达索幻影2000

25 One piece rudder (aluminium honeycomb filled, boron/epoxy/carbon) 26 Cantilevered multi-spar wing 27 Machined main spars and attachment fittings 28 Rear spar attachment lug 29 Front and mid spar attachment lugs 30 Machined ribs 31 'Sine wave' section ribs 32 Integrally machined stringers, one-piece skin panels (upper and lower, sealed for tankage) 33 Inspection panels 34 Brake chute housing (towers for deploy- ment, bydrauiicalty actuated) Air conditioning A1 Air duct bleed from engine HP system to air conditioning and pressurisation bay A2 Precooler and control valve A3 Overboard duct Underside view showing carriage of typical weapons Structure and general 1 Radome (Kevlar) is mounted on a porta- ble dolly and pulled forward for access 2 Forward electronics bay (temperature controlled) 3 Forward pressure bulkhead 4 Electrically actuated canopy (counterbal- anced) hot air demisted 5 Canopy emergency ground release 6 Anti-detonation chords (ADC) 7 Fully shrouded instrument panel 8 Rear pressure bulkhead 9 Martin-Baker Mk.FIOQA zero-zero ejec- tion seat 10 Rearward-opening panel over main avionic bay (carbon fibre aluminium hon- eycomb filled) 11 Semi monocoque fuselage structure 12 Fuselage intercostals and longerons (sealed for tankage) 13 Machined main fuselage/wing attach- ment frames (steel) 14 Area ruled and 'blended wing', all metal fuselage Instrument panel showing five CRT displays 15 Bifurcated engine air-intakes (slope for- ward) 16 Boundary air-layer ramps 17 Bi-contc air-intake cones, move parallel to fuselage via hydraulic screwjack (gen- erates four shock-waves at Mach 2) 18 Ventral suck-in doors (open at high an- gles of attack) 19 Fixed intake strake 20 Fin/fuselage attachment lugs 21 Rear fuselage, covered with extruded stringer stiffened skin panels 22 Two-spar cantilevered fin torsion box.covered with boron/epoxy/carbonfi- bre panels 23 Leading-edge (aluminium) 24 Detachable fin tip incorporating anti ero- sion strip A4 ECS bay A5 Primary and secondary heat exchangers (bootstrap system) A6 Ram air "in" from NACA intakes below aircraft via plenum chambers A7 Overboard air touvres A8 Mixing air units and water separators A9 Duct to cockpit via turbocompressors A10 Cockpit pressure relief valves (one each side) A11 Lox converter (5litres) behind sloping bulkhead Controls C1 Control column C2 Rudder pedals with toe-brakes C3 Cockpit side consoles C4 Control links to "Q" feel units (aircraft is totally FBW controlled) C5 Rudder hydraulic .servo actuator C6 Full-span, two-segment leading-edge variable-camber slat (CFRP) 17*30- inboard section, 30°outboard section C7 Slat actuator (hydraulic) C8 Segmented torque drive shaft • C9 Nut and screw drive actuators C10 Guide rails and rollers C11 Two section elevons (aluminium honey- comb core, CFRP skin) -16°+25c,can be deflected independently or differentially C12 Hydraulic servo actuator, (all actuators electrically signalled) C13 Push-pull rods and bellcranks C14 Machined hinges with glassfibre fairings C15 Upper and lower airbrake panels C16 Hydraulic actuator and cross-head Electr ics and e lec t ron ics E1 Thornson-CSE RDY look-down/shoot- down multimode radar E2 Head-up, eye-level and head-down dis- play E3 Pressure head (each side), electrically heated E4 Outside temperature probe E5 High alpha transmitter E l3 E6 Battery compartment, 28V 40Ahr ni-cad battery (both sides) E7 Avionic racks housing inertial navigation and flight control computers E8 Format ion-keeping lights E9 Refuelling floodlight E10 TACAN aerial E11 IFF aerial E12 Upper a nti -co I lis ion beacon E13 Electronic countermeasures (ECM) E14 Anti-radar jammers E15 VOR-glide aerials E16 VHF aerial E17 Position light E18 Chaff/flare dispenser E19 Navigation light E20 High-intensity landing lights E21 Total temperature probe (TTP) E22 UHF ariel Fuel system F1 Wing tanks F2 Feeder tanks F3- Mini feeder tanks F4 Forward tanks F5 External fillers (total four) F6 Pressure refuel/defuel coupling, {total in- ternal capacity 4,000litres (1.057US gals) F7 Interconnecting pipes F8 Fuel vent tine F9 Detachable inflight refuelling probe F10 Fuel tank capacitance probes IMUMXn? John Marsden AMRAeS Istres '91 Location of fuel tanks Powerplant P1 Engine power lever P2 SNECMA M53-P2 tu rbo fan eng ine, 95.1kN (21,3851b with afterburning), . FADEC controlled P3 Afterburner variable-ejector nozzle P4 Nozzle actuation hydraulic plumbing P5 Main thrust trunion mounting P6 Forward mounting ring and attachment s links P7 Rear mounting ring and attachment links P8 Upper torque links P9 Engine accessory gearbox P10 Angle driveshaft to/from auxiliary power unit (APU) P11 Airframe-mounted auxiliary engine gear- box (AMAD) both units mounted on the aircraft centre-line in a stainless-steel fireproof compartment P12 Auxiliary power unit P13 APU electric starter P14 APU exhaust ducts P15 Gearbox driving two 25kVA alternators and one generator Undercarr iage and hydraul ics U1 Hydraulic reservoir and accumulators (duel system mounted on both sides U2 Rearward-retracting nose undercarriage 360mm X 136-6 tyres, steering through 90°, incorporating a single disc brake (Messier-Hispano-Bugatti) U3 Pre-opening and closing undercarriage bay doors U4 Leg door (all doors CFRP) U5 Main undercarriage, incorporating single wheel with anti-skid polycrystalline graph- ite disc brakes and 750mm X 230-15 low profile tyres (Messier-Hispano-Bugatti} U6 Hydraulic retraction jack U7 Hydraulic contents guage Weapons and external s tores W1 DEFA 30mm cannon (both sides) W2 Muzzle blast trough W3 Ammunition magazine W4 Spent cartridge and link container W5 External wing pylons (total four) W6 Centre-line pylon W7 MICA missiles W8 MAGIC missiles W9 Super 530D ) R e e d Bus iness Pub l ish ing G r o u p