Traditional Culture Encyclopedia - Photography and portraiture - Taiwan Province IDF fighter upgrade plan.
Taiwan Province IDF fighter upgrade plan.
In the technical development stage, it is estimated that two technical verification machines will be produced, and the factory numbers are single seat 10005 and double seat 10006 respectively. Among them, the airframe structure numbered 10005 is still in the old configuration, and only the avionics system is upgraded and verified; Airframe number 10006, delivered in 2007, with complete configuration, will include all airframe and avionics improvement projects. The aircraft 10006 was officially released on March 27th, 2007, and was named Goshawk by Chen Shui-bian. There are media reports that this is in line with "going to Chiang Kai-shek", and it is controversial to rename the "Guo Jing" fighter as "Eagle". In fact, "Eagle" can only be used to refer to the new fighter after the completion of the Xiangsheng project, and it is a new name for the new fighter. The original "Guo Jing" fighter is still a Guo Jing fighter, which is different from the "Eagle" fighter and has not been renamed.
● (IDF) F-CK- 1 A/B National Fighter.
● (IDF) F-CK- 1 C/D Eagle Fighter
Update the cockpit interface of elevator.
Install a new integrated color display system (ICDS). The main components include the following:
● Scanning/vector head-up display (raster /Storke HUD).
● Three large color liquid crystal multifunction displays (CMFD)
● Color cockpit photography system (CCTVS)
● New integrated head-up control/input panel (UFCP)
● The original six groups of engine monitoring instruments under the right panel are updated to electronic engine display system (EEDS).
● Standby electronic flight instrument (STBY EFIS Company)
Pointing helmet
Xiang sheng hang Dian
The avionics system of Xiangsheng Aircraft adopts 32-bit flight control computer of BAE Systems Company, which replaces the original standard flight control computer of 16-bit 1750 of Lear Astronics Company, and a brand-new FBW flight control mode (such as terrain tracking) is built into the computer to provide stronger processing capability. Albert Lin, project manager of BAE F-CK- 1C/D, said that this 32-bit computer based on PowerPC processor is the fourth generation flight control computer adopted by F-CK- 1C/D, replacing the 16-bit 1750 standard computer on A/B model. The A/B fly-by-wire control system is a three-redundancy digital plus three-redundancy analog backup system, while the C/D model does not need the original analog backup system. Lin said that the analog backup system provided good flight control quality for the F-CK- 1A/B aircraft: "Flight officials initially preferred analog systems to digital systems". Lin also said that the development of C/D flight control system and control law is the responsibility, and BAE Systems only provides computers-six flight control computers have been provided for two Xiangsheng prototypes.
Core avionics system update
● Introduce a set of color display processors.
● Expand the bus architecture to three sets of 1553B military standard interfaces (there is room for upgrading to four sets of 1553B military standard interfaces).
● Update flight procedures.
Communication/Navigation/Friend or Foe Identification System Update (CNI)
● Replace with a new inertial navigation system (GPS/INS).
● Replace two sets of new UHF/VHF radios (ARC-2 10).
●APX- 1 13(V)AIFF advanced friend or foe identification system.
Update of GD-53 launch control radar
GD-53' s 5-piece LRU was changed into 3-piece LRU architecture, and all the old 3-piece LRU such as radar target processor, radar data computer and control/power supply were replaced with 1 new radar data processor (RDPs).
New working mode of GD-53 elevator launch control radar;
● Combined radar mode (CRM)
● Groove area indicator for tracking target.
● Automatic scanning adjustment (TWS) in scanning synchronous tracking mode.
● Search target, absolute altitude and speed vector display.
● Add flight path recorder and fault diagnosis system.
Enhancement of electronic countermeasures for GD-53 launch control radar;
● Interference source detection (DOJ)
● Interference source tracking (TOJ)
● Passive ranging.
Typical passive ranging has the following four types:
● Angular velocity ranging
● Triangulation distance measurement
● Signal strength ranging
● Third-party information
● Silent mode (sniffing)
● Other ECCM functions:
● Quickly re-lock.
● Single receiving beam (primary)
Low pulse edge distance (LET)
● Single receiving cone scanning (COSRO)
Flight control performance and range improvement
Flight control software
In terms of software, AIDC rewrote the flight control software in C language to improve the low-altitude autopilot capability of fighters.
Improvement of take-off and landing performance
● Accurate lifting speed of fighter front wheel.
● Improve the crosswind capability of fighters to 56 km/h..
Increase the approach angle of attack and shorten the runway distance
● The fighter's approach speed decreases18.5km/h..
● Reduced landing distance 10%
● Replace the digital braking system.
Conformal fuel tank CFT
The two CFTs installed on the Eagle aircraft are located at the rear, covering almost the entire rear of the aircraft. The total oil load of these two CFTs is 65,438+200 lb (545 kg, only 40% of the F-65,438+06 Block 50/52 CFT), which makes the range of elevators increase by 20% on average. In the future, it will be decided whether to increase the fuel load of two CFTs according to the engine thrust and customer demand. The weapon system strengthening plan of F-CK- 1 fighter includes a variety of weapons under development, such as Qingyun oil-gas bomb and Wan Jian bomb, in order to increase the ground strike capability of F-CK- 1 except air superiority tasks.
Qingyun oil and gas bomb
A kind of oil-gas bomb developed by Chinese Academy of Sciences can kill a large area of personnel and equipment, and give a devastating blow to large troops or material assembly areas.
Wan Jian bomb
JSOW-like out-of-sight attack weapons can carry multiple submunitions.
It is reported that the test was successful in early 2006. In August 2008, the photos of the F-CK- 1 of the Qingquangang Combat Team with Wan Jian bombs were circulated on the Internet, presumably distributed to the combat teams in small batches for evaluation.
● Warhead: There are about 100 submunitions in it.
● Power: Kunpeng turbine engine.
Tian Jian 2A anti-radiation missile
● Projectile length: 3.593m.
● Bullet diameter: 19 cm
● Bomb weight: 184kg
● Warhead: 22k g 1 member (A and C single landline); Two captains (type B and type D)14.48m wingspan 8.53m overall height 4.7m wing area 24.26m2 empty weight 6492kg combat weight 9072kg maximum takeoff weight 12, 530kg power FE- 1042-70 (US military code: Honeywell F/.
2 kN) Maximum speed 1.8
Mach oil single-seat type 2111kg; Two-seat 1884 kg, and the two CFTs planned in Xiang Sheng can increase the oil quantity 1200lb (about 545kg). Emergency interception:130km; Power cruise: 1 100km (with 1040L auxiliary fuel tank× 3) service ceiling 16760m sea level climb rate 14326m/min, with 1 040L auxiliary.
Low altitude air-to-air missile;
● Tian Jian-1 missile
● Tian Jian II missile ●AIM-9 Sidewinder infrared guided short-range missile.
● Air-to-surface missiles:
●AGM-65 Mavericks Missile
● Rocket:
●LAU-60 rocket pod /2.75 inch ground-to-ground rocket
* LAU-69 rocket pod/19 68mm ground-to-ground rocket
● Bomb:
MK20 cluster bomb
●MK-82SE Snake-Eye Delay Fuze Bomb
●2000-pound bomb, 750-pound M 1 17 bomb.
●GBU- 10. 12.24 paving type II laser-guided bomb (without guidance device, do you need wingman guidance or external guidance? Cabin)
● It can only be used after upgrading through Xiangzhan Project:
* Air-launched Xiongfeng II anti-ship missile
● Tian Jian II A anti-radiation missile
● Qingyun oil and gas bomb
● Ten thousand arrows missile
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