According to the Liyang employee, the WS-10 initial variant (12.5 tonne thrust) received
recently, attaining development-termination status; that is, no more improvements can realistically be made on its design. Future production of that variant will be done according to the now-finalised specs and no modifications will need to be done to it thereafter. This entails the WS-10 variant that first flew in the early-2000s has now reached technological readiness level 9.
He knew this because Liming consulted with Liyang's experts on production certification. This is due to Liming's last production certification's being granted over forty years ago so that cohort has since retired, meaning the current Liming cohort has no experience with production certification. This contrasts to Liyang, which had concluded production certification in 2015 for the JL-9's engine so they have plenty of experience with production certification.
In answering further questions, he divulged additional info:
- J-10 family will not transition to this production-certified variant because of its higher bypass ratio compared to the AL-31 family which entails its having less consistent power output during flight at high altitudes or during vigorous manoeuvres. The J-10 series is increasing the electronics content of every successive iteration from the J-10 to 10A to 10B to 10C, so it's imperative that the engine does suffer unpredictable drops in power output as the electronics cannot function without a consistent power supply. The WS-10B, on the other hand, does have decent prospects of future wide-scale adoption on the J-10 series. The Sino-Flanker series can mount the production-certified WS-10 just fine because of their twin-engine design which means both engines supply power to the electronics basically guaranteeing that, even if the WS-10s suffer power output drops during high-G manoeuvres, there would still be enough power from the two engines for the electronics.
- The 2004 J-10 mounted with a WS-10A never reached design certification before being cancelled. However, valuable lessons were learnt from that experience.
- The WS-10B has received or is in the process of receiving design certification.
- The WS-15's nozzles are short and stubby, and comes with serrated edges. It'll be pretty obvious when a J-20 mounts them.
From another thread about the
AL-222-25 copy, there were these tidbits:
- The Minshan project was a technology demonstration project from the very start. Only 3-5 examples were made and underwent testing.
- One such example, when undergoing testing, had its turbine disk shatter which flung out debris in all directions, puncturing the casing and severing hydraulic tubes. This resulted in a fire which got put out by the automatic fire extinguisher. The example thus met its end like so.
- Chongqing Tianjiao Aerospace Propulsion Corporation, in cooperation with Ukraine's Motor Sich, competed with 624th Institute's AL-222-25 copy using the OG design. They ended up winning due to Motor Sich's willingness to contribute all its prior knowledge of the AL-222-25 series to the joint venture with Tianjiao as well as a prevailing expectation among industry and the PLAAF towards 624th that it should be conducting next-gen R&D - as it has the more talented aviation powerplant researchers - instead of spending their time reverse-engineering a low-thrust previous-gen design.
A few miscellaneous points from other threads that weren't as juicy:
- The WS-13E is intended for use on the FC-31 in lieu of a 4th-gen medium-thrust engine. The original WS-13 (RD-33) is already sufficient for use on the FC-31 but 624th wanted a practice project before beginning a full-scale next-gen medium-thrust project, so they went ahead with the WS-13E.
- The WS-13E has ~9 tonnes of thrust, with a TWR slightly lower than 8.
- It is at a similar level of readiness as the WS-10B; so almost received or have already received design certification.
- The WS-12 is the non-afterburning version of WS-13.
- 624th currently has two projects under its wings; the WS-500 500kg-thrust engine and the WS-13E. After completing development of these two, which is close, they will be progressing onto the next-gen medium-thrust engine (WS-19?), whose target thrust is slightly higher than the EJ200's.
- 青城 is project codeword for the WS-500, 黄龙 is the turbojet version of WS-500.
- The WZ-10 turboshaft has been flight-tested and initial deliveries are to begin this year for further evaluation. Looking forward to seeing this on the Z-20.
- The naval WS-10 is simply the WS-10 with additional anti-corrosion treatment.