Chinese Engine Development

siegecrossbow

General
Staff member
Super Moderator
Important component in Chinese turbofan engine reaches a lifespan of 50,000 hours.

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Component in question.

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Red tsunami

Junior Member
Registered Member
Russian jet engines fell behind because of the lost decade in the 1990s. If you look at the specs of the Saturn AL-41F for the Soviet MiG Project 1.44 they are not behind those in the US ATF. The Soviets had times when they were behind in jet engine technology, and times when they were slightly ahead in some aspects, more times when they were behind, but in the late Brezhnev era they were pretty much either to par or the Soviets had a slight edge. The main issue the Soviets had was lack of modern FADEC.

But this AL-41F is too big.

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gelgoog

Brigadier
Registered Member
The original AL-41F engine was supposed to be used in pairs on the MFI aka MiG Project 1.44 and as a single unit on the LFI.
You usually do not define engine generation by either size or thrust but by thrust-weight, turbine inlet temperature, and things like that.
The AL-41F was a variable bypass ratio engine, so it was in fact technologically more advanced than either the F-22 or F-35 engine and more similar to the GE engine used in the YF-23. The turbine inlet temperature is similar to that of the F-22 engine and the thrust-weight is better and closer to the F-35 engine.

The AL-41F was large because in order to fullfill the missions required by the Russian defense ministry with the single engine aircraft back then they needed more power than could be done with a smaller engine. The AL-41F engine prototype first flew on a MiG-25 which is an aircraft with much larger engines than a Flanker.

Anyway the project got cancelled and the engine never got properly finished, never got certified, and never entered serial production. They made several prototypes for testing including flight testing but that was about it.
 
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