J-10 Fighter - máy bay Tàu

J-10 Fighter - máy bay Tàu

Từ trưóc tới nay, có ít thông tin về loại máy bay này của TQ. Tại triển lãm hàng không Chu Hải (TQ). Người ta đã rất ấn tượng với việc , TQ đã cho thấy sự tiến bộ rất nhanh của họ đối với nhựng công nghệ thuộc hàng top-tier của thế giới. Dưới đây là một trong những hình ảnh hiếm hoi về ****pit của loại multirole fighter bản địa này . Trông cũng khá ấn tượng đấy chứ các bạn nhỉ?

http://www2.ttvnol.com/uploaded2/bac_gia/20041207_6j10****pit.jpg


Được bac_gia sửa chữa / chuyển vào 16:13 ngày 19/05/2006

PLA khoe về con Lavi lai Mirage, lai..v.v...của nó như thế này, chả biết ra làm sao
J-10 MULTIROLE FIGHTER AIRCRAFT
The Jian-10 (J-10) is the multirole fighter aircraft developed for the People?Ts Liberation Army (PLA) as the four-generation indigenous fighter aircraft. The main contractors are Aircraft Design Institute and Chengdu Aircraft Industry Corporation (CAC) located in the suburb of Chengdu, Sihcuan Province. The aircraft competed its flight trails in 2002 and the delivery of 50 initial production variant J-10 fitted with a Russian-made AL-31F engine reportedly began in 2003. The two-seat fighter-trainer variant J-10B made first flight in December 2003.
PROGRAMME
The J-10 fighter programme began in the early 1980s to counter the Soviet four-generation fighters such as MiG-29 Fulcrum and Su-27 Flanker. The aircraft was originally designed as an air superiority fighter but changing requirements shifted development towards a multirole fighter with both air-to-air and ground/sea attack abilities. The J-10 development has benefited from both Israeli and Russian technologies. The aircraft?Ts aerodynamic layout is evidently based on the cancelled Israel Aircraft Industries (IAI) Lavi fighter design, and the Russian contribution includes the AL-31F turbofan engine. Ad***ionally, the aircraft?Ts avionics and weapon suites may also be based on either Israeli or Russian designs.
he J-10 programme officially began in 1986. Following a slow start, the project entered full-scale development when Chengdu took over the IAI Lavi fighter design, which was cancelled in 1987 under the US pressure, while IAI continued with the development of avionics for the fighter. Initially China wished to obtain high-performance turbofan engine technology from the West to power the J-10 fighter, but this soon became impossible as the US and other Western countries imposed an arms ban on China following the June 1989 incident. This almost traumatised the J-10 development, but China?Ts new ally Russia saved the programme by agreeing to offer its Lyulka-Saturn AL-31F turbofan engine as an alternative.
The J-10 went through some major redesign work because the oversized Russian AL-31 engine would not fit in the aircraft?Ts fuselage. This had caused some further delay in the programme. The first flight of the J-10 took place in late 1998. By late 1999 Chengdu had built six prototypes (1001~1006), two of which were used to static tests. The flight tests of the J-10 fighter was then transferred to Yanliang-based China Flight Test Establishment (CFTE) in Spring 2000. The aircraft received its design certificate in Spring 2004.
The initial batch production of 50 J-10 fighters began in mid-2002. It was widely reported that Lyulka-Saturn delivered 54 AL-31F turbofan engines to China between 2002 and 2004. PLAAF 44th Air Division based at Mengzi, Yunan Province became the first combat unit to have received the J-10 fighter. At the same time, Chengdu continued to develop a two-seat J-10B for advanced training and ground attack roles. It is believed that later variants of the J-10 will be powered by an indigenous WS-10A ''Taihang'' turbofan engine. Preliminary design a twin-engine version J-10 has also reportedly completed.
DEPLOYMENT
Unit
Base
Military region
PLAAF 44th Air Division Kunming, Yunnan Chengdu
DESIGN
The J-10 is single-engine fighter with a rectangle belly air intake, low-mounted delta wings, and front canard wings. The design is aerodynamically unstable, to provide a high level of agility, low drag and enhanced lift. The pilot controls the aircraft through a computerised digital fly-by-wire (FBW) system, which provides artificial stabilisation and gust elevation to give good control characteristics throughout the flight envelope. The J-10 is also the first Chinese-made fighter to be fitted with a large two-piece bubble canopy to give the pilot a better view in close air combat. If necessary, the aircraft could also be fitted with an in-flight refuelling probe.
