cabatli_53
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TEI has achieved great success inside a relatively short time period and TEI-TS-1400 turboshaft engine core turbine is passed the acceptance trials succesfully. 250 TEI engineers have designed it.
TEI-TS-1400 is a 60cm diameter class engine and It will generate a power around 1400 to 1660shp. TEI states that The core section of Ts-1400 will be converted into turbojet, turboprop and turbofan engines when they applied needed modifications for air inlet and exhaust section.
When 60cm diameter class TS-1400 (T700-GE-701 (2000shp) turboshaft engine:66cm diameter) core engine converted into turbofan, Turkiye will have developed a turbofan which has a dry thrust up to 9500lbf. Turboprop variant of TS-1400 core will be integrated on Hürkuş trainers.
70cm (I suppose) diameter class TS-3000 (3000shp) turboshaft engine is under development phase by TEI. TS-3000 will be the main power source of Atak-II and 10+t utility helicopter programs. When TS-3000 core engine is converted into turbofan engine, Turkey will have developed a new jet engine having a dry thrust ratio up to 16500 shp. With afterburners, Thrust of this engine can be increased up to 20000lbf. This modification will allow us to power Hürjet advanced jet trainer and light fighter aircraft.
TEI-TS-1400 is a 60cm diameter class engine and It will generate a power around 1400 to 1660shp. TEI states that The core section of Ts-1400 will be converted into turbojet, turboprop and turbofan engines when they applied needed modifications for air inlet and exhaust section.
When 60cm diameter class TS-1400 (T700-GE-701 (2000shp) turboshaft engine:66cm diameter) core engine converted into turbofan, Turkiye will have developed a turbofan which has a dry thrust up to 9500lbf. Turboprop variant of TS-1400 core will be integrated on Hürkuş trainers.
70cm (I suppose) diameter class TS-3000 (3000shp) turboshaft engine is under development phase by TEI. TS-3000 will be the main power source of Atak-II and 10+t utility helicopter programs. When TS-3000 core engine is converted into turbofan engine, Turkey will have developed a new jet engine having a dry thrust ratio up to 16500 shp. With afterburners, Thrust of this engine can be increased up to 20000lbf. This modification will allow us to power Hürjet advanced jet trainer and light fighter aircraft.
- TurboMeca M88-4E (69,5cm inlet diameter): 20000lb (planned)
- F404-GE-102 (71cm diameter): 18000lbf
- F404-IN20 (71cm diameter): 19000lbf
- EJ-200 (80cm diameter): 20000lbf