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{{Short description|Russian military turbofan engine variants}} | |||
{{refimprove|date=May 2014}} | |||
{|{{Infobox aircraft begin | {|{{Infobox aircraft begin | ||
|name= AL-41F | |name= AL-41F | ||
|image = |
|image = | ||
|caption = |
|caption = | ||
}} | }} | ||
{{Infobox aircraft engine | {{Infobox aircraft engine | ||
|type= ] ] | |||
|type= ] | |||
|national origin = Russia | |national origin = Russia | ||
|manufacturer= ] | |manufacturer= ] | ||
|first run= | |first run= | ||
|major applications= | |major applications=] | ||
|number built = | |number built = | ||
|program cost = | |program cost = | ||
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The '''AL- |
The '''AL-41''' is a designation for two different Russian military turbofan engine variants by ]. The original '''AL-41F''', development designation '''''izdeliye''''' '''20''', was a variable-bypass ratio ], designed for ] flight for the ''MFI'' (''Mnogofunktsionalni Frontovoy Istrebitel'', "Multifunctional Frontline Fighter") program, which resulted in the ]. It is considered by ] as the Russian counterpart to the ] engine which lost to the more conventional fixed-bypass YF119 in the ] engine program. | ||
Since the cancellation of the MFI program, the '''AL-41F1S''' (''izdeliye'' 117S) and '''AL-41F1''' (''izdeliye'' 117) designations were assigned to engines developed by Lyulka-Saturn, now ], that respectively power the ] and ], but these are heavily upgraded variants of the ], rather than variants of the ''izdeliye'' 20 design. | |||
⚫ | ==Design and development== | ||
The AL-41F program was launched in 1982, and the first prototype engine flew in a ] testbed. Originally developed for the ],<ref>http://archive.russia-today.ru/2009/no_12/12_from_backlog_01.htm</ref><ref>http://maria-online.com/cinema/article.php?q=%D0%90%D0%9B-41%D0%A4</ref> 28 engines were built, however the engine did not advance beyond prototype stage and when the MiG 1.44 was cancelled. | |||
⚫ | ==Design and development== | ||
The AL-41 designation was reused for heavily upgraded variants of the AL-31 used to power the Su-35S (Izdeliye 117S / AL-41F1A) and initial production PAK FA (Izdeliye 117 / AL-41F1) stealth aircraft. Some of the technologies of the original AL-41F were applied in the 117S and 117 engines. | |||
In the late 1970s and early 1980s, the Soviet Defence Ministry identified the need for a 1990s fighter, or I-90, that would eventually succeed the MiG-29 and Su-27, resulting in the MFI fifth-generation multirole fighter program. The AL-41F, with development project designation ''izdeliye'' 20, was launched in 1982, and was intended to power the MFI, which was to be developed by Mikoyan under its ].<ref>Butowski 2021, p. 6</ref> The first prototype engine flew in a ] testbed. An 18–tonne (177 kN, 40,000 lbf) class engine, the AL-41F used a variable bypass architecture to facilitate the aircraft in supercruise, or fly at speeds of Mach 1.5 without afterburner. It had the ambitious goal of increasing the turbine inlet temperature by 250 °C over its ] predecessor, and was expected to incorporate ] to enhance the fighter's maneuverability.<ref name="flight international"/> After the collapse of the Soviet Union, both the MFI and the AL-41F suffered from severe funding disruptions and lengthy delays; production plans for the MFI was halted in 1997 due to high costs. Eventually, 28 AL-41Fs were built and the engine was first flown on the MiG 1.44 in 2000, but it did not advance beyond prototype stage when all further work on the MFI ceased later that year.<ref>{{cite web |url=http://archive.russia-today.ru/2009/no_12/12_from_backlog_01.htm |title=Виктор ЧЕПКИН (Victor CHEPKIN interview), "Сатурн" выходит из-за туч |work=Russia Today |date=June 2008 |accessdate=2012-09-21 |url-status=dead |archiveurl=https://web.archive.org/web/20100616231722/http://archive.russia-today.ru/2009/no_12/12_from_backlog_01.htm |archivedate=2010-06-16 }}</ref> | |||
With the abandonment of the MFI, the Russian Defence Ministry embarked on the more affordable PAK FA fifth-generation fighter program, with the competitive tender announced in April 2001. As the aircraft from this program would be smaller than the MFI, the AL-41F was too large to fit into the competing proposals.<ref name="new al-41">{{cite web |url=https://www.flightglobal.com/new-al-41-unveiled-at-maks-2001-/39275.article |title=New AL-41 Unveiled at MAKS 2001 |work=Flight International |date=27 August 2001}}</ref> The AL-41 designation was then reused for heavily upgraded variants of the ] that would power Sukhoi's T-50 design for the PAK FA; these include the AL-41F1 (''izdeliye'' 117) developed for the T-50, eventually named ], as well as the slightly simpler AL-41F1S (''izdeliye'' 117S) derivative for a highly upgraded Su-27 variant called the T-10BM, eventually designated ].<ref>{{cite web |url=https://nplus1.ru/material/2019/03/06/engines |title=Плазменный мотор |work=nplus1.ru |date=6 March 2019}}</ref> Some of the technology of the original AL-41F were applied in the ''izdeliye'' 117S and 117 engines, but it is important to note that these engines are not considered a part of the same AL-41F line (''izdeliye'' 20) as was planned for the ] because their cores are based on the AL-31F's, whereas the AL-41F utilizes an entirely different approach. The designation is present because the engine approaches some of the projected specifications of the AL-41F. As Sukhoi anticipates that the Su-57 will be the basis for a family of stealth combat aircraft, future improved variants are expected to incorporate a new design from Saturn designated the ], or ''izdeliye'' 30, that would eventually replace the AL-41F1.<ref>Butowski 2021, p. 89</ref> | |||
