{"id":110940,"date":"2017-11-30T11:50:00","date_gmt":"2017-11-30T11:50:00","guid":{"rendered":""},"modified":"2023-01-08T11:05:28","modified_gmt":"2023-01-08T11:05:28","slug":"aerospace-engine-situation-with-big","status":"publish","type":"post","link":"https:\/\/cvnextjob.com\/index.php\/2017\/11\/30\/aerospace-engine-situation-with-big\/","title":{"rendered":"Aerospace Engine situation with the big transport"},"content":{"rendered":"<div style=\"margin-top: 0px; margin-bottom: 0px;\" class=\"sharethis-inline-share-buttons\" ><\/div><h3 class=\"post-title entry-title\" itemprop=\"name\"><\/h3>\n<div class=\"post-header\"> <\/div>\n<p>As you guys all know, the biggest problem that PLAAF have always had is  the lack of high performing engine series.  J-10 still relies on  AL-31FN.  We didn&#8217;t see any new J-10s for a while, because they used up  all of the AL-31FNs.  J-11B used WS-10A for a while, but had so much  problems that many of them are also using AL-31F.  H-6K project was  basically stopped, because the suspension of the contract for 240  D-30KP2.  J-10 and H-6K production basically only restarted recently  because China started to purchase engines from the Russians again.   Similarly, the L-15 project has been delayed and Z-10 project has been  delayed.  Of all the project, I think the one that is the most important  for PLAAF and has suffered the most is the large transport project.   It&#8217;s quite apparent that PLAAF needs something in the class of D-30KP2  to equip not only the large transport but also H-6K, newer variants of  H-6 and possible future bomber projects.  We all know about the  tremendous need for large transport in PLAAF.  They basically can&#8217;t  build newer KJ-2000 units, because they are running so low on IL-76  airframes.<\/p>\n<p>Having said all of this.  It appears that the  prototypes and first batch of the large transport will be using D-30KP2  or the domestic version WS-18.  WS-18 is being produced by ChengFa group  (<a href=\"http:\/\/www.cftrt.com\/chinese\/index.php\">Website<\/a>).   Chengdu engine group (aka Factory 420) is also tasked with license  production of L-15&#8217;s engine AI-222-25F.  People will ask why they are  depending on something so old (China has had access to it since the 80s  when they imported Tu-154).  The truth is that PLAAF just needs  something that works.  D-30KP3 at this point is still not ready for mass  production, so they have to go with KP2.  PS-90A is a possibility, but  PLAAF is going for the cheaper option for purchase and license  production (or possibly unlicensed production).  Therefore, WS-18 is  pretty much just going to be the domestic version of D-30KP2, although  maybe slightly improved in fuel efficiency and such.  This engine was  said to have had its first flight in January of 2007, so it should be  ready for the large transport when it makes its first flight in 2012.   It will probably ready even earlier for H-6K, H-6U and other variants of  H-6.<\/p>\n<p>On top of WS-18, there is also a high bypass turbofan  engine under development with its core based on WS-10A.  It will  eventually be the engine used to power the large transport.  I think a  variant of it will probably also be pitched as the engine for C919.   Now, we all thought that Shenyang Liming (606 Institute) was going to be  developing it, but we found out recently that the work has been given  to Xi&#8217;an AeroEngine (410 Institute).  In many ways, it does make sense  for XAEC to develop\/produce this engine, because Xi&#8217;an is also the home  of XAC\/SAC, which is in charge the large transport project.  However,  Shenyang Liming is the developer of WS-10A and follow-up variants, so  it&#8217;s unusual for the large bypass variant of the engine to be given to  someone else.  At this point, Liming still has WP-14 Kunlun series,  WS-10A Taihang series, a bunch of domestic gas turbines (QC-70, QC-128,  QC-168, QC-185 and QC-260).  We all know about the troubles in the  WS-10A, but I&#8217;ve read that the Kunlun series also have had a lot of  problems. Amongst all the major gas turbine projects, only QC-70 and  QC-128 are ready for production.  XAEC is now working on WS-9, WS-15,  1\/3 of the production work for WS-10A, the large bypass turbofan engine  for large transport and most of the production for QC-280.  As the  result of this, XAEC will be responsible for the future power plant of  JH-7A, 5th gen fighter, large transport\/special mission aircraft and  major warships and also be very instrumental in the power plant of J-10  and J-11.  A few years ago, it seemed that Liming was becoming the  dominant engine maker in China due to its role in Kunlun and Taihang  series, which were the 2 most important aerospace engine projects at  that time (and possibly still are).  