Even protein folding research benefit from advanced technology so will metallurgy field. As far as we can see Türkiye has already achieved some levels in hot section parts of engines. I guess we can achieve F110 engine power levelc already and looking for better performance. We will know what we are made of when the engine is built. Or I would say as early as when the TF10000 is built.No sir, they won't help much. There is a huge difference between TF35000 and TF10000. Why? You see, as the thrust requirement increases, the intake temperature at the turbine increases. The only limit on this temperature is due to metallurgical constraints. And no one will share with you the metallurgy because this is decades of research. Even in the US-India F414 engine deal, where the US agreed to share 80% of the TOT, the metallurgy details were not included. China has struggled with jet engine technology for years. Why? The jet engine blades run at extreme temperatures, and the challenge of overcoming the heat problem has plagued China until now. The blades overheated at higher output levels, causing premature failure and forcing engineers to reduce power output so the engines would have a reasonable lifespan. Aerodynamics, thermodynamics, material science, structural integrity, and control systems are very complex for optimized performance and efficiency. It is no easy task to bring a high-thrust output engine to life in less than a decade.
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