And something about the Al-31FP itself :
The Su-30MKI is powered by the Al-31FP (P for povorotnoye meaning “movable”), which is a development of the Al-37FU (seen in the Su-37 Terminator).
AL-31FP which is designed by the Lyulka Engine Design Bureau (NPO Saturn) is also different from Al-31F (by the same company). The Al-31F is the ‘baseline’ powerplant found in most Su-27 and its variants, and perhaps in the China’s J-10 in the future and lacks TVC. The AL-31FP was only 110Kg heavier and 0.4 m longer than the AL-31F, while the thrust remains the same. Planes equipped with AL-31F can be upgraded to AL-31FP later on without any changes in the airframe. It is being produced now at the Saturn manufacturing facility at Ufa, Russia.
The Al-37FU (FU stands for forsazh-upravlaemoye-sopo or “afterburning-articulating/steerable-nozzle”) basically added 2D Thrust Vectoring Control (TVC) Nozzles to the Al-31F. 2D TVC means that the Nozzles can be directed/pointed in 2 axis or directions – up or down. TVC obviuosly makes an aircraft much more maneuverable. Al-31FP builds on the Al-37FU with the capability to vector in 2 planes i.e. thrust can be directed side-ways also. The nozzles of the MKI are capable of deflecting 32 degrees in the horizontal plane and 15 degrees in the vertical plane. This is done by angling them inwards by 15 degrees inwards, which produces a cork-screw effect and thus enhancing the turning capability of the aircraft.
The TVC nozzles will be made of titanium to reduce the nozzle’s weight and can deflect together or differentially to achieve the desired thrust vector for a particular maneuver. The engine designers are also working to reduce the infrared signature for thrust settings below afterburner.
Also, the 2-nozzles can be vectored un-symmetrically, i.e. each nozzle can point at different directions independent from the other nozzle and thus multiplying the effect.The aircraft is capable of near-zero speed airspeed at high angles of attack and super dynamic aerobatics in negative speeds up to 200 km/h.
TVC allows the MKI for example, to rapidly loose speed and turn in any direction and fire its weapons. The complete range of maneuveres possible in the MKI are impossible on any other combat fighter in production. “We even made a corkscrew spin a controllable manoeuvre – the pilot can leave it at any moment by a single motion of the stick that engages thrust-vectoring and aerodynamic surfaces,” says Sukhoi’s earlier general designer Mikhail Simonov.
Two AL-31FP by-pass thrust-vectoring turbojet reheated engines (25000 kgf full afterburning thrust) ensure a 2M horizontal flight speed (a 1350 km/h ground-level speed) and a rate of climb of 230 m/s. The Mean Time Between Overhaul (MTBO) for the AL-31FP is given at 1,000 hours with a full-life span of 3,000 hours. The titanium nozzle has a MTBO of 500 Hrs.
The Al-31FP improves upon the Al-37FU in two ways:
Firstly, the Al-37FU cannot vector thrust in 2 planes unlike the Al-31FP.
Secondly, the nozzle drive connection is effected now from the aircraft fuel system and not from the aircraft’s hydraulic system. The change-over to the fuel system, to control swiveling nozzles, enhances the dependability of the aircraft and its survivability in air combat.
Infact i would like to know what the actual deal on the Al-31FP is and what tech is actually transferred .
All i found about the deal was this :
India’s Defence Minister George Fernandes laid the foundation stone of a new HAL factory at Sunabeda (20 kms from Koraput, Orissa) on Dec 15, 2002. This brand new facility is licenced to produce 1200 AL-31FPs. It is said that the manufacture of the AL-31FP engine “involved 31 new technologies required to be adopted and mastered”
link
heck 1200 Thrust vectoring Al-31FP’s are a lot of engines; its tech & core must be reverse engineered.
India is licence producing sooooo many the Al-31FP’s ..now what do you suppose is going on ??
We are assembling all the parts that come from Russia…right ?
I mean with a little effort we can make the same copies of the Russian parts and put it apart like its done for the other engines, right ?
BF…..India appear to have “missed the bus” in this copying game π by trying to be the “good boy” because of our patethic honour abiding congress govt. leaders π‘
For how much do you suppose Russia will sell someone (say India) the top-to-bottom of the Al-31 tech ??? …do you think they will give us the core of their new engine (al-41xx ?) if we finance a part of the PAK-FA engine ???