==Variants== | |||
A heavily upgraded version of the AL-31F is being developed for the ] and ]. This engine has been named the ] and AL-41F1. It is important to note that the AL-41F1S is not considered a part of the same AL-41 line as was planned for the ] because it uses the core of the AL-31F, whereas the AL-41F utilizes an entirely different approach. The designation is present because the engine approaches the projected specifications of the AL-41F. It is also notable that the engine is capable of mounting 3D ] nozzles for extra maneuverability. | |||
⚫ | ==Specifications (AL-41F, ''izdeliye'' 20)== | ||
===Operators=== | |||
* {{flag|Russia}} | |||
* {{flag|People's Republic of China}} | |||
⚫ | ==Specifications== | ||
{{jetspecs | {{jetspecs | ||
<!-- If you do not understand how to use this template, please ask at ] --> | <!-- If you do not understand how to use this template, please ask at ] --> | ||
<!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> | <!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> | ||
|ref=Kommersant,<ref name="kommersant">{{cite web |url=http://www.kommersant.ru/doc/833099 |title=Подробнее |work=Kommersant |date=10 December 2007}}</ref> Leteckemotory,<ref name="leteckemotory">{{cite web |url=http://www.leteckemotory.cz/motory/al-41/ |title=AL-41F |work=Leteckemotory}}</ref> Flight International<ref name="flight international">{{cite web |last=Velovich |first=Alexander |url=https://www.flightglobal.com/news/articles/al-41-engine-problems-are-over-says-lyulka-saturn-25271/ |title=AL-41 engine problems are over, says Lyulka Saturn |work=Flight International |date=1 August 1995}}</ref> | |||
|ref= | |||
|type=Turbofan | |type=Turbofan | ||
|length= |
|length= | ||
|diameter= |
|diameter= | ||
|weight= | |weight=1,500 kilogram | ||
|compressor=axial | |compressor=axial | ||
|combustion= | |combustion= | ||
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|oilsystem= | |oilsystem= | ||
|power= | |power= | ||
|thrust={{ |
|thrust={{Convert|176|kN|lbf|abbr=on|order=flip}} | ||
|compression= | |compression= | ||
|bypass= | |bypass= | ||
|aircon= | |aircon= | ||
|turbinetemp= | |turbinetemp={{cvt|1642|C|K F|0}} | ||
|fuelcon= | |fuelcon= | ||
|specfuelcon= | |specfuelcon= | ||
|power/weight= | |power/weight= | ||
|thrust/weight=11:1 | |thrust/weight=10.5 - 11:1 | ||
}} | }} | ||
==See also== | ==See also== | ||
{{Aircontent | |||
* ] | |||
|see also=<!-- other related articles that have not already linked: --> | |||
|related=<!-- designs which were developed into or from this engine: --> | |||
* ], highly improved AL-31 variant with AL-41F technology applied | |||
|similar engines=<!-- For aircraft engine articles. Engines that are of similar to this design: --> | |||
* ] | |||
* ] | * ] | ||
* ] | * ] | ||
* ] | |||
|lists= | |||
* ] | |||
<!-- See ] for more explanation of these fields. --> | |||
}} | |||
==References== | ==References== | ||
{{reflist|30em}} | {{reflist|30em}} | ||
== |
==Sources== | ||
{{Refbegin}} | {{Refbegin}} | ||
* {{Cite book |last=Butowski |first=Piotr |title=Su-57 Felon |location=Stamford, UK |publisher=Key Books |year=2021 |isbn=978-1-913870-44-7 |url=https://shop.keypublishing.com/product/View/productCode/KB0043/Su-57%20Felon}} | |||
* Butowski, Piotr. "Raptorski's Maiden Flight". '']'', Vol. 78, No 3, March 2010, pp. 30–37. Stamford, UK: Key Publishing. | |||
* Butowski, Piotr. "T-50 Turning and Burning over Moscow". '']'', Vol. 85, No 4, October 2013, pp. 79–82. Stamford, UK: Key Publishing. | |||
{{Refend}} | {{Refend}} | ||
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] | ] | ||
] | ] | ||
] | ] |
Latest revision as of 20:02, 6 November 2024
Russian military turbofan engine variantsAL-41F | |
---|---|
Type | Variable cycle turbofan |
National origin | Russia |
Manufacturer | NPO Saturn |
Major applications | Mikoyan Project 1.44 |
The AL-41 is a designation for two different Russian military turbofan engine variants by NPO Lyulka-Saturn. The original AL-41F, development designation izdeliye 20, was a variable-bypass ratio turbofan engine, designed for supercruise flight for the MFI (Mnogofunktsionalni Frontovoy Istrebitel, "Multifunctional Frontline Fighter") program, which resulted in the Mikoyan Project 1.44. It is considered by Jane's as the Russian counterpart to the General Electric YF120 engine which lost to the more conventional fixed-bypass YF119 in the Advanced Tactical Fighter engine program.
