闪电LIGHTNING

46 FLIGHT, 13 July 1961 LIGHTNING 10 I I 12 13 14 15 16 17 18 19 20 21 22 23 24 25 24 27 28 29 30 31 32 33 34 35 36 37 38 General Fuselage 1 Kelvin Hughes 91 in pi cot boom 2 Intake bullet housing Airpass radar Top bullet spigot access Nosewheel bay in lower bullet-strut Engine air duct Bullet alignment adjustment Supplementary intakes (those in bullet stalk locked shut in produtcion aircraft) Duct flattens below cockpit Air to lower (No I) engine Air to upper (No 2) engine Top gun longeron Lower longeron Gun shroud structure Two gaseous-oxygen bottles Oxygen charging connection Nose jacking point Attachments for cockpit ladder Magnesium-forged canopy top frame Shoot-bolts Canopy latches Inflatable canopy seal Front pressure bulkhead Rear pressure bulkhead Side pressure walls Access to ammunition tanks, autopilot computers, fuel- contents amplifiers, Tacan T/R. master reference gyro, emergency battery Armament bay between frames 13 and 22 Multi-bolt joint between front and rear fuselage at frame 25 Wing/fuselage front main attachment Wing/fuselage rear main attachment Multi-bolt attachment plate Stress-bearing hatch under No 1 engine Oil filler access Engine drains Hatch attachment bolts Stress-bearing hatch over No 2 engine Hatch-lifting lug Fin spars bolted to frames Jetpipe trunnion access panels 39 Light-alloy honeycomb sand- wich structure 40 Dielectrically isolated fin tip 41 Braking-parachute compart- ment 42 Parachute streaming anchor and jettison unit 43 Streamer cable spring-clipped around rear lip 44 Main pack 45 Vane-type auxiliary para- chute 46 Cables actuating internally retracting doors 47 Tail bumper 48 Tie-bars across four