However, due to its failure in  those 2 projects and delays in the gas turbine projects, it has really  lost out to XAEC, which performed well with WS-9 and QC-280.  I think  the shift of this extremely high profile project is a sign that PLA is  really unhappy with Liming.<\/p>\n<p>Anyhow, there is a really good  article written by SAERI (Shenyang AeroEngine Research Institute).  It  talks about the 2 engine possibilities (WS-18 and the one based on  WS-10) that could be used to power a domestic large transport.  The  engines are designed to be comparable to D-30KP2 in size\/dimension.   China has two previous attempts at medium to large turbofan engine.   WS-5 from the 60s had a bypass ratio of 1.49 and WS-6 had a bypass ratio  of 1.85.  Comparatively speaking, D-30KP2 has a bypass ratio of 2.42  while a modern airliner engine like CFM-56-5A has a ratio of 6 and  PS-90A has a ratio of 4.6.  In this article, SAERI put out to proposals:<\/p>\n<ol>\n<li>WS-Y1  (I guess WS-18 here) that has the same dimension as D-30KP2, with the  same thrust, but slight improvement in the bypass ratio<\/li>\n<li>WS-Y2  (the one based on WS-10) that has slightly different ratio, with the  same thrust, but bigger improvement in the bypass ratio<\/li>\n<\/ol>\n<p>In  the analysis, they believe that the air consumption of Y1 would be 285  kg\/s and of Y2 would be 380 kg\/s.  That will produce bypass ratio of  around 3 for Y1 and 5 to 6 for Y2.  The fan diameter of Y1 would be  1460mm like it is for D-30KP2 and 1700 mm for Y2.  The thrust at takeoff  mode would be the same for Y1 and Y2 as it is for D-30KP2 (12000 kgf).   At an altitude of 11000 m and speed of mach 0.8, the fuel consumption  rates would be 0.67-0.68 for Y1 and 0.6-0.62 for Y2 compared to 0.7 for  D-30KP2 and 0.595 for PS-90A.  And the takeoff fuel consumption rates  would be 0.45-0.48 for Y1 and 0.35-0.38 for Y2 compared to 0.51 for  D-30KP2.<\/p>\n<p>Unfortunately, it&#8217;s hard to verify how close these  figures would be to the engines that get developed.  However, due to the  fact that this was written by SAERI which basically developed the  engines that are now being produced by Shenyang Liming, I think the  published numbers should not be that far from the truth.  It looks like  they have achieved much better fuel consumption numbers than D-30KP2,  but still trails PS-90A and obviously the latest variants of CFM-56.   Something along the line of Y2 is more than enough for China&#8217;s large  transport needs.  However, I find it curious that they think they can  develop a domestic engine option that can compete against next  generation Western options (like PW&#8217;s GTF series), when it would likely  be inferior to CFM-56-7 series.<\/p>\n<p>The order for 240 D-30KP2 made in  2005 is finally getting carried out this year.  These engines might all  be delivered by 2012.  I think China chose this ahead of KP3 and PS-90A  due to maturity of the engine, its lower cost and not wanting to  support two lines of high-bypass Russian turbofan engines.  By that  time, WS-18 should be more than ready to be equipped.  WS-10-118 (which  is the code name for the large bypass engine prototype based on WS-10A)  will probably be ready 3 or 4 years later for the domestic large  transport project.  WS-18 will still be produced at that point to  service the existing fleet using D-30KP2 engines.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>As you guys all know, the biggest problem that PLAAF have always had is the lack of high performing engine series. J-10 still relies on AL-31FN. We didn&#8217;t see any new J-10s for a while, because they used up all of the AL-31FNs. J-11B used WS-10A for a while, but had so much problems that [&hellip;]<\/p>\n","protected":false},"author":3,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":[],"categories":[1],"tags":[],"aioseo_notices":[],"_links":{"self":[{"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/posts\/110940"}],"collection":[{"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/users\/3"}],"replies":[{"embeddable":true,"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/comments?post=110940"}],"version-history":[{"count":0,"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/posts\/110940\/revisions"}],"wp:attachment":[{"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/media?parent=110940"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/categories?post=110940"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/cvnextjob.com\/index.php\/wp-json\/wp\/v2\/tags?post=110940"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}