Chinese Engine Development

montyp165

Senior Member
I for one don't consider the reliability issue to be the primary factor for aircraft placement insomuch as the conceptual differences between the WS-10 and the AL-31 resembles that of the F110 vs F100 engines in the USAF.
 

johnqh

Junior Member
Umm. It's either reliable or unreliable. If they don't trust the engines reliability then clearly that means there are still quality issues.

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I have been following China's military and watching this site for years. I think I know what I am talking about. There is never just one prototype when a new aircraft is developed, there will be at least 3 J-15 prototypes built. As of right now, China has no aircraft carrier, so to test takeoff and landing...this will be done on land. Therefore, there is no reason at all that WS-10 cannot be used. There is no risk of "corrosion" (not sure if I buy that argument in the first place) that would require a redesign of the WS-10 to WS-10H level. The first J-15 prototype will probably never see the Varyag.



First of all, we're not talking about the "first couple of years." The WS-10 was certified in early 2006. They have had 5 years to ramp up production. And trust me, SAC would find some WS-10s for J-15 testing. Testing the J-15 with AL-31F is a disadvantage for them because the final design will presumably use WS-10. The WS-10 has different weight, aerodynamic, fuel, and intake requirements. In other words, the J-15 will have to go through a lot more testing using WS-10 later on. SAC would be using WS-10 from the start if they could.



I never said they were enemies. But from SACs perspective, they lost the 5th generation fighter competition, and the least that they could have contributed was their engine they had been working on for 24 years. Instead CAC chose AL-31F. There is a reason they chose it, it has nothing to do with production quantity or performance. It has to be reliability. The same reason CAC did not want to risk putting an immature engine on the J-20 is the same reason they refuse to put it on the J-10. The engine is not as reliable as they would like.


Again (am I repeating myself?)

J-20 project is at least 10 years old. Even if you must argue it is 5 years old, WS-10A was not in production in 2005. Even if you say it was 3 years old, WS-10A was not used in any fighters in PLAAF 3 in 2007. Not for quality issue, but for slow "spool-up" time. (It takes twice as long to spin up as AL-31F).

Regarding J-15, there is NO POINT in spending the time and money on one with WS-10A because anyone with any little bit of clue would know WS-10A cannot be used for J-15 production for years. You want them to do it just for fun?

The only way that your argument makes any sense is if you believe it takes five months to design J-20.

Who knows, maybe you are right. Maybe the Chinese designers are so incredible. Maybe you are an aircraft designer that you know how to design a 4G fighter in months.
 

dingyibvs

Senior Member
Umm. It's either reliable or unreliable. If they don't trust the engines reliability then clearly that means there are still quality issues.

No, those two don't follow, and I'm not sure why you're not getting this. Not knowing if something's reliable doesn't mean that it's unreliable. It's very possible that the WS-10 hasn't been installed in enough numbers for a long enough period of time for the PLA to know its availability before constructing the J-20 prototype.
 

montyp165

Senior Member
The reason for the delay from certification in 2006 to production in 2009 is due to quality, not neccessarily slow spool-up times. This forum has repeatedly shown that the delay was due to an inability to mass produce the engine with satisfactory quality. Slow spool up times may (among other things) have been a problem but it wasn't the major thing holding it back.

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Why can't WS-10 be used on J-15. It has been used on J-11BS and J-11B...both very similar aircraft. If you are arguing that they are waiting for WS-10H which is "corrosion resistant," that argument doesn't hold water. First, as I said before, the J-15 needs years of flight testing...and China has no aircraft carrier which means for the time being will be tested on land just like any J-11BS or J-11B. Second, the whole corrosion argument doesn't make sense for two reasons:

If the WS-10 couldn't operate near water than why is it being used on naval J-11BS and J-11Bs. Those aircraft are being delivered to the PLAN and will operate primarily over water...no engine redesign needed.

Second, the Russian Su-33 uses regular AL-31F engines, there was no need to "corrosion" proof and delay the project redesigning the engines.

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If you are arguing that there simply isn't enough WS-10s being produced, I think that is highly unlikely:

First, there have been no AL-31F ordered in years, if anything...THEY are in shorter supply.

