PRC VCE and low bypass engines (fighters, tactical jets, UAVs, others)

00CuriousObserver

Senior Member
Registered Member
Moderator edit:
Old thread here:


Thread for high bypass engines, turboprops, tubroshafts here:



==

Hehe

(I remember there was a VCE thread but I can't seem to find it) or maybe not

6EqlqYe.png

8153qpj.png


This application belongs to the technical field of aircraft engine design, and specifically relates to a three-duct variable-cycle aircraft engine.

A third duct is added between the inner duct and the outer duct, and a diversion fan is added behind the main fan. The diversion fan further includes:

a first-stage diversion fan

a second-stage diversion fan

The first-stage diversion fan is located inside the inlet of the third duct, in front of the inner duct.

The second-stage diversion fan is located inside the inlet of the inner duct.

The first-stage and second-stage diversion fans are connected by a drum/casing.

The second-stage diversion fan is connected to the front end of the low-pressure shaft through a diversion-fan shaft.

A variable-speed gearbox is connected inside the front end of the low-pressure shaft, and the output shaft of the variable-speed gearbox is connected to the fan through a fan shaft.
CN116163854A, “Method for Controlling Mode Switching of a Dual-Bypass Compressor in a Variable-Cycle Aircraft Engine”

Publication date: 2023-05-26

Application date: 2023-02-20

Category:
Combustion engines, engine installations using hot gas or combustion products

Invention title:
Method for Controlling Mode Switching of a Dual-Bypass Compressor in a Variable-Cycle Aircraft Engine
 
Last edited by a moderator:

Blitzo

General
Staff member
Super Moderator
Registered Member
Old thread here:


Thread for high bypass engines, turboprops, tubroshafts here:



The reason for this delineation in engine topics is because a bulk of the previous engine thread's discussions revolved around low bypass engines/engines for fighter aircraft, which understandably is a major focus and source of major interest.

This thread will be primarily for those types of engines, a list of examples but not exhaustive including:
- WS-10, WS-15, WS-13, WS-21, WS-19, WS-9, etc...
- VCE/ACE efforts for future fighters
- Engines for various trainers
- Likely engines for H-20 and GJ-X and WZ-X etc

If you're wondering if an engine is "high bypass" or "low bypass," I advise to just use some common sense. If something looks like it'll fit on a modern airliner, then it's probably high bypass.
 
Last edited:

Alfa_Particle

Senior Member
Registered Member
Moderator edit:
Old thread here:


Thread for high bypass engines, turboprops, tubroshafts here:



==

Hehe

(I remember there was a VCE thread but I can't seem to find it) or maybe not

6EqlqYe.png

8153qpj.png
They're putting GTF tech in ACEs? Fun.
 

Alfa_Particle

Senior Member
Registered Member
Moderator edit:
Old thread here:


Thread for high bypass engines, turboprops, tubroshafts here:



==

Hehe

(I remember there was a VCE thread but I can't seem to find it) or maybe not

6EqlqYe.png

8153qpj.png
And here I was wondering what 606 projects that would ever need a GTF mechanism (great dig by @sunnymaxi), guess we found the culprit:
20260315_211445.jpg
 

ACuriousPLAFan

Lieutenant General
Registered Member
Moderator edit:
Old thread here:


Thread for high bypass engines, turboprops, tubroshafts here:



==

Hehe

(I remember there was a VCE thread but I can't seem to find it) or maybe not

6EqlqYe.png

8153qpj.png

Another one, likely from the same patent document(s).

vcepatent16032026.png
 

Alfa_Particle

Senior Member
Registered Member
Another one, likely from the same patent document(s).

View attachment 171645
This is what I originally envisioned their ACE would be, yeah:
Screenshot_20260315_211916_org_mozilla_firefox_HomeActivity.jpg

With the GTF one they're taking a special approach of having a geared fan then two diverting fans, one nested in the HPC duct and the other where the CDFS would usually be. I guess we'll see eventually what kinda novel architecture they'll settle on.

Edit: hold on I completed skimmed over an extremely important detail. The CDFS here has adjustable blades?? Whoa. That's also quite neat.

Edit #2: this design with the VCDFS has one of the patentnees listed as 刘永泉... Something to note.
 
Last edited:

Alfa_Particle

Senior Member
Registered Member
While we've talked about this before, I don't believe anyone has posted this yet. Here's a radar + IR blocker integrated afterburner, one of the patentnees being the very chief engineer of the WS-15, dating back to 2021. I think this should give a very solid (but of course, not concrete) answer to the "does the WS-15 actually have a radar blocker?" question (I personally find it silly that this is even a question in the first place):
Screenshot_20260316_024924_org_mozilla_firefox_HomeActivity_edit_802727684652374.jpgScreenshot_20260316_024950_org_mozilla_firefox_HomeActivity_edit_802753063630333.jpgScreenshot_20260316_024954_org_mozilla_firefox_HomeActivity_edit_802766962351786.jpgScreenshot_20260316_024958_org_mozilla_firefox_HomeActivity_edit_802777874195949.jpgScreenshot_20260316_025006_org_mozilla_firefox_HomeActivity_edit_802803340835627.jpgScreenshot_20260316_025002_org_mozilla_firefox_HomeActivity_edit_802810652949374.jpgScreenshot_20260316_025012_org_mozilla_firefox_HomeActivity_edit_802831871653220.jpgScreenshot_20260316_025018_org_mozilla_firefox_HomeActivity_edit_802844205278580.jpg
 
Top