J-20 5th Generation Fighter VII

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by78

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I said that I read these posts quite a while ago and therefore cannot provide the link. I'm pretty sure this is the third time I've said this already ... do you have a problem with reading comprehension (as in your own words)?

You may simply admit that you don't have any proof for your claim. Why is it so hard?
 

Blitzo

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I already answered your question in this post, which I made at 2:54 pm. And yet you kept insisting that there was no delay in the WS-15 ... which led to the next string of back and forths. Please read the bolded and italicized sentence I wrote.

I think we are reaching the crux of the issue.

Look, two basic yes/no questions to answer for yourself and for @by78 and then i hope we can wrap this whole episode up or else I'm going to put my moderator hat on again.

1: Do we all agree the timeline for WS-15 that we have publicly been told from the mid 2000s, has been moved right over the years? (Call it a delay, or call it the revised development schedule whatever -- point is, it has shifted to the right).

2: Do you think your sources are sufficient for the community to seriously entertain the idea that WS-15 has seen some sort of enhanced performance revision and that it is related to WS-15's delay/revised schedule/etc? Keep in mind this question is asked in the context of IMO the desire for the PLA watching community to want to be cautious about optimistic/ambitious engine projections.

I believe if these two questions can be answered by the two of you then you can at least reach a state of agreeing to disagree and we can move on from this.
 

Figaro

Senior Member
Registered Member
You may simply admit that you don't have any proof for your claim. Why is it so hard?
I literally addressed this in two previous posts and for some reason you are now just catching on? Why is it so hard?

No I wasn't. The WS-10 is a different engine than the WS-15 so why would I be mixing up those two? Please don't falsely speculate on my behalf. The
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of the WS-15, as described by a well known big shrimp "Maya" was an engine in the 150 kN class (along with using 2nd gen DD6 single crystal superalloy, FGH 96 P/M superalloy), roughly analogous to the F119. Then starting around the early 2010s, there were reports of the WS-15 being an
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instead and the WS-15 was even listed as an 180 kN engine in the AVIC organized "
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" Obviously, these figures are quite a step up from the original 150 kN class design goal as stated by Maya. Unfortunately, I could not find the specific CJDBY threads detailing this revision since it was quite some time ago but you're more than fine to go search for this yourself. If anything, I'm surprised as to why you find a WS-15 design revision to be shocking. Since then, 3rd generation DD9 and DD10 single crystal superalloys have come out, not to mention the FGH-98 P/M disk, all of which offer substantial material performance upgrade over the original WS-15 materials. It is very plausible for 606 to take advantage of this and alter the design to include these materials rather than coming out with a quarter century old F119 class engine, as the original specs entailed.

Regarding the delay, Maya said it would take about 10 years for the WS-15 to enter mass production after testing its core at high altitude in late 2009. I hope you can agree that the WS-15 is not nearly in mass production stage yet right? As I've said before, I highly recommend you read through the 545 page engine thread. Perhaps it can enlighten you a bit on the Chinese aeroengine development :p.
Now now we don't have to resort to personal insults like "memory problems." I have kept this discussion cordial and I expect the same of you. Note in my previous post I did said the following : "I could not find the specific CJDBY threads detailing this revision since it was quite some time ago but you're more than fine to go search for this yourself." I told you I read them some time ago and hence unfortunately cannot provide you the specific links. As I said, you're more than welcome to spend the time to look them up for yourself.

I really don't know why you have such a difficult time comprehending this Maya clearly mentioned that the WS-15 was expected to enter service about tens years after the completion of its high altitude testing. I do not need to refer to a five year plan or anything ... it is pretty clear by what Maya meant that if the WS-15 was on schedule, J-20s would have already been equipped with them, which is simply not the case. Earlier you said you had never heard of any delays with the WS-15 program, which is why I brought up Maya's quote. It seems that you have a hard time understanding what exactly you're arguing about, not me. Do you seriously need to be presented with a classified official timeline of the WS-15 to be convinced the program is behind schedule?

Also out of consideration for not derailing this thread any further, I am willing to settle this discussion via pm.
 

by78

General
I think we are reaching the crux of the issue.

Look, two basic yes/no questions to answer for yourself and for @by78 and then i hope we can wrap this whole episode up or else I'm going to put my moderator hat on again.

1: Do we all agree the timeline for WS-15 that we have publicly been told from the mid 2000s, has been moved right over the years? (Call it a delay, or call it the revised development schedule whatever -- point is, it has shifted to the right).

2: Do you think your sources are sufficient for the community to seriously entertain the idea that WS-15 has seen some sort of enhanced performance revision and that it is related to WS-15's delay/revised schedule/etc? Keep in mind this question is asked in the context of IMO the desire for the PLA watching community to want to be cautious about optimistic/ambitious engine projections.

I believe if these two questions can be answered by the two of you then you can at least reach a state of agreeing to disagree and we can move on from this.

I agree there has been "shifts to the right", compared to the very early and therefore tentative projections, but it's quite a stretch to say these are delays, IMO.

So yeah, shifts to the right is the right way of putting it, no pun intended.
 
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by78

General
I literally addressed this in two previous posts and for some reason you are now just catching on? Why is it so hard?

So you claim to have proof but you really don't. Is that what you are saying?

Can we and should we trust you that you have indeed read what you profess to have read?
 

by78

General
J-20 has received a Gold Design Patent Award. The second image is the design patent in question.

50124601087_bf342df0a0_b.jpg


50124377666_a064af9016_o.jpg
 

latenlazy

Brigadier
The
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were 18 tonnes of thrust. As for the 197 kN claim, the only place I saw something similar to that was in the paper of the WS-15 core's chief designer Jiang Hefu. I think it is referring to the theoretical maximum thrust of the WS-15 core, most likely using the core for a large bypass ratio engine. But since the WS-15 itself is a low bypass engine, I doubt the 197 kN or 200 kN claim is credible.

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Hey Figaro, it seems you’ve been doing your share of diving through a lot of academic articles. Do you have an collection of them that you can share? I think it might make sense to create an archive of these things so we have a clearer view on the state of research and development for a lot of these technologies.
 

Figaro

Senior Member
Registered Member
Hey Figaro, it seems you’ve been doing your share of diving through a lot of academic articles. Do you have an collection of them that you can share? I think it might make sense to create an archive of these things so we have a clearer view on the state of research and development for a lot of these technologies.
Sure. I'll dig through some of the academic articles I've read on Chinese aeroengine development and if they're of significance, I'll post them in the engine thread.
 
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Blitzo

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Okay, @by78 and @Figaro, I've deleted a number of your more recent posts from both of you.

Sometimes people can get worked up over disputes and debates over minor points of contention, but that is no reason to make personal attacks or to be unable to engage in good faith discussions.

This particular strain of discussion has gone on long enough, and I'm drawing a line here now.

Any further discussions or debates on this matter will be deleted in this thread, and I also expect that if there are any personal grudges that you may have had because of this particular exchange will not cause needless provocation and personal remarks in other threads as well.
Failure to abide to the above will result in formal warnings and eventually temporary bans as well.


===

I would also add that on SDF we do seek to avoid "fanboy" type posts -- and we do have some new members whose posts may be described as such.
However if there is someone you believe is exhibiting those behaviours, it is poor form to deride them as fanboys. There are more constructive and polite ways to inform them of those type of posts and to encourage change rather than using degrading remarks that could be construed as personal attacks.
 
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