Stub icon|20x20px]] |
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|''This article about aircraft engines is a [[Wikipedia:Stub|stub]]. You can help Wikipedia by [//en.wikipedia.org/enwiki/w/index.php?title=Ivchenko_AI-9&action=edit expanding it].''<div class="plainlinks hlist navbar mini" style="position: absolute; right: 15px; display: none;"> |
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==Specifications (AI-9) == |
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* [[Template:Engine-aircraft-stub|<abbr title="View this template">v</abbr>]] |
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{{jetspecs |
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* [[Template talk:Engine-aircraft-stub|<abbr title="Discuss this template">t</abbr>]] |
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* [//en.wikipedia.org/enwiki/w/index.php?title=Template:Engine-aircraft-stub&action=edit <abbr title="Edit this template">e</abbr>] |
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|ref=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=216 }}</ref> |
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|type=Auxiliary Power Unit (APU) |
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<span> </span> |
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|length={{cvt|740|mm}} |
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|diameter={{cvt|500|mm}} casing diameter |
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|weight={{cvt|45|kg}} |
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|compressor=1-stage centrifugal compressor |
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|combustion=Annular combustion chamber with 6 fuel injectors |
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|turbine=1-stage axial turbine (gas generator) |
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|fueltype=Aviation [[Kerosene]] such as [[JP-4]] |
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|oilsystem= |
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|power={{cvt|75|hp|order=flip}} (air hp) at 38,500 rpm or {{cvt|0.4|kg/s}} of compressed air at {{cvt|35|psi|bar|order=flip}} |
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|thrust= |
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|compression=2.8:1 |
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|bypass= |
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|aircon={{cvt|1.5|kg/s}} at 38,500 rpm |
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|turbinetemp= |
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|fuelcon={{cvt|120|kg/h}} maximum |
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|specfuelcon= |
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|power/weight={{cvt|0.75|hp/lb|order=flip}} (air hp) |
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|thrust/weight= |
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}} |
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==References== |
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{{Commons category}} |
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{{Reflist}} |
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<!-- ==External links== --> |
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{{Ivchenko aeroengines}} |
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[[Category:Ivchenko-Progress aircraft engines]] |
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Latest revision as of 00:28, 21 September 2024
AI-9 | |
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AI9-3B | |
Type | Auxiliary Power Unit (APU) |
National origin | USSR |
Manufacturer | Ivchenko / Ivchenko-Progress / Motor Sich |
First run | 1966 |
Major applications | Antonov An-140 Kamov Ka-27 Kamov Ka-28 Kamov Ka-29 Kamov Ka-32 Kamov Ka-50 Kamov Ka-52 Mil Mi-8 Mil Mi-14 Mil Mi-24 Mil Mi-28 Yakovlev Yak-40 |
The Ivchenko AI-9 is an aircraft auxiliary power unit developed and produced by Ivchenko-Progress and Motor Sich.[1]
Variants
[edit]- AI-9
- The base model which is used to supply compressed air to air-start systems. It can also be used as cabin heating if necessary.[1]
- AI-9V
- A variant of the base model that is used to supply compressed air to air-start systems and air conditioning. It also supplies electricity to on-board electrical systems with a 3 kW generator.[2]
- AI9-3B
- The AI9-3B is used to provide air to engines and air conditioning systems and provide electricity to on-board electrical systems.[3]
Specifications (AI-9)
[edit]Data from Aircraft engines of the World 1970[4]
General characteristics
- Type: Auxiliary Power Unit (APU)
- Length: 740 mm (29 in)
- Diameter: 500 mm (20 in) casing diameter
- Dry weight: 45 kg (99 lb)
Components
- Compressor: 1-stage centrifugal compressor
- Combustors: Annular combustion chamber with 6 fuel injectors
- Turbine: 1-stage axial turbine (gas generator)
- Fuel type: Aviation Kerosene such as JP-4
Performance
- Maximum power output: 56 kW (75 hp) (air hp) at 38,500 rpm or 0.4 kg/s (53 lb/min) of compressed air at 2.4 bar (35 psi)
- Overall pressure ratio: 2.8:1
- Air mass flow: 1.5 kg/s (200 lb/min) at 38,500 rpm
- Fuel consumption: 120 kg/h (260 lb/h) maximum
- Power-to-weight ratio: 1.23 kW/kg (0.75 hp/lb) (air hp)
References
[edit]Wikimedia Commons has media related to Ivchenko AI-9.
- ^ a b Il'yashenko, Matviy. "AI-9 - Motor Sich". www.motorsich.com. Archived from the original on 2017-01-10. Retrieved 2016-11-22.
- ^ Il'yashenko, Matviy. "AI-9V - Motor Sich". www.motorsich.com. Archived from the original on 2017-01-10. Retrieved 2016-11-22.
- ^ Il'yashenko, Matviy. "AI9-3B - Motor Sich". www.motorsich.com. Archived from the original on 2017-01-12. Retrieved 2016-11-22.
- ^ Wilkinson, Paul H. (1970). Aircraft engines of the World 1970 (21st ed.). Washington D.C.: Paul H. Wilkinson. p. 216.