The ongoing achievements on national gas turbine R&D studies.
TEI designed 9 stage compressor providing same press/airflow ratio with original HP compressor with 10 stage designed by GE.
TEI designed combustion chamber reached %98+ Combustion efficiency in trials. That is a good indication for compressors and fuel injection working efficienctly to mix optimum amount of air/fuel particulars (1/14) in chamber.
TEI is working on advanced blades cooling technology to minimize the maintenance costs, while improving the efficiency and reliability of national gas turbine engines.
You can see the single crystal blade produced by TEI and domestic partners.
Other big problem inside the turbine is the retaining the strength level of blades. Steel, even Titanium drop off its strength level as you reach %40-50 of their melting points but Nickel alloy retain its strength up to %85 of its melting point. In turbine blades, Nickels combined with Aluminium improve strength of blades on even higher temperatures.
This magical alloy for turbine blades have been manufactured with additive manufacturing method by
TEI.
The first FBS module manufactured with titanium moulding process has been seen on image.
Blade Repairing with laser cladding technology is being developed for gas turbine engines.
TEI has reached technological maturity to manufacture all sections of turbine engines. Nickel, Aluminium, Titanium alloys and stainless steel with different manufacturing technics...
01/2014, Red dots were the sections that TEI didn’t have capability to produce in 2014. Within 3 years, All defficiencies have been filled with new manufacturing technics...