That’s why they sent it to Russia to reverse engineered, but western engine is too complex, the russian engineers couldn’t crack it, the engine then blew up in the test in Moscow..Now, GTRE is begging SNECMA for help.
Stop being riddiculous…..The engine test facilities in Russia are cheap…thats the only reason the engine was sent to Russia. And the engine sent to Russia was the Kaveri not the GE 404.
and what are you thinking next…France will try their hand at reverse engineering ????? 

BTW : I must appreciate you imaginative thinking…maybe you must write a science fiction conspiracy theory book or something………good luck π
largely the US desighn they aquired in th 80s.
i want to know more about this. Could you(or anyone) give me a list of major tecnologies/designs that china obtained/stole from the West in the 80’s ?
It is also very likely that in recent years AL31 tech has been introduced to the WS10A.
I second you on that.
Also remember that when J10 development began china and the soviet union were not exactly good friends, thus the chances of china recieving thier latest engine technology during that era are slim to say the least.
China got the Al-31FN’s from Russia in the early/mid 1990’s when Russia were desperate for money due to the USSR collapse.
and will anyone care to answer my query on the WS-13(?) and RD-93. :confused:
and every now and then i hear about some thrust vectoring for the WS-10 …how true is this ??
crob, i dont intend to offend you chinese guys around, but you’ve missed these from the article :
Western vendors have provided Chinese aircraft with the MIL-STD 1553B data bus, which now has been installed on new 052 DDGs. China has used a Type-W datalink provided by France
As on the U.S. Aegis ships, such systems can retain many of the original hardware cabinets, but the unique display console might be replaced with a standard shared console including open architecture LAN access. Chinaβs choice of a LAN could be a Russian GOST standard or a Digibus LAN used on French TAVITAC CDS aboard recent PLAN ships.
and do you also debunk these claims from sinodefence ??
The propulsion system might be in the form of CODOG consisting of two Ukraine-made DA80/DN80 gas turbines rated at 72,600hp (55 MW) and two indigenous diesels (Chinese copy of the MTU 20V956TB92) rated at 8,840 hp (6.5 MW).
It is common knodwledge that HQ-9 SAM is made out of the S-300 and the Patriot from Israel.
The antisubmarine warfare suite would be Italian triple antisubmarine warfare torpedo tubes and 12-barrel Type-75 mortars.
and the Type-95 is a chinese copy of the Russian RBU-1200
Everyone keeps saying that China will reverse engineer the RD-93 and make their own WS-13 (?) to supply to pakistan.
how hard is this ?? and how much time would such a thing take if its done ??
Incorrect. The Kvant radar is a pure search radar only and lacks fire control Clueless people citing clueless sources do not make things right.
Yeah clueless…check out this link >> http://www.afcea.org/signal/articles/anmviewer.asp?a=992&z=38 … blows the top on the 052c’s non-indegenous hi-tech components.
and sinodefence (although you discredit it) says : Reports indicate this radar system may be a co-development program with the Kvant-Radiolokatsiya company of the Ukraine. The band and performance of this radar have not yet been publicly reported. The radar may be a developed version of that first seen on the 970 weapons test ship, and could either be S-Band or Russian-style X-Band.
http://www.sinodefence.com/navy/surface/052c.asp
and both the links also say that most of the propulsion, anti-sub warfare system, gun, etc.. is all plagerised.
and i found a chinese fellow say this on another forum :
The PAR’s origin is yet unknown, some say its from Ukraine with the help of Chinese scientists, somesay its from a institute within China, some say China stole it during the Clinton years alongside the nuke blueprints
and what about these nuke blueprints :confused:
chinese homegrown missiles – all plagerised ??
and about all the chinese missiles :
The famed PL-12 or SD-10
The PL-12 was said to be derived from the Italian Aspide technology and integrated with active radar-homing seeker technology obtained from Russia.
The missile was developed indigenously, but also with helps from foreign manufacturers. Several Russian missile and subsystem developers are reportedly supporting the program, with much of the missile utilizing components from the R-77 (AA-12 Adder).
In 1996 China revealed an active radar-homing seeker AMR-1, which is possibly based on Russian technology. Claimed to be developed for the new generation active radar-homing MRAAM, the AMR-1 seeker or its developed variant could be used to guide the SD-10.
http://www.sinodefence.com/missile/airlaunched/sd10.asp
PL-11
Chinese copy of Italian Alenia’s Aspide missile (which inturn was derived from the U.S. AIM-7E Sparrow) that it got in the late 1980s
http://www.sinodefence.com/missile/airlaunched/pl11.asp
PL-9
Apart from its control surfaces the PL-9 is almost identical to the Israeli Python-3, which was developed from the AIM-9L. The one major difference, according to information in Jane’s All the World’s Aircraft, is that the PL-9 has only about one-third the range of the Python 3.
China has improved upon the PL-9 by marrying it to an apparent copy of the Arsenel helmet sight from the R-73.
http://www.sinodefence.com/missile/airlaunched/pl9.asp
PL-8
The PL-8 infrared homing short-range air-to-air missile is a Chinese copy of the Israeli Python-3.
http://www.sinodefence.com/missile/airlaunched/pl8.asp
The PL-4
The PL-4 is a Chinese copy of the U.S. AIM-7B Sparrow. (from Pak ?)
http://www.sinodefence.com/missile/airlaunched/pl4.asp
Its other missiles : R-73, R-77, R-27 – These are Russian missiles.
oh i see that stuff has moved here from the other 2 threads. thanks
oh and about the FC-1’s radar :
The Italian Grifo S-7 fire-control radar was chosen by the PAF to equip its JF-17 Thunder >> http://www.sinodefence.com/airforce/fighter/fc1.asp
and this : Pakistan Air Force officials expressed dissatisfaction with the quality of Chinese avionics and radar systems, preferring European-made systems.
http://www.atimes.com/atimes/South_Asia/GC29Df03.html
care to explain this carbato ??
WS-10 thread
The WS-10A is the Chinese engine intended to replace the Russian ones in the J-10 and the Chinese Su-27 (J-11).
I have a feeling it is a reverse engineered chinese copy of the Al-31FN.
China’s previous history in reverse engineering and making illegal copies of proven designs further strengthen’s this feeling.
Look at these :
Russian arms industry sources have disclosed that China is close to mastering the complex skills required to build(reverse engineer ?) the Al-31 engine
page 7 of http://www.sipri.org/contents/armstrad/ch10.MASTER.050513.pdf
Russia reportedly had denied China the license to produce the engine locally. As the result, an indigenous engine WS-10A (came up)
http://mil.jschina.com.cn/huitong/J-10_J-11_FC-1.htm
The CAC is also trying to replace the Russian AL-31F with the indigenously developed WS-10A, which is said to be a Chinese copy of the AL-31FN.
http://www.sinodefence.com/airforce/fighter/j10.asp
what are your views ?? for China have never failed to copy any proven design that they get their hands on…and the examples for this are innumerable.
So SNECMA, Klimov or General Electric are going to make the Kaveris for the MCA?
At least one of us can’t read.
Pardon me sir, but let me clarify this >>
The State owned Gas Turbine Research Establishment [GTRE] was to indigenously develop the Kaveri engine to power the LCA and MCA. But there have been major slippages in all the milestones. GE, SNECMA, and Klimov had all offered to provide the engines for this aircraft.
But now the GTRE is asking these companies for help in designing the MCA Kaveri instead of asking them to provide the whole engine themselves (if you read the article on the previous page)
and the MCA kaveri details is there at >> http://www.geocities.com/spacetransport/aircraft-mca.html#engine
There are different Kaveri’s for the LCA and the MCA.
check out the MCA’s Kaveri’s details at http://www.geocities.com/spacetransport/aircraft-mca.html#engine
and this link >> http://www.bharat-rakshak.com/IAF/Info/Aircraft/MCA.html
says : (pay attention to the bold part)
The Medium Combat Aircraft [MCA] is projected as the replacement for the Jaguar and Mirage 2000 fleets in the IAF. It is under design at the Aeronautical Development Agency (ADA) in Bangalore. The MCA will cost $2 billion to develop and will be a tailless delta design with two engines, combined with a thrust vectoring control capability. It is hoped that the engines on the aircraft will develop a thrust-to-weight ratio of 7.8:1. Although it is unclear which company will be selected to supply the engines; SNECMA, Klimov and General Electric have been identified as potential suppliers.
The Donier looks dumb :
