cabatli_53
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https://www.flightglobal.com/military-engines-russia/73364.article
- Prototype is prototype. The real overhaul hour after mass production and deployment is the number count.
- Also it's not professional to compare Turboshaft Engine with turbofan engines.
- The data of overhaul hours of turbofan engines is so outdated. AL-31F is 1500 hours 13 years ago.(TBO, not Mean time between overhaul)
Salyut-produced AL-31 powerplants are now qualified for a 1,500h time between overhauls (TBO) in 2007.
I don't want to slander anyone, but sorry to say Turkey is quite new to Engine. Turkey need at least decades to catch up.
The figures would need some update If they are really outdated but I received most figures from Wiki articles and Wiki revealed own figures by showing/quoting a source from 2008. At most idealistic scenarios, The Russian Al-31/41 series have a TBO around 1000-1500h and overall life time around 3000-4000h. In this source, It is stated that AL-41F(improved version of AL-31) has 1500h TBO and 4000h lifetime for exm. The Russian latest engines reach these figures in best scenarios. If We let the figures talk louder than our biasses, It seems Russian metallurgy lack behind than European engines developed around 20-25 years ago.
About Turkey, It is true that We are new in this field but We have qualified engineers transfered from abroad. Turkish institutes have great experiences and knowledge on some European and especially US engine programs. TEI itself is producing %70 of GE T700 (2000shp) turboshaft engines at present. 2500TAC equal to a figure around min 1000h TBO and Acc to TEI manager TEI TS-1500 will have min. 2500TAC but In final, We expect to reach 5000TAC in turbine core so serious investments have been done for metalurgy projects, especially on nickel coating, titanium alloy and blade cooling technologies. Indeed, We will see whether these figures will be reached. What TEI engineers are doing is pushing the limits of turbine blades (non-stop) at very high rpm figures while internal temperature of turbine is reaching 1700-1800 degrees on labratory scale. They have a trial roadway and they are following the steps in according to NATO standarts. If they didn't have anything worth to mention in their hands, They wouldn't have talked in that way with safe speeches about life of their turbine blades.
That's the sections that TEI reached knowledge on production processes. 01/2014, Red dots were the sections that TEI didn’t have capability to produce in 2014. All defficiencies have been closed with new manufacturing technics within 3 years.
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