This is about our capability gaps wrt materials (year 2022)
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Now tell me, should I believe scientists at GTRE or reporters who can not even visually differentiate between su-30 and mig-29?
So according to you we are manufacturing AL-31 engine from scratch from 2011 onwards...?
This is the only reason why I said what you have no knowledge about our manufacturing capabilities.
The slide you have posted shows our capabilities and limits when it comes to materials. These are the various exotic alloys that are yet to be indigenized. What does 'indigenisation' mean?
Indigenisation means made in India. What does it entail here.? Here it means from having ingots , powders of the various elements like Nickel, chromium , lanthanum, iron, titanium ,aluminium, etc you synthesise the alloys here in Indian plants and then supply them to the plants that require them, ie in this context HAL Koraput.
Now where do these elements come from ? These are present as compounds in their respective ores. You have to mine them and then extract the elements themselves from the oxides and compounds in the form of which they exist in nature. This is a different branch and is ultra vast.
It is metallurgy which is different from manufacturing of assemblies of engines.
Now coming to the matter in hand, besides the alloys indigenized by Midhani , the rest which comprises the vast majority are supplied to us by Russian OEM. These are the materials that are highlighted in your slide as yet to be indigenized.
besides, the alloys which are mentioned in the slide are half to almost a gen ahead of the materials used in AL-31 FP.
YOU are MIXING up MAKING HOT END COMPONENTS of AL-31FP and other jet engines with MANUFACTURING and SYNTHESISING the required ALLOYS from their RESPECTIVE ELEMENTS. Koraput GETS THEM from RUSSIA.
these high pressure turbine blades are made at Sukhoi division through investment casting. The surface finish achieved is as smooth as glass. So no further machining is required. These blades are the actual castings .
notice the series of fine holes on the leading edge of the turbine blade. Those are cooling channels through which relatively cooler air which has been diverted from the high pressure compressor section is passed through the blades to prevent them from losing their tensile strength and melting in the high thermal load environment.
Do read up about jet engines and the various processes that go into making each of the parts.Coz you simply don't have the basic understanding required to comprehend these stuff . You are mixing one thing with another.
Just watching some seminars from GTRE engineers on youtube won't cut it.