Does anyone know how the blades are prevented from sliding laterally and potentially falling from these disks?
It is basicly has a locking mechanism, this video talks about it among many other intersting subjects related to Turbuine blades.
Does anyone know how the blades are prevented from sliding laterally and potentially falling from these disks?
So now we have a name for the indigenous turbofan for Gezgin cruise missile.
A smaller engine than a full size fighter jet engine like the TS1500 or TS300 would be a good testbed to work on to experiment towards exotic applications due to its smaller size which will mean easier handling. A VTOL UCAV derived from such an engine could be the Turkish version of an F35B style fighter. Giving credit to Selçuk Bayraktar who alleged years ago that the F35 will be the last of the manned fighters.So now we have a name for the indigenous turbofan for Gezgin cruise missile.
I had also heard the name TJ1600 as a jet engine but it is not mentioned in other news.
However in one post TAI mentioned the number 34 as the number of projects they worked on. Which I believe includes several other configurations that were worked on in the process of developing the TS1400 turboshaft engine. If they worked on enough many configurations of engines that will lend itself to more exotic applications like VTOL propulsion can be derived from those engines. An axial flow turboshaft can be turned into a discrete fan turbofan engine with jet exhaust in the back. Kind of an extended shaft geared turbofan or the configuration that is on the F35B. I don't see why not.
Thanks to @Zafer
This might be totaly experimental stuff nonetheless It is exciting
From 2018 TEI magazine
Under "Original Engine development programs"
"...Beside, Syncronized Engineering work is contuined, supported by Production engineering department Design support under Turboshaft, TJ1600 and DP370 projects."
View attachment 9275
From CV of an Engineer from TEI
View attachment 9276
So There is indeed Turbojet Engine work in TEI with TJ1600 name.
Thanks to @Zafer
This might be totaly experimental stuff nonetheless It is exciting
From 2018 TEI magazine
Under "Original Engine development programs"
"...Beside, Syncronized Engineering work is contuined, supported by Production engineering department Design support under Turboshaft, TJ1600 and DP370 projects."
View attachment 9275
From CV of an Engineer from TEI
View attachment 9276
So There is indeed Turbojet Engine work in TEI with TJ1600 name.
Thanks to @Zafer
This might be totaly experimental stuff nonetheless It is exciting
From 2018 TEI magazine
Under "Original Engine development programs"
"...Beside, Syncronized Engineering work is contuined, supported by Production engineering department's Design support under Turboshaft, TJ1600 and DP370 projects."
View attachment 9275
From CV of an Engineer from TEI
View attachment 9276
So There is indeed Turbojet Engine work in TEI with TJ1600 name.
It is highly likely that the engine in question is this engine; but no specs mentioned.
1600hp equals around 3800lbf dry thrust. It will be in same league with Ivchenko Process Al-25TLT (3790lbf max)
Highly likely.Goksungur engine?
But isn't it a TJ and not a TS and thus the figure corresponds with thrust instead of hp?1600hp equals around 3800lbf dry thrust. It will be in same league with Ivchenko Process Al-25TLT (3790lbf max)
But what is DP37?Thanks to @Zafer
This might be totaly experimental stuff nonetheless It is exciting
From 2018 TEI magazine
Under "Original Engine development programs"
"...Beside, Syncronized Engineering work is contuined, supported by Production engineering department's Design support under Turboshaft, TJ1600 and DP370 projects."
View attachment 9275
From CV of an Engineer from TEI
View attachment 9276
So There is indeed Turbojet Engine work in TEI with TJ1600 name.
As it is 1600 HP and TJ as you say ; this is a thrust HP. Not Shaft HP!But isn't it a TJ and not a TS and thus the figure corresponds with thrust instead of hp?
But doesn't TEI use the number after the 'TJ' to indicate the thrust in pounds? For example: TEI TJ300 has 300 pounds of thrust.As it is 1600 HP and TJ as you say ; this is a thrust HP. Not Shaft HP!
According to Cabatli-53’s above share, two of these engines with this sort of dry thrust, can easily power a subsonic Hurjet or a supersonic Goksungur.
This engine seems to have been developed as a side product to the TS1400 engine and probably has the same BHP rating as its turboshaft equivalent. I have seen this engine at one of the trade-shows and it does have a similar combustor size to the TS1400 engine.But isn't it a TJ and not a TS and thus the figure corresponds with thrust instead of hp?
Hmm, I'll have to take your word for it then, but I am not entirely convinced.This engine seems to have been developed as a side product to the TS1400 engine and probably has the same BHP rating as its turboshaft equivalent. I have seen this engine at one of the trade-shows and has similar combustor size to the TS1400 engine.
Do you take bribes.Hmm, I'll have to take your word for it then, but I am not entirely convinced.
$30000Do you take bribes.