****PIT
The J-10 is available as a single-seat or two-seat multirole fighter. It is the first Chinese indigenous combat aircraft to be fitted with a ?~glass ****pit?T, which features three flat-panel liquid crystal multifunction displays (MFD), including a colour one and two black-and-white ones. The ****pit is also equipped with a wide field-of-view head-up display (HUD).
It is very likely that the pilot is equipped with the helmet-mounted sight (HMS). It is not know whether the HMS is the basic Ukrainian Arsenel HMS copied by China''s Luoyang Avionics, or a new helmet display featured briefly at the 2000 Zhuhai Air Show.
The pilot manipulates the J-10 by the Iron Bird quadruplex (four channels) digital fly-by-wire (FBW) system. The pilot is also aided by advanced autopilot and air data computer.
RADAR
The J-10 is reported to be fitted with an indigenous KLJ-3 pulse-Doppler fire-control radar developed by Nanjing Research Institute of Electronic Technology (also known as 14th Institute). The KLJ-3 radar, which might be based on early variant AN/APG-66/68 technology, is said to have a maximum detecting range of 100~130km (attacking range 80~90km), and is capable of engaging two targets simultaneously. The radar system was tested on a Y-7 aerial radar testbed before being fitted on the J-10.
Russian company Phazotron is prompting its Zhuk-10PD, a version of the system in later Su-27s, with 160km search range and ability to track up to six targets. Israel has also offered its Elta EL/M-2035 radar for competition.
For low-level navigation and precision strike, a forward-looking infrared and laser designation pod is likely to be carried F-16-style on an inlet stores station. A Chinese designed pod similar to the Israeli Rafael Litening was revealed at the 1998 Zhuhai air show.
POWERPLANT
The initial low-rate production J-10s are powered by the Russian Lyulka-Saturn AL-31F turbofan rated at 17,857lb (79.43kN) dry and 27,557lb st (122.58kN) with afterburning. The same powerplant is also being used by Chinese air force''s Su-27s and Su-30s. Lyulka-Saturn reportedly delivered 54 AL-31F turbofan engines to China between 2002 and 2004. These are the AL-31FN model with special modifications to be fitted in the J-10.
Shenyang-based AVIC1 Aviation Engine Institute is also developing its own WS-10A (commercial name ''Taihang'') turbofan powerplant, and it could be fitted on the later versions of the J-10.
In 2005, China has reportedly ordered ad***ional 100 improved model AL-31F engines with increased thrust and possibly all-aspect thrust vector control (TVC), which will further enhance the aircraft''s manoeuvrability.
WEAPONS
The fixed weapon on the J-10 includes a single-barrel 23mm internal cannon. The aircraft also has 11 stores stations - six under the wing and five under the fuselage. The inner wing and centre fuselage stations are plumped to carry external fuel tanks.
The aircraft carries a range of air-to-air and air-to-ground weapons for different mission profiles. For interception and air-superority mission, the aircraft carries the indigenous PL-12 active radar-homing air-to-air missile and the PL-8 infrared-homing short-range air-to-air missile. The fire-control radar may also be configured to fire Russian-made AAMs such as R-73 (AA-11) and R-77 (AA-12).
For ground attack missions, the J-10 will carry laser-guided bombs, YJ-8K or YJ-82K anti-ship missile, as well as various unguided bombs and rockets. Some missiles currently under development such as the YJ-9 (Kh-31) ramjet-powered anti-radiation missile may also be carried by the J-10.
HISTORY
Oct 1986
J-10 project started
1998
Maiden flight successful
1999
Six prototypes produced
20 Dec 1999
Design completed. The six prototypes were transferred to Yanliang-based CFTE for flight test
2000 Q1
Intensive flight test began
2002 Q3
Flight test was relocated to a newly built airbase in the Gebi Desert
2003 Q1
Radar test conducted onboard a Y-8 radar testbed in Shandong Province
2003 Q3
First successful aerial refuelling simulation
2003 Q4
First successful PL-12 MRAAM test fire
2004 Q1
Development completed with the design certificated issued
SPECIFICATIONS
Crew: 1 (basic variant); 2 (fighter-trainer variant)
Dimensions: N/A
Weight: N/A
Max Speed: Mach 1.2 (sea-level) or Mach 2.0 (high altitude)
Range: Combat radius over 550km
Service Ceiling: N/A
Max Climb Rate: N/A
G Limit: N/A