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The first airplane powered by two
Ivchenko AI-24 turboprops was the An-24. They drove four-bladed AV-72T constant-speed reversible propellers. Early production aircraft had AI-24 engines providing 1,790 kW (2,400 shp) takeoff power each, while later production airplanes were equipped with the
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The AI-24A was manufactured in large numbers in both the USSR and China. The popularity and success of
Antonov's An-24 series ensured that the AI-24 turboprop engine became one of the Soviet Union's most prominent and widely distributed engines worldwide. According to SE Ivchenko Progress, 2735
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Each engine nacelle included a fire extinguishing system that could be set to an automatic operation mode. The AI-24 turboprop engines featured wide gas dynamic stability margin at all power conditions, altitudes and flight speeds. The most notable feature of the engine was in its operational
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Attempts were made to also produce a turboshaft variant - for instance in 1960, eleven pre-production units of AI-24V turboshaft variants rated at 2000 hp were manufactured for powering the first two V-8 (Mi-8) prototype helicopters. However, later on, due to the fact that the
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passenger aircraft. True to the Soviet tradition, design was kept separate from serial production which was started in 1960. The turboprop engine along with many of the bureau's other designs were manufactured at Motor Sich which is also located in
Zaporozhye, Ukraine.
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The later AI-24T had water injection giving increased power output. It also introduced automatic limiting of power overloads and exhaust gas temperatures, along with vibration monitoring, automatic shutdown and feathering.
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turboprop engine and using advanced methods of simulation, a scaled-down turboprop engine, AI-24, rated at 2,550 hp (1,900 kW) (equivalent) was developed. The engine was specifically designed to power the
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Uprated variant produced 2,100 kW (2,820 shp) differentiated because it was coupled with an RU19A-300 APU/booster instead of the regular TG-16M auxiliary power unit (APU) turbine. It is mainly used to power the
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2,100 kW (2,800 shp) equivalent at 15,100 rpm with water injection and flat-rated to 11,500 ft (3,500 m) for take-off, (1,900 kW (2,500 shp) + 2.57 kN (578 lbf)).
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reliability. The main advantages of the engine were simple design, high reliability, long service life and easy maintainability.
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airplanes and 11750 units of the AI-24 engines of various modified versions were manufactured in total before production ended.
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Later
Production variant with performance maintained in hot-and-high conditions. maximum takeoff power 1,875 kW (2,515 ehp).
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Uprated variant which produced 2,103 kW (2,820 ehp) takeoff power for greater payload capability.
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engine was selected for powering the Mi-8, the works on the AI-24V engine aborted.
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Initial production variant producing 1,790 kW (2,400 shp) maximum takeoff power.
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574:(4th ed.). Sparkford, Nr Yeovil, Somerset, : P. Stephens. pp. 93–94.
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542:"RESTRICTED-TYPE CERTIFICATE DATA SHEET EASA.IM.A.351 Aircraft: Antonov 26"
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In 1958, based on the experience gained in the course of designing the
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599:(21st ed.). Washington D.C.: Paul H. Wilkinson. p. 218.
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was designed and developed in the late-1950s by the
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551:. European Aviation Safety Agency. 15 October 2009
186:The AI-24A produced 1,900 kW (2,550 shp).
412:3.52 kW/kg (2.14 hp/lb) (equivalent)
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499:. London: Jane's Publishing Co. p. 719.
331:Annular combustion chamber with 8 flame tubes
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360:pressure spray at 4.4 bar (64 psi)
284:Single-shaft turboprop with water injection
189:An improved series was introduced in 1966.
650:
636:
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435:"International Turbine Engine Directory"
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403:0.533 lb/(hp⋅h) (0.324 kg/kWh)
497:Jane's all the World's Aircraft 1980–81
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27:1950s Soviet turboprop aircraft engine
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572:World encyclopaedia of aero engines
823:Ivchenko-Progress aircraft engines
597:Aircraft engines of the World 1970
388:14.4 kg/s (1,900 lb/min)
272:Aircraft engines of the World 1970
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296:360 mm (14 in) (intake)
303:0.1 m (1.1 sq ft)
209:The AI-24 was later used on the
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495:Taylor, John W.R., ed. (1980).
137:and manufactured thereafter by
624:at the Polish Aviation Museum.
433:Fulton, K. (13 January 1979).
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290:2,436 mm (95.9 in)
595:Wilkinson, Paul H. (1970).
309:600 kg (1,300 lb)
141:. It was designed to power
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617:Motor Sich company website
392:Turbine inlet temperature:
49:Flugausstellung Hermeskeil
399:Specific fuel consumption
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394:823 K (550 °C)
828:1950s turboprop engines
470:. Ivchenko-progress.com
276:General characteristics
265:Specifications (AI-24T)
570:Gunston, Bill (1998).
408:Thrust-to-weight ratio
378:Overall pressure ratio
206:newer AI-24A engines.
161:Design and development
706:auxiliary power units
468:"ГП Ивченко-Прогресс"
371:Maximum power output:
442:Flight International
47:AI-24 on display at
523:. Motorsich.com.ua
100:Major applications
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659:Ivchenko-Progress
622:Ivchenko AI-24TW
157:aircraft series.
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16:(Redirected from
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448:(3643): 81–104
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145:'s successful
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135:design bureau
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113:Antonov An-30
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109:Antonov An-26
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105:Antonov An-24
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85:ZMKB Progress
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77:Manufacturer
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553:. Retrieved
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450:. Retrieved
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217:transports.
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71:Soviet Union
698:Turboshafts
549:easa.europa
365:Performance
358:Oil system:
320:Compressor:
307:Dry weight:
817:Categories
702:turboprops
527:2015-09-18
474:2015-09-18
417:References
354:or similar
344:Fuel type:
327:Combustors
314:Components
139:Motor Sich
91:First run
745:Turbofans
346:Aviation
294:Diameter:
270:Data from
125:turboprop
59:Turboprop
749:propfans
555:22 March
452:22 March
348:Kerosene
225:Variants
132:Ivchenko
81:Ivchenko
521:"AI-24"
336:Turbine
288:Length:
254:AI-24VT
181:TV2-117
143:Antonov
772:AI-322
762:AI-222
730:AI-450
578:
503:
382:7.05:1
260:An-26.
246:AI-24T
238:AI-24A
33:AI-24
802:D-436
797:D-236
782:D-18T
767:AI-25
757:AI-22
735:D-136
725:AI-24
720:AI-20
708:(APU)
688:AI-26
683:AI-14
545:(PDF)
438:(pdf)
282:Type:
230:AI-24
215:Аn-30
211:Аn-26
167:AI-20
155:An-30
151:An-26
147:An-24
94:1958
55:Type
792:D-36
787:D-27
777:DV-2
747:and
715:AI-9
704:and
678:AI-4
576:ISBN
557:2019
501:ISBN
454:2019
352:JP-1
213:and
153:and
120:The
446:115
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Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