Second, as I said before, it makes no sense to test and aircraft with a different engine than it will use in combat...unless there is a reason that they can't. Which is this case is clearly NOT do to corrosion concerns, or availability. It has to be quality issues or concerns. I'll even give you that maybe it's not powerful enough to get the plane off the aircraft carrier...but corrosion it is not.



Let's tone it down a bit. I am just being constructive and thinking this thing through in detail.

There is a reason the WS10 is not installed on the J-10B. Do you think China wan't to continue buying AL-31FNs from Russia? It is because the J-10A/B are single engined...if the engine goes out the plane is lost. The quality control methods have to be higher and CAC is still not confident with WS-10.



I don't quite understand your sentence. You talk of both reliability and availability. Let's assume you are right, the WS-10 is reliable, why not put it on J-10, J-15, and J-20? I mean, it's indigenous, it's a matter of national pride, and the AL-31Fs are in short supply. There is no reason not to install WS-10 UNLESS they still had some doubts that it would fail in flight.

Note: Of China's recent aircraft, J-11B, J-15, J-11BS, J-10B, and J-20, ALL of them should have and could have had WS-10s from the start, but only one aircraft used WS-10 on its prototype....the J-11BS. Check huitong's site...it was rumored that a J-11BS crashed in 09. Due to engine failure maybe? Seems odd that the only prototype that crashed is the only one fitted with WS-10s.


This is the last I will write on the subject. All I am saying that there is something wrong with WS-10, something bad enough where they will only use it when they have no other choice. I joined this forum years ago and I pointed out that the J-11B wasn't using WS-10 back then, I got ridiculed because "WS-10 was certified years before" but I turned out to be right.

There are quite a number of questionable assertions here, but I don't have the time right now to explain things. Suffice it to say, too many POVs with too little (or even biased) sources running around to make these sorts of firm conclusions.
 

dingyibvs

Senior Member
I don't quite understand your sentence. You talk of both reliability and availability. Let's assume you are right, the WS-10 is reliable, why not put it on J-10, J-15, and J-20? I mean, it's indigenous, it's a matter of national pride, and the AL-31Fs are in short supply. There is no reason not to install WS-10 UNLESS they still had some doubts that it would fail in flight.

Note: Of China's recent aircraft, J-11B, J-15, J-11BS, J-10B, and J-20, ALL of them should have and could have had WS-10s from the start, but only one aircraft used WS-10 on its prototype....the J-11BS. Check huitong's site...it was rumored that a J-11BS crashed in 09. Due to engine failure maybe? Seems odd that the only prototype that crashed is the only one fitted with WS-10s.


This is the last I will write on the subject. All I am saying that there is something wrong with WS-10, something bad enough where they will only use it when they have no other choice. I joined this forum years ago and I pointed out that the J-11B wasn't using WS-10 back then, I got ridiculed because "WS-10 was certified years before" but I turned out to be right.

Well, let's use an analogy. If you're running a company and you hired a new guy fresh out of college, would you trust his reliability? No. Because there's nothing to confirm that he is. However, just because nothing confirms that he's reliable doesn't mean that he's unreliable either, or else every single fresh graduate would be labeled unreliable by this standard. The solution to this problem would be to treat everyone as unreliable, especially when the project is important, until he proves his reliability.
 

johnqh

Junior Member
The reason for the delay from certification in 2006 to production in 2009 is due to quality, not neccessarily slow spool-up times. This forum has repeatedly shown that the delay was due to an inability to mass produce the engine with satisfactory quality. Slow spool up times may (among other things) have been a problem but it wasn't the major thing holding it back.

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Why can't WS-10 be used on J-15. It has been used on J-11BS and J-11B...both very similar aircraft. If you are arguing that they are waiting for WS-10H which is "corrosion resistant," that argument doesn't hold water. First, as I said before, the J-15 needs years of flight testing...and China has no aircraft carrier which means for the time being will be tested on land just like any J-11BS or J-11B. Second, the whole corrosion argument doesn't make sense for two reasons:

If the WS-10 couldn't operate near water than why is it being used on naval J-11BS and J-11Bs. Those aircraft are being delivered to the PLAN and will operate primarily over water...no engine redesign needed.

Second, the Russian Su-33 uses regular AL-31F engines, there was no need to "corrosion" proof and delay the project redesigning the engines.