Since the cancellation of the MFI program, the AL-41F1S (izdeliye 117S) and AL-41F1 (izdeliye 117) designations were assigned to engines developed by Lyulka-Saturn, now NPO Saturn, that respectively power the Sukhoi Su-35S and Sukhoi Su-57, but these are heavily upgraded variants of the AL-31F, rather than variants of the izdeliye 20 design.
Design and development
In the late 1970s and early 1980s, the Soviet Defence Ministry identified the need for a 1990s fighter, or I-90, that would eventually succeed the MiG-29 and Su-27, resulting in the MFI fifth-generation multirole fighter program. The AL-41F, with development project designation izdeliye 20, was launched in 1982, and was intended to power the MFI, which was to be developed by Mikoyan under its 1.44/1.42 project. The first prototype engine flew in a MiG-25 Foxbat testbed. An 18–tonne (177 kN, 40,000 lbf) class engine, the AL-41F used a variable bypass architecture to facilitate the aircraft in supercruise, or fly at speeds of Mach 1.5 without afterburner. It had the ambitious goal of increasing the turbine inlet temperature by 250 °C over its AL-31F predecessor, and was expected to incorporate thrust vectoring to enhance the fighter's maneuverability. After the collapse of the Soviet Union, both the MFI and the AL-41F suffered from severe funding disruptions and lengthy delays; production plans for the MFI was halted in 1997 due to high costs. Eventually, 28 AL-41Fs were built and the engine was first flown on the MiG 1.44 in 2000, but it did not advance beyond prototype stage when all further work on the MFI ceased later that year.
With the abandonment of the MFI, the Russian Defence Ministry embarked on the more affordable PAK FA fifth-generation fighter program, with the competitive tender announced in April 2001. As the aircraft from this program would be smaller than the MFI, the AL-41F was too large to fit into the competing proposals. The AL-41 designation was then reused for heavily upgraded variants of the Saturn AL-31 that would power Sukhoi's T-50 design for the PAK FA; these include the AL-41F1 (izdeliye 117) developed for the T-50, eventually named Su-57, as well as the slightly simpler AL-41F1S (izdeliye 117S) derivative for a highly upgraded Su-27 variant called the T-10BM, eventually designated Su-35. Some of the technology of the original AL-41F were applied in the izdeliye 117S and 117 engines, but it is important to note that these engines are not considered a part of the same AL-41F line (izdeliye 20) as was planned for the Mikoyan Project 1.44 because their cores are based on the AL-31F's, whereas the AL-41F utilizes an entirely different approach. The designation is present because the engine approaches some of the projected specifications of the AL-41F. As Sukhoi anticipates that the Su-57 will be the basis for a family of stealth combat aircraft, future improved variants are expected to incorporate a new design from Saturn designated the AL-51F-1, or izdeliye 30, that would eventually replace the AL-41F1.
Specifications (AL-41F, izdeliye 20)
Data from Kommersant, Leteckemotory, Flight International
General characteristics
- Type: Turbofan
- Length:
- Diameter:
- Dry weight: 1,500 kilogram
Components
- Compressor: axial
Performance
- Maximum thrust: 40,000 lbf (176 kN)
- Turbine inlet temperature: 1,642 °C (1,915 K; 2,988 °F)
- Thrust-to-weight ratio: 10.5 - 11:1
See also
Related development
- Saturn AL-41F1, highly improved AL-31 variant with AL-41F technology applied
Comparable engines
Related lists
References
- Butowski 2021, p. 6
- ^ Velovich, Alexander (1 August 1995). "AL-41 engine problems are over, says Lyulka Saturn". Flight International.
- "Виктор ЧЕПКИН (Victor CHEPKIN interview), "Сатурн" выходит из-за туч". Russia Today. June 2008. Archived from the original on 2010-06-16. Retrieved 2012-09-21.
- "New AL-41 Unveiled at MAKS 2001". Flight International. 27 August 2001.
- "Плазменный мотор". nplus1.ru. 6 March 2019.
- Butowski 2021, p. 89
- "Подробнее". Kommersant. 10 December 2007.
- "AL-41F". Leteckemotory.
Sources
- Butowski, Piotr (2021). Su-57 Felon. Stamford, UK: Key Books. ISBN 978-1-913870-44-7.
External links
Lyulka and Saturn aircraft engines | |
---|---|
Turbojets | |
Turbofans | |
Turboprops | AL-34 |
Joint development | PowerJet: SaM146 (Turbofan) |