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Viewing 15 posts - 1,036 through 1,050 (of 1,105 total)
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  • in reply to: PLA (All Forces) Missiles #2042520
    Pinko
    Participant

    I think This One is the TV-command terminal guidance head for YJ63

    in reply to: PLA (All Forces) Missiles #2042532
    Pinko
    Participant

    Get the following from Sinodefense.com, only I think the engine for YJ63 is a small Turbofan instead of turbojet

    http://www.sinodefence.com/airforce/groundattack/h6.asp

    H-6H

    The H-6H bomber was developed in the 1990s to meet the PLAAF’s requirement for a new aerial platform that can launch ‘stand-off’ land-attack weapons outside the range of enemy’s air defence system, thus increasing the survivability of the bomber in modern air combat. The development of the H-6H began in January 1995, and the aircraft first flew in December 1998. The first successful missile fire test took place in November 2002. Currently two prototypes are undertaking various flight and system tests before the design can be finalised for batch production.

    Based on the design of the H-6D naval anti-ship missile carrier bomber, the H-6H carries two YJ-63 (also known as KD-63) LACMs on its under-wing hardpoints. The YJ-63 is a land-attack cruise missile (LACM) developed from the HY-4 (XW-41) anti-ship cruise missile. Powered by a small turbojet, the YJ-63 delivers a 500kg HE warhead over a distance of 200km at subsonic speed. While guided by inertial/GPS midcourse homing coupled with TV-command terminal guidance, the missile also receives target information via the bomber’s datalink antenna accommodated in the under-belly fairing behind the bomb bay doors. Like the H-6D, the H-6E is not equipped with any 23mm cannon.

    in reply to: PLA (All Forces) Missiles #2042799
    Pinko
    Participant

    That’s a DaMn*d a lot!! :diablo:

    in reply to: WS-10A: Current Status #2605698
    Pinko
    Participant

    As a matter of Fact, the blade manufacturer for WS10A –Guizhou xinyi is also manufacturing blades for Snecma CFM56s, It’s not the other way around:

    http://www.snecma-moteurs.com/en/presse/archives/cp310502.htm

    Alongside the successful operation by Chinese airlines of more than 700 CFM56 engines as well as numerous projects with the Chinese aviation industry, Snecma Moteurs has also established close subcontracting ties with 4 other plants over the past twelve years: Shenyang Liming Engine Manufacturing Corporation, Guizhou Xinyi Machinery Factory, Guizhou Liyang Aero-engine Corporation and Beijing Aero-Lever Plant.

    Snecma Moteurs praises the quality and on time delivery of the parts as well as the very competitive approach adopted by their Chinese partners and fully appreciates the continuous support provided by China Aero-Technology Import/Export Corporation and China Aviation Supplies Import/Export Corporation.

    In addition to the delivery of this 1000th turbine disk, large numbers of CFM56 parts have already been delivered by all the above-mentioned Chinese factories, in particular 50000 turbine blades and 1000 labyrinth rings, reflecting the tremendous success of the Snecma Moteurs relationship with the Chinese industry.

    http://www.zhtv.com/airshow/upload/2004_11/041106200354861.jpg

    in reply to: WS-10A: Current Status #2605699
    Pinko
    Participant

    So again, Your saying let people believe in that the Turbofan engine design and manufacturing is a simple “copycat” job. your production depends on the products for that production is “availble” in the market or not. You buy the “blade” in the market as “dual use product”, then the 2nd day you ” sure ” can produce it at home.

    Of course, for China, a new member of the exclusive turbofan engine club, the best way to catch up is to follow the mature and proven technologies. RE sometimes is the way to achieve that. To do a RE, you have to do 2 things, 1st, you need the physical product sample you want to RE, 2nd, you need your own effort to make your “copied” product up to the standard of the original. yo try to emphasis here is the 1st part is more important for a Re job done. However, as I and some othe mumber posted here already point out, the 2nd part, how to make your own REed product up to the standard is much more difficult and important than your” availablity of original product sample” theory. My previous post already said: “Most other countries got better access to those civil engines and relevant technologies as well as much wider choice of assistances from the well established western countries in designing such engines. However, why there are not so many F110-alikes everywhere? Because the complexity of making a turbofan engine still determines finally.”

    Your words are quite “confusion” at 1st place, never mind, let me look into what the 2nd possible meaning of your post so no argue at the end:

    If you say the WS10A going to use all ” imported” blades via the “dual use prodcut” channel, ( because China got enough CFM56s to claim the demand 😀 ). Then, you can ignore what I posted for the progress what China achieved in the area of Avaition materials technologies. but just use simple logic to judge yourself.