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If you are arguing that there simply isn't enough WS-10s being produced, I think that is highly unlikely:

First, there have been no AL-31F ordered in years, if anything...THEY are in shorter supply.

Second, as I said before, it makes no sense to test and aircraft with a different engine than it will use in combat...unless there is a reason that they can't. Which is this case is clearly NOT do to corrosion concerns, or availability. It has to be quality issues or concerns. I'll even give you that maybe it's not powerful enough to get the plane off the aircraft carrier...but corrosion it is not.



Let's tone it down a bit. I am just being constructive and thinking this thing through in detail.

There is a reason the WS10 is not installed on the J-10B. Do you think China wan't to continue buying AL-31FNs from Russia? It is because the J-10A/B are single engined...if the engine goes out the plane is lost. The quality control methods have to be higher and CAC is still not confident with WS-10.



I don't quite understand your sentence. You talk of both reliability and availability. Let's assume you are right, the WS-10 is reliable, why not put it on J-10, J-15, and J-20? I mean, it's indigenous, it's a matter of national pride, and the AL-31Fs are in short supply. There is no reason not to install WS-10 UNLESS they still had some doubts that it would fail in flight.

Note: Of China's recent aircraft, J-11B, J-15, J-11BS, J-10B, and J-20, ALL of them should have and could have had WS-10s from the start, but only one aircraft used WS-10 on its prototype....the J-11BS. Check huitong's site...it was rumored that a J-11BS crashed in 09. Due to engine failure maybe? Seems odd that the only prototype that crashed is the only one fitted with WS-10s.


This is the last I will write on the subject. All I am saying that there is something wrong with WS-10, something bad enough where they will only use it when they have no other choice. I joined this forum years ago and I pointed out that the J-11B wasn't using WS-10 back then, I got ridiculed because "WS-10 was certified years before" but I turned out to be right.

You have no background in engineering and manufacturing, do you?

1. Certification happens when the engine satisfies the design requirement. That does not mean the engine was ready for production.
2. Certification doesn't even mean the engine is ready for integration. That requires additional design and testing. In this case, problems were found that about spool-up time.
3. Only once all the bugs were figured out, the engine goes into manufacturing.
4. An engine which performs well during the design stage does not mean it can be easily manufactured. WS-9 (which Chinese bought the right) took YEARS before it can be manufactured reliably. It was so bad that China had to buy refurbished Spray for JH-7. So it is bound that problems will be found during the initial years of manufacturing. That's why the initial production rate is low.

Finally, have you ever lived (and driven a car) close to the beach? Or lived (and driven a car) in a city which snow a lot during the winter and use salt to clean the roads? The erosion is incredible. It takes years from the usable life of the car.

And operating land-based aircraft is not the same from operating on a carrier. Nobody builds airport next to the water. However, on the carrier, you will get mist of salt water.

AL-31F doing fine on the carrier does not mean WS-10A will do fine. Remember the Russian standard on maintenance is only few hundred hours. The requirement for WS-10A was much higher.

Finally, since you are such a big fan for CAC (I am a fan for CAC too but I am much more realistic). Have you see the cockpit photo of J-10? It is ancient comparing to JF-17. JF-17 was flying six years ago. Why couldn't CAC come up with J-10B in 2006 with the updated cockpit? Well, that's the life in aircraft development. I am sure J-10B program started ground 2006, and it took them five year to get to first flight.

So, assuming WS-10A fixed the spool-up problem in 2008/2009 timeframe, we will not see it used in any new projects (other than J-11B, which has been testing WS-10A since ~05/06) until 2015.
 

Centrist

Junior Member
. Certification happens when the engine satisfies the design requirement. That does not mean the engine was ready for production.
2. Certification doesn't even mean the engine is ready for integration. That requires additional design and testing. In this case, problems were found that about spool-up time.
3. Only once all the bugs were figured out, the engine goes into manufacturing.
4. An engine which performs well during the design stage does not mean it can be easily manufactured. WS-9 (which Chinese bought the right) took YEARS before it can be manufactured reliably. It was so bad that China had to buy refurbished Spray for JH-7. So it is bound that problems will be found during the initial years of manufacturing. That's why the initial production rate is low.

What are you credentials with regard to engineering? Have you been involved with military jet engine development before?

