With all due respect to what you have written here, how do you know that electric generation, noise issue, IR signature and sound performance of the F110 engine won’t be any problem? Do you have concrete figures that support your suppositions to share with us?
If what you suppose were the case, there would be no need to develop a 5th generation engine specific to this plane. There would be no mention of 5th generation class engines.
Another point I have not included among the list would be the engine’s thrust potential to be high enough to support plane’s high supercruise capability.
Those guys in TEI and TAI and those guys in P&W and GE must see these points as lacking and not up to 5th generation requirements in the F110 as is. Hence they see the need to develop an engine that is suitable to provide above 5th generation properties.
Regarding engine fan design/inlet of turbofan with respect to stealth properties and electromagnetic scattering;
Quote:
With the continuous advancement of rotor dynamic electromagnetic scattering research, the radar cross-section (RCS) of turbofan engines has attracted more and more attention. In order to solve the electromagnetic scattering characteristics of a biaxial multirotor turbofan engine, a dynamic scattering method (DSM) based on dynamic simulation and grid transformation is presented, where the static RCS of the engine and its components is calculated by physical optics and physical theory of diffraction. The results show that the electromagnetic scattering of the engine is periodic when the engine is working stably, while the rotors such as fans and turbines are the main factors affecting the dynamic electromagnetic scattering and the ducts greatly increase the overall RCS level of the engine. The proposed DSM is effective and efficient for studying the dynamic electromagnetic scattering characteristic of the turbofan engine.
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PS
APU of all jet planes are there for starting power for the main engines, Pneumatic power for cabin air conditioning systems, Shaft power for other pneumatic and hydraulic systems, Back up and emergencies, Electric and pneumatic power for ground operations with the engines shut down.
Nothing to do with 5th generation power requirements.
1- I said they are not an issue for now, they will be a problem when TAI/Havelsan decides to increase AI etc. And keep in mind that 2 of these F110s also keep F-15EX at the sky, yeah TF-X will probably consume more power, but at least for IOC, it should be enough.
I didn't said F110 won't have IR problems, but it won't be a great difference, as IR performance hugely depends on air scoops and thermal isolation of the body, you can't really achieve IR stealth with only engine or only body, that's why I said it will have worse IR, but this doesn't mean that it is going to shine
As you can see, in non IR stealth jets, body around the engine shines while in F-22, only where the engine is situated shines, and that's the result of body and engine combined.
For noise, at least for now, or for the limited time it is going to be used, there are no noise triangulation method to find enemy aircraft, there will definetly be in the future, but not for now.
Yes you are right about supercruise, it wont be around 1.5-1.6 Mach with F110 for sure, but I didn't list it either because most of 5th gens don't have high supercruise capability.
Hmm, so you were talking about "fan" inlet and blades, yes you are right, but how much is it going to affect and we just dump down all geometric stealth and call it a 4.5?
And yes you are right, I confused it with electric generation on ground to electric generation on air.
PS: I never said we don't need an engine, I just stated the reason why it can't be 4.5th gen with it, for it to be 4.5, it must lack VLO geometry+RAM, and KF-21 lacks:
Serrated edges, RAM (to some extent), canopy coating and various other stealth features, that's why it is not a true 5th gen but something in between 4.5 and 5
TF-X is like J-20 with older engines, it is still 5th gen because VLO and subsystems but lacks IR stealth of engine and has worse performance than what it should have