 Wysłany: Sob 19:31, 18 Wrz 2010 Temat postu: Gaul Eagle French Rafale fighter |
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| Reprinted from the heart ^ _ ^ Angel's blog
\1983, the company announced the development of advanced experimental fighter (ACX), called \ experimental \the company's push Dongkemadi research than 10 of the M88 turbofan engine. \February 1990 \\A total of 5 prototype was manufactured for trial, including two Air Force \body aircraft delivery in Toulouse, October 1991 to do fatigue testing center. First a \\ Rafale A prototype Dassault original estimates, \planes, the French Navy needs 78. The Air Force's 234 in 139 is a two-seat fighter. Navy will begin delivery in 1996. \Estimated unit price more than 60 million U.S. dollars. naval version of the Rafale M Although the Government to formulate a multi-year procurement plan has been delayed again and again, but the aircraft development work has not stopped. Now the French government finally issued the first batch of procurement plans, the first batch of production is also carried out using the test, users will be delivered soon. \fighter development. The new factory of the \Particularly impressive, the French Ministry of Defense has started on the \ seater Rafale B \lion and called the European \Although they did not use F-22 Raptor as fourth-generation fighter technology, such as the shape design of stealth technology, thrust vectoring technology, supersonic cruise technology, compared with the current third-generation fighter in service with a lot of modern technology, Thus, the comprehensive combat capability has been greatly improved, and there is considerable potential for further development. \intake efficiency, the inlet is located under the fuselage; extensive use of carbon fiber and Kevlar fiber composite materials, aluminum-lithium alloy; diffusion bonding of titanium components / processing of superplastic forming, etc.; use of a threshold, automatic overload protection, Under fault conditions the system function and anti-recombinant bumpy features fly-by-system; by side stick, fiber, voice, wide-angle holographic head-up display, side alignment sight and the two multi-function color displays and other advanced equipment. single-seat Rafale C \wing with carbon fiber composite material. Components to install aluminum lithium alloy joints. Movements may be in the same direction and the differential aileron deflection. Two-stage titanium full span leading edge slats, flaps down automatically and the linkage, can change the wing bend, increasing lift. Wing root fairing for the poly-aramid fiber composites. All control surfaces are fly-by hydraulic steering gear control system. conventional semi-monocoque body structure, 50% of carbon fiber composites. The former is mainly conventional aluminum fuselage, aft fuselage for the carbon fiber composite. Al-Li alloy machine body side skin. Fairing nose fairing and the nozzle for the poly-aramid fiber composites. Landing gear and engine hatch for the carbon fiber composite material. Front of the fuselage in the tail on both sides of a door-type brake. front wing is swept on all fixed wing, power transmission hydraulic control system of control. Mainly titanium superplastic forming diffusion bonding. Landing gear down, the front wing can be automatically lifted 20 °, to provide additional lift. Carbon fiber composite cantilever vertical stabilizer and rudder with honeycomb core structure embedded. Tail tip for the poly-aramid fiber composites. Rudder control system of hydraulic power transmission control. No auxiliary control surfaces. Mercier Spanish company as a \Front-wheel hydraulic control can be turned, before the main round are forward put away. Design landing sink speed of 4 m / sec, without leveling the aircraft before landing. Lin main round of the Michelin radial tire size company 810 × 275-15, tire pressure 16 × 105 Pa (16.3 kg / cm 2). The main, front carbon brakes are used. Power transmission control system control. Emergency on the rudder with the drag parachute cylindrical root compartment. Snecma's M88-2 engines its installed 2 sets of Snecma M88-2 engine, single- Taiwan, 48.7 kN of static thrust, afterburning thrust of 72.9 kN, optional M88-3 afterburning engine of up to 87 kN thrust. Two independent semi-circular inlet is located in the ventral side, no air conditioning into the cone, there are manifold, can work to ensure no interference of two engines. Body aircraft capable of carrying 5,700 liters of fuel tank, the fuselage center line within the wing pylons and two wing pylons and two in 1250 liters of fuel tank can be linked to the maximum external fuel capacity up to 9500 liters, the total fuel capacity up to 15,200 liters. Aerial refueling probe tube is located right in front of the cockpit windshield, B / C type is fixed, M-type to be telescopic. Using pressure-type fuel injection, 4 minutes in the tank will be filled within 7 minutes, all the fuel tanks filled. \Single block windshield, hatch opens to the right. Hatch painted gold coating to reduce radar reflection area of the cockpit. Throttle lever with a small stroke. In the right side of the stick with the console. Abbe heat - Sai Muka's cabin air conditioning system. Two hydraulic systems, stress 280'105 Patrick, the use of two mercier - Bigatti the company's hydraulic pumps. Frequency communication system, there are two 30/40 KVA Auxilec alternator. A set of three redundant digital flight control system and a telex dual redundant flight control system, analog fax, integrated engine control system with arms linked. Eros's oxygen system. machine using the Thomson-CSF company with the next video / radio capability RBE2 under the radar, can track eight targets simultaneously and can automatically Threat assessment goals, prioritize. EAS's UHF / VHF radio and UHF radio TRT's, SB 25A and Information transceiver device, sextant's voice radio control system and voice warning system. SOCRAT's TLS-2020 integration of ILS / MLS, and VOR / DME systems, mechanical electrical company RL90 RLG inertial navigation systems, Thomson-CSF's NC 12E AHV 17 TACAN and radio altimeter, SFIM / Dassault Electronics Technology flight recorder and the sextant's GPS system. Sextant company's side of the color LCD touch screen set Duo Gongneng can be integrated Xianshi fuel, engines, hydraulic, electrical, oxygen and other systems of digital information, CTH3022 type wide-angle holographic HUD integrates Thomson's OTA 1320 CCD 照相机and recorders. Level tactical navigation / sensor information display. Sextant's Topsight Helmet. Thomson-CSF company's electro-optical sensors, MIDS data link and a variety of reconnaissance, electronic countermeasures, forward-looking infrared and laser targeting pod and so on. In addition to the high radar warning receivers and electronic countermeasures equipment, the machine is also equipped with a laser warning system. Airborne electronic equipment and rack up to 780 kg total weight. At present, \ as flight control systems and structural materials technology advances, \small size and weight of the aircraft. The current thinking from the traditional aerial battle to from close-range fighting far, medium-range missile engagement and the direction of transfer of the coexistence of short-range combat, so these three generations of semi-fighters have been focusing on enhancing operational effectiveness missiles, airborne radar and weapon systems require can be found as far away from goal, also requested to launch pre-emptive weapon to shoot down the other side. In this attack, in addition to track and destroy the missile's own ability, but also depends on the machine tool's own kinetic energy, greater energy, firing missiles can fly farther, and more efficient operations. At the same time the pilot must look for a \Asked the mother function as the highest possible speed in launching missiles, so like the \In addition, because the missile's maximum firing distance is determined not only by the energy of machine tools, but also depends on the enemy close to the rate between the two units. To attack a fleeing enemy missile is the largest attack range is always smaller than the head of a flying enemy is range, so pilots must also take into account the missiles can as quickly as possible, with the smallest possible energy loss of enemy fled, to avoid being counter-attack enemy missile launch. This requires \ gust Navy F/A-18 and U.S. imperialism dog fight the HUD screenshots, this aircraft Hornets doomed the read to keep abreast of the ... copy the successful, press CTRL + V to send to a friend, forum or blog. 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