That is what I have been saying, but you previously denied that the WS-10 has quality issues. You said that the reason it was held up was due to spool-up times. I am saying that quality control has been the bigger problem.

Finally, have you ever lived (and driven a car) close to the beach? Or lived (and driven a car) in a city which snow a lot during the winter and use salt to clean the roads? The erosion is incredible. It takes years from the usable life of the car.

And operating land-based aircraft is not the same from operating on a carrier. Nobody builds airport next to the water. However, on the carrier, you will get mist of salt water.

I still don't buy it, an aircraft engine is going to corrode or not corrode, just because it is Russian doesn't automatically make it resistant to sea salt. Your argument makes no sense. What you are saying is that SAC engineers decided not to test the J-15 with the engine that it would use in production because it would corrode the engines. So instead, they decided to go with the AL-31F...and engine which...is also unprotected and not designed to handle sea salt. The AL-31F is just a regular engine, it has no special modification that make it corrosion resistant. But I'll even give it to you.

It makes no difference anyway. The J-15 is, and will be for the next few years, tested on LAND. There is no reason to use AL-31s.


Well, that's the life in aircraft development. I am sure J-10B program started ground 2006, and it took them five year to get to first flight.

I am well aware that these things take a long time to develop, perhaps better than you. You said the J-10B project began in 2006 and it took five years for the first flight. The J-10B flew in 2009, check it. That is three years...not five.

I am being very realistic. I am not some huge CAC fanboy either, I am just looking at the facts.

You keep telling me that I am wrong but you are not inadequately explaining why the PLAAF is so hesitant to use WS-10s.

The J-11BS prototypes used WS-10, but the J-15s prototypes have not. Why? The J-11BS flew years before the latter, the engine was more mature by the time the J-15 came around.

The J-15 prototypes aren't seeing any water or any corrosion. They could be fitted with WS-10s just as the J-11BS was years EARLIER. Why are they not? You still haven't explained this. Huitong suggests that a J-11BS crashed, maybe the crash caused SAC to rethink putting an immature engine on future prototypes (hence the J-15 and J-20 were stuck with AL-31Fs). SAC is going to use WS-10 engines on the prototypes if they can because ultimately the J-15 is going to be powered by them. It doesn't make sense to test and aircraft with a different engine, and then go back and repeat some of the testing again with the final engine. The fact that SAC did not use WS-10 on the J-15 is telling.

The J-20 is in not threat of corrosion either. The J-11BS flew with WS-10s 3-4 years before the J-20. My argument still applies as it does with the J-15. There is a reason that these engines are not being used.

That reason is not supply. They will make sure there are enough engines for testing aircraft, aside from the fact that AL-31Fs are not being ordered or produced anymore, and therefore are in shorter supply.

It is not spool-up times because the J-20 and J-15s don't require faster spool up times for now. Besides, they wouldn't be using the WS-10 engines on J-11B or J-11BS if their performance was all that bad. If it can power a combat ready J-11B it can power a J-15 or a J-20 prototype.

It is not corrosion resistance.

It can only be concerns with quality. That's it.
 

ReneDad

New Member
It's either reliable or unreliable..

It depends on how the Chinese would use the engines.

For example:

Boeing's 787 is planned to be reliable in 2014.....for common passengers like you and me...

But it will not be considered as a reliable plane for important passengers like Obama and Arabian kings by then.

A prototype is more important than a mass produced plane just as a president is more important than a common passenger. If the prototype crashes, the whole project will be delayed for several months to several years. Some Chinese fanboys said SAC once used newly-developed WP-14 on their J-8C prototype in 1990s. After the protoptype crashed due to the engine failure, the project was delayed and cancelled at last.

AL-31 was used on prototypes of J-15 and J-20 because it had been in service for over 20 years so it was considered as a more reliable engine than Taihang, which was reportedly in service in 2007(?).

In engineering, reliability is given by the form of decimal fraction, like 0.9 or 0.999, so there isn't a reliable engine or an unreliable engine but a more reliable engine and a less reliable engine. A F110-GE-100 may be more reliable than an AL-31F, and AL-31F is more reliable than WS-10, so the Chinese would use F110 to power their prototype J-15 for it was more reliable if they could get some. But they will use Taihang to power the mass produced planes just because America is less reliable.;)
 
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