Nothing wrong in talking to yourself. Its only when you answer
Take a closer look. The nozzles were clearly moving.
So? Who said that was a Chinese engine? Unless they specifically said "this is the ws10 engine" then its probably not Chinese.
"WS-10A is reported to have 13,200 kilograms (29,000 lb) of thrust and a 7.5:1 thrust-to-weight ratio, making it comparable to the AL-31F turbofan. The WS-10A was first displayed in public at the 2008 Zhuhai Air Show.[6] The WS-10A design consists of a 7-stage high pressure compressor, short annular combustor with air blast atomizer and air film cooling blade. It is the first production turbofan from China to feature single crystal nickel-based turbine blades, which allow higher intake temperatures and greater engine thrust. WS-10A has also been equipped with a FADEC (full authority digital engine control) system. An asymmetric thrust vector control (TVC) nozzle, similar to the TVC nozzle of the Russian AL-31F-TVN engine, has also been reported undergoing testing.
On 2 April 2009, the director of AVIC (Aviation Industry Corporation of China) Lin Zuoming (林左鸣), stated that there were problems with the quality control procedures on the WS-10A production line, meaning the Taihang turbofan was still of unsatisfactory quality. He said that solving these problems would be a key step.[7] The Chinese engines have been lasting 30 hours at a time vs 400 for the Russian originals.[8]
Derivatives of the WS-10 are under development, such as a high-bypass turbofan variant for propelling large transport aircraft and marine gas turbine variant for propelling ships.
A thrust-vectoring variant with higher thrust (132 kilonewtons (30,000 lbf)), called the WS-10B, is also in testing and is ready for combat aircraft installation.
An even further upgrade with higher thrust (155 kilonewtons (35,000 lbf)), designated the WS-10G, is also under testing.
Variants
* WS-10 - original design producing a thrust of 126 kilonewtons (28,000 lbf)
* WS-10A - upgraded variant producing a thrust of 132 kilonewtons (30,000 lbf)
* WS-10B - upgraded thrust-vectored variant producing a thrust of 135 kilonewtons (30,000 lbf)
* WS-10G - upgraded variant producing a thrust of 155 kilonewtons (35,000 lbf) with Thrust Vectoring and stealthy nozzles that have jagged edges and tiles"
Then Gates was obviously talking himself and he answered it as well.![]()
By Henry Ivanov JDW Correspondent
Moscow 09 January 2006
China is developing an advanced version of the Chengdu Aircraft Industrial Corporation (CAC) J-10 multirole fighter aircraft, referred to as the Super-10, with a more powerful engine, thrust-vector control, stronger airframe and passive phased-array radar, according to Russian sources.
Russian Aircraft Corporation MiG (RSK-MiG) specialists, contracted to provide technical assistance to Chinese design houses, said the enhancement to the J-10 airframe is a logical step, since the fighter was initially intended to have the compact Pratt&Whitney PW1120 engine that powered the Israeli Lavi aircraft, which served as a basis for the J-10.
However, the imposition of US export restrictions forced the decision to install the 20 per cent heavier Russian AL-31FN engine, which requires a larger intake as it needs 40 per cent more air flow.
In late 2005 China placed a USD300 million order for a second batch of AL-31FN engines; these are a derivative of the Su-27's AL-31F for single-engine aircraft, with a lower positioning of the gearbox. At first, it was believed the contract was for the same engines as in the first batch of 54 units supplied in 2001-02 and installed into development prototypes and initial production J-10s. However, AL-31FN-maker Moscow Machine Production Plant (MMPP) Salyut in December 2005 revealed the order to be for the AL-31FN M1, which is claimed to be a new AL-31FN production standard.
The company's general manager, Yuri Eliseyev, said the new engine was purposely developed for what he referred to as the "Chinese Super-10 fighter". Four such engines have been seen assembled at MMPP Salyut's Moscow production site. One of these has been demonstrated undergoing fire testing, during which its swivel nozzle was deflected up/down and sideways at full power and reheated thrust.
Chinese television has shown images of President Jiang Zemin inspecting this project. The concepts indicate that the thrust-vectoring nozzle can be deflected by up to ±15º in any direction.