Has WS-15 even entered service yet?Does anyone know if there is a next gen engine for the 6th gen fighter? Will it be an up-thrust version of WS-15 or a new design?
Go to the previous page thought not explicitly said so but the author has alluded progress has been made . The fact that WS10 is now mature and used in large number even in J10 seem to be the proof. They still struggling with WS 15 but that is another level and another mountain to climb seem like they get the prototype working but no production model sofarIts been a long while for me to dip back into this, but I am curious how far China has gotten in the turbine blade side of things. My technical knowledge is limited to RR circa 2004. Back then SRR99 was first gen, CMSX4 was regarded as the second generation single crystal material and RR3000 considered 3rd generation single crystal. RR3000 was for the EJ200, but on the table it said EJ200 uses 2nd generation single crystal alloy, so the generation reference is different between Chinese and Western?
How is the manufacturing process for the cooling vents in China? I remember we used water jets from tubes the size of hairs to make the vent holes in the blades, and some of the Chinese students would grab a few when they went through the factory tour. Have our processes caught up yet?
How is the Chinese coating method as well? We used EB/PVD for the MCrAlY bond coat and the thermal barrier coating back then. I noticed with things like thermal aluminum spray coating is still quite uncommon in China in other industrial application even in the last few years, so I wonder how is these coating process for Chinese aerospace?
Finally, since I am out of the loop for over a decade, what is the bleeding end now for the turbine material? Have we gone all ceramic matrix composite on single crystal oxide fiber? Is Niobium alloy a thing now i.e. did anyone resolve the oxidation problem on them? Or are we still dosing the nickel with Ruthenium and Rhenium? Also, I am curious to know how much these material costs now? Back then it was around 80-85 quid a kilo for bar stock of cmsx4 & rr3000
Here's what I know.Its been a long while for me to dip back into this, but I am curious how far China has gotten in the turbine blade side of things. My technical knowledge is limited to RR circa 2004. Back then SRR99 was first gen, CMSX4 was regarded as the second generation single crystal material and RR3000 considered 3rd generation single crystal. RR3000 was for the EJ200, but on the table it said EJ200 uses 2nd generation single crystal alloy, so the generation reference is different between Chinese and Western?
How is the manufacturing process for the cooling vents in China? I remember we used water jets from tubes the size of hairs to make the vent holes in the blades, and some of the Chinese students would grab a few when they went through the factory tour. Have our processes caught up yet?
How is the Chinese coating method as well? We used EB/PVD for the MCrAlY bond coat and the thermal barrier coating back then. I noticed with things like thermal aluminum spray coating is still quite uncommon in China in other industrial application even in the last few years, so I wonder how is these coating process for Chinese aerospace?
Finally, since I am out of the loop for over a decade, what is the bleeding end now for the turbine material? Have we gone all ceramic matrix composite on single crystal oxide fiber? Is Niobium alloy a thing now i.e. did anyone resolve the oxidation problem on them? Or are we still dosing the nickel with Ruthenium and Rhenium? Also, I am curious to know how much these material costs now? Back then it was around 80-85 quid a kilo for bar stock of cmsx4 & rr3000
Just to clarify, when you say 10-20 years gap, it doesn't mean that China will reach tech parity in 10-20 years right? So for example, if the WS-15 becomes fully operational then the gap is essentially fully narrowed right?Here's what I know.
Turbines for power generation.
China can make domestically F class Turbines (recent breakthrough). Dongfang Electric did that. There are other powerful manufacturers of turbines (Gas, Steam etc). Shanghai Electric is well-established.
Summary : 20 years gap in technology for electric generation industrial Gas turbines.
Mitsubishi J class leads with stunning efficiency.
Gas turbines for Marine Application
Mainly through Ukraine Zorya Mashproekt UGT-5000. China fully made it Indigenous and improved upon it to QC-280.
Comparison with Leader -
Few percentage points (3-4% points?) behind in Thermal Efficiency of leading Marine GTs of Rolls Royce in Queen Elizabeth but makes up with stellar power delivery.
Summary : 5-10 years behind? Only due to MT-30 RRoyce. I say it's a solid entry.
Aero-Engines
High Bypass
WS-20. Has started appearing on aircrafts. Don't know the technological level blwhen compared to foreign engines but should be comparable to Cfm engines that came before cfm LEAP.
CJ-1000A. Same level as CFM Leap or designed to compete with it. Product of Globalism and derives many subsystems from Global suppliers.
Summary : So, 20 years gap in technology. But ecosystem lags as there was no established supply chain or processes. So discussing a gap is not relevant.
Low Bypass
WS-10
A success story in the making. Had a troubling start with many issues but now seems to be entering in numbers.
Has many variants with wide ranging thrust figures ( After Burning :120 kN to 150 kN).
WS-15
The non Afterburning thrust or dry thrust of Chinese Engines never breaches the 100 kN ceiling. But WS-15 is an attempt to do that. The only engines that do that outside China are F119 and F135. The in-development Russian engine for Su-57 should also have dry thrust above 100 kN. It's important for supercruise (if weight isn't reduced).
Summary : 20+ years gap with the leading edge player (US).
No. The gap remains.Just to clarify, when you say 10-20 years gap, it doesn't mean that China will reach tech parity in 10-20 years right? So for example, if the WS-15 becomes fully operational then the gap is essentially fully narrowed right?
Hi thanks for the info! If I may ask, where do you think China currently stands in terms of engine tech with other major countries/blocs? Are they behind the EU in turbofan, etc?No. The gap remains.
Comprehensively speaking what exactly is the gap?
For example - say that US (through GE) is applying CMC in its engines in various places and adopting novel methods to cool it.
China may not be tackling the issues like US. They may use other methods. Some novel, some tried and tested.
Ultimately, we only can judge through specifications. Other numbers like MTBO, cost of production, maximum numbers in service etc are discounted here.
So the lead US has is mammoth. It can't be plugged. But China can catch up in some specification that help it to make aircrafts that can counter US tech. Ultimately, that's what important.
Note:I speak as an amateur. Take it for what it is. As far as I know, we don't have any detailed specifications for Chinese Engines.
The gap will be closed when China successfully delivers an Adaptative/Variable Cycle Engine at the same time as the US does. Those engines are the next big thing and are planned to be introduced on F-35 advanced variants or next generation fighter programs ( PCA, NGAD, etc...).
Does anything have been released through chinese media about studies on such technology ?