    Just ask some simple questions to yourself:

    1st: How many WS10A going to be produced?

    As a comparison, the demand for RD93 grade engine for FC-1 fighter alone is 500-600 as estimated by Russians. As the main stream Engine for PLAAF, Do you think the demand of WS10A is below 1000 units in future? Then again how many CFM56s does China have? can you import so many blades as replacement for “spoilt parts” of those CFM56s to fullfil the need of WS10A productions?

    2nd: Is the design of the CFM56 blades are the the same as those of WS10A? my references and what other ppl already posted show there’s different.

    You know who is viewing the WS10A blades

    in reply to: WS-10A: Current Status #2605787
    Pinko
    Participant

    Regarding the materials for WS10A’s complex internal cooling blades, it’s believed to be still Ni-based Directionally Solidified Superalloy Alloy DZ125/DZ125L –Though the more advanced DD3 ( Similar to US PWA1480) Single crystal Alloy is available.

    Regarding the new 10:1 t/w-ratio core engine of china’s next generation Turbofan, it will use the DD6 Single crystal Alloy blade as confirmed by a Chinese academic paper published back in 2002. According to the paper, the performance of the DD6 is comparable to the US 2nd Generation Single crystal Alloy PWA1484, the below image is a screen capture of the performance data of the DD6 Single crystal Alloy scanned from the academic paper:

    in reply to: WS-10A: Current Status #2605948
    Pinko
    Participant

    The CFM core engine delivers the technical layout. Even the blades for that core engine can be bought as replacement parts and those are high-tech parts too. You can trade the high lifetime of such blades against performance.

    As a matter of fact, China “borrowed” only 2 unit of CFM56 from US for evaluation during honeymoon period in 1980s when then USSR is their main concern. The 2 units of CFM56 were supposed to “return” to US once the evaluation period was over.
    However, 1 unit of the CFM56 was reported destroyed during a fire and never returned to US. So do you think US will supply the needed blades to Chinese? And China is stupid enough to rely on such “spare parts”? and don’t make such blades by themselves?

    in reply to: Pakistan test-fires first ground-launched cruise missile #2044267
    Pinko
    Participant

    Wow, No bad, now the PAF got another decent deterring means

    in reply to: WS-10A: Current Status #2606132
    Pinko
    Participant

    Nothing is wrong for China to start a Military grade turbofan from a civil engine. Most other countries got better access to those civil engines and relevant technologies as well as much wider choice of assistances from the well established western countries in designing such engines. However, why there are not so many F110-alikes everywhere? Because the complexity of making a turbofan engine still determines finally.

    in reply to: WS-10A: Current Status #2606324
    Pinko
    Participant

    How should I say…

    Thanks US and her great friendship towards China that helps China builds up the core of her military Aviation? 😉

    Hmm.. Just kidding..

    But still there’s something hard to copy, like the materials technology used for Turbofan engine, These all depend on China’s own development.

    Pinko
    Participant

    Wow, Great picture , And the following ships will be built in Singapore as well.

    BTW, is the 2 picutres showing the FFG doing sea trial or on the way back home( Singapore)?

    in reply to: WS-10A: Current Status #2606486
    Pinko
    Participant

    IMO, the 450 hours endurance test is not inclusive of the QT150h which bears similarities to the MIL-5007D but an all new ( compared to old 300h Kunlun test)TAC- based test procedure. See the picture below(Sorry, guys, AVic1’s news always in Chinese).

    1 thing interesting if according to the data table that Deino posted is the Total Pressure Ratio of WS-10A is over 30. similar to F110 and a lot of differences from AL31

    in reply to: WS-10A: Current Status #2606920
    Pinko
    Participant

    The information is openly available on the AVIC1’s official website( Of course it won’t call the engine directly as WS-10A)

    I think the initial AMT finished (450hrs Duration Test) at end of last month. No606 Institute tries to finalize the design by the end of this year. Maybe small batch production already started after the 450hrs Duration test(IMO). Formal production likely at beginning of the next year.

    in reply to: China's News, Pics and Speculation Part 8 #2606998
    Pinko
    Participant

    But how you know it’s J10B? Just because somebody used photoshop or somthing to add a caption?

    This’s a good example on how words just spreaded across the BBS rooms

    in reply to: China's News, Pics and Speculation Part 8 #2608026
    Pinko
    Participant

    Oh, Game over for SAC J8…

Viewing 15 posts - 1,036 through 1,050 (of 1,105 total)