Chengdu next gen combat aircraft (?J-36) thread

latenlazy

Brigadier
Im curious but how big of an impact does electricity generation have on thrust? I feel like even with a high power requirement like say 1MW, that still represents a relatively small amount of total power an engine is capable of producing. Now amortizing that over 2 or even 3 engines I feel would probably be negligible per engine
It’s the other way around. The thrust will be fine. It’s the electrical system that needs a reliable generator. If you’re running two engines and there’s power drop off in one or both of them the plane will fly fine but the electrical output might get disrupted. You’re not likely to *lose* all electric power but for high output electrical systems especially losing output can disrupt system performance, sometimes when you need surge capacity. Distributing that load to three sources with one primary and two auxiliary helps resolve those kinds of situations.
 

Blitzo

Lieutenant General
Staff member
Super Moderator
Registered Member
Fair point, three WS-15s provide about 40% more thrust than two turbocharged F135s.

It's not just about thrust, it is also about bypass ratio and exhaust velocity.


That said, this three engine arrangement just seems bizarrely complex.

It's probably simpler than developing an engine that is able to meet all of the requirements for J-36 in a two engine configuration, in a manner which is timely and effective.


These three engines will burn a ton of fuel.

Three engines will burn more fuel than two engines of the same model.
However an aircraft with three engines can also be heavier than an aircraft with two engines of the same model, thus carry more fuel.

It may well be that an aircraft with three engines of the same model can achieve greater range than an aircraft with two engines of the same model, because the two engine design will inevitably have a lower MTOW.


The dorsal intake will increase drag and make stealth more challenging.

You're really looking at things from an individual perspective here.
A dorsal intake will increase and compromise signature reduction relative to having no dorsal intake yes -- but no dorsal intake means either no third engine (thus having a smaller aircraft), or forcing your two side mounted intakes bigger, which is something perhaps the airframe is unable to accommodate with adverse consequences to signature reduction and drag (compared to having a dorsal mounted intake as a solution instead).


The third intake make the pilot's rear visibility (already bad with the J-36 cockpit) even worse. I guess rearward visibility isn't seen as an issue given that this thing will have a solid DAS capability and the aircraft will operate at stand-off ranges.

If the aircraft is in a position where they need the Mk1 eyeball to glance rearwards, then something has gone wrong.


Also, how will the dorsal engine affect air-to-air refuelling?

Air refuelling probes are usually mounted on the side, thus offset from the dorsal air intake.
X-47B uses a probe and has a single dorsal intake. I consider it a non-issue, and it's odd you would even raise it as if it is a genuine engineering conundrum.



KFX, the best way for you to approach the 3 engine matter, is to try to reverse engineer out the combination of compromises by first assuming the following conclusion:
"The three engine configuration for J-36 is the most effective and capable configuration for the mission that the PLA expects, and is irrespective of engine technology relative to the rest of the world".

From there, you can start to come up with reasons for yourself for why they've chosen the three engine, three intake configuration among the permutation of engineering decisions they've made.

Instead of "why would they choose a three engine design because of XYZ deficiencies," think and come at it from this angle "of course they would choose a three engine design, because of XYZ benefits".
 
Last edited:

Blitzo

Lieutenant General
Staff member
Super Moderator
Registered Member
It’s the other way around. The thrust will be fine. It’s the electrical system that needs a reliable generator. If you’re running two engines and there’s power drop off in one or both of them the plane will fly fine but the electrical output might get disrupted. You’re not likely to *lose* all electric power but for high output electrical systems especially losing output can disrupt system performance, sometimes when you need surge capacity. Distributing that load to three sources with one primary and two auxiliary helps resolve those kinds of situations.

Three engines overall also offer more growth capacity for power generation in the long term -- assuming each engine has its own genset, and as gensets will likely advance and improve in future, you'll get disproportionately more power generation from a three engine setup versus an equivalent two engine setup.
 

FairAndUnbiased

Brigadier
Registered Member
Ai yah. It's not about being pro-China or anti-China, just discussing things objectively. One fault I have with these forums is the nationalistic assumption that Chinese aircraft designers are ten feet tall. Chinese aircraft designers screw up, Western designers screw up...and sometimes they get things right. J-36 is a fascinating aircraft, but its worth being objective about it...and admitting how little we actually know.

Yeah, I'm sure they can sort out the air-to-air refuelling bit...maybe a bit more work, but doable...
Aircraft designers are working with billions of dollars and state of the art national level scientific resources with multiple teams cross checking each other at all times and comparing to both physical prototypes and computational models.

They don't "screw up".
 

sevrent

New Member
Registered Member
It’s the other way around. The thrust will be fine. It’s the electrical system that needs a reliable generator. If you’re running two engines and there’s power drop off in one or both of them the plane will fly fine but the electrical output might get disrupted. You’re not likely to *lose* all electric power but for high output electrical systems especially losing output can disrupt system performance, sometimes when you need surge capacity. Distributing that load to three sources with one primary and two auxiliary helps resolve those kinds of situations.
3 engines are good for redundancy in case of failures, true. But wouldn't distributing the load evenly across three engines be better for reliability/redundancy? So as to minimize the impact of any disturbances in any one engine?
 

asif iqbal

Banned Idiot
There are reasonably serious Chinese PLA watchers out there who believe China is now ahead of the US in tailless aircraft design and control methods.

Until we see a tailless NGAD prototype or something along those lines flying, some of us might be inclined to agree with said PLA watchers.

Don’t think you need to be a PLA watcher

it’s pretty clear to everyone China has leaped frogged every 6th generation fighter project

and showing these kinds of manoeuvres so early on the development is clearly making a big statement

6th generation fighter shouldn’t be able to make these kinds of turns without traditional add ons unless you have a serious advantage and advancement in relevant technology
 
Top