Ok, thank you.I don't know. He didn't give much detail.
Latest Thread
Ok, thank you.I don't know. He didn't give much detail.
Just recently they announced 98% domestic rating and now they are not lying by saying +90%, they are ust not being precise.TEI Programs Director Ahmet Kain:
"In TEI-PD170, our domestic contribution rate has exceeded 90%. Aluminum alloy engine block, turbo systems, gearbox, alternator, etc. they are all local. "
It is becoming tedious to hear 70%, 90% etc% domestic crap!Just recently they announced 98% domestic rating and now they are not lying by saying +90%, they are ust not being precise.
TEI made its first trademark application for the turbofan engine on 5 May as the TF-6000.
Türk Patent Çevrimiçi Araştırma Uygulaması | Hoşgeldiniz...
online.turkpatent.gov.tr
In the biography of an engineer who worked at TEI, the project he worked on was described as follows.
Centrifugal Compressor, Axial Compressor and Axial Fan Aerodynamic Design of Turbofan(TFX & TF6000), Turbojet(TJ300 and TJ90) and Turboshaft (TS1400)
Either in kN or lbf, it sounds more of an UAV engine (Considering name of Goksungur was already spilled along with a time to be operational). This rather sounds like a project to be completed in short time, thus they have patented /labelled the product's name.So can we separate the two projects between TFX Turbofan engine studies and TF6000?
Would 6000 in TF6000 be the thrust in lbs ?
If so, we could expect engine similar to Adour Mk 106 which has 6,000 lb (27.0 KN) dry / 8,430 lb (37.5 KN) with reheat
Possibly the APU.Either in kN or lbf, it sounds more of an UAV engine (Considering name of Goksungur was already spilled along with a time to be operational). This rather sounds like a project to be completed in short time, thus they have patented /labelled the product's name.
Hurkus/TFX neither of them uses an engine in this league. (Correct me if i am wrong)
All TEI jet engines are named after their lbf values TJ90 TJ300.. Therefore could be 6000 lbf turbofan like the ones in business jets (like PW300,F124) It is too big for an APU role. Might be developed from TS1400. Engine at this size could power an Jet engine UAV or twin engine trainer. First I thought may be also for a big cruise missile but still too big for Gezgin.Possibly the APU.
Engines for even large cruise missiles are way smaller, Tomahawk uses a 2.7kn engine iirc.First I thought may be also for a big cruise missile but still too big for Gezgin.
Definitely too big for Gezgin, it will use AL-35 but still you can built an intercontinental cruise missile, found SM-62 Snark (was using 10000 lbf engine) as example, historic example but nowadays hypersonic cruise missiles for that range is more logical. As mentioned I think it is directly converted from TS1400.. If they have chosen twin engine hurjet, it could power a trainer (like M-346) .Engines for even large cruise missiles are way smaller, Tomahawk uses a 2.7kn engine iirc.
Not all. TS-1400 is not named after its lbf value. But I agree with you. 6000 probably stands for lbf.All TEI jet engines are named after their lbf values TJ90 TJ300.. Therefore could be 6000 lbf turbofan like the ones in business jets (like PW300) It is too big for an APU role. Might be developed from TS1400. Engine at this size could power an Jet engine UAV or twin engine trainer. First I thought may be also for a big cruise missile but still too big for Gezgin.
It looks like TS (Turbo Shaft) TJ (Turbo Jet) so TS1400 probably named after shp value(1,400 shp), TP (Turboprop) PD (piston, diesel?) PG (Piston Gasoline) (hp values) and TF6000 (Turbofan 6000)Not all. TS-1400 is not named after its lbf value. But I agree with you. 6000 probably stands for lbf.
Then it means TAI entering business jet job via Gulfstream G200 (aka the Gulfstream’s 1st product) like product.All TEI jet engines are named after their lbf values TJ90 TJ300.. Therefore could be 6000 lbf turbofan like the ones in business jets (like PW300,F124) It is too big for an APU role. Might be developed from TS1400. Engine at this size could power an Jet engine UAV or twin engine trainer. First I thought may be also for a big cruise missile but still too big for Gezgin.
What is Gezgin weight? AL-25 seems like it has a lot of thrust even compared to MDCN, and the Kalibr cruise missile engines.Definitely too big for Gezgin, it will use AL-25 (1140 lbf) but still you can built an intercontinental cruise missile, found SM-62 Snark (was using 10000 lbf engine) as example, historic example but nowadays hypersonic cruise missiles for that range is more logical. As mentioned I think it is directly converted from TS1400.. If they have chosen twin engine hurjet, it could power a trainer (like M-346) .
I made a typo sorry, I think it should be AL35 (c4defence says so) or AI-305 (under development) , probably less powered than AL25. I don't know the size and weight but fellow forum members could inform us. I am guessing it is directly similar to Tomahawk and could fit in Mark 41 VLS. So engine range would be between 600 to 1000 lbf, less than AL25What is Gezgin weight? AL-25 seems like it has a lot of thrust even compared to MDCN, and the Kalibr cruise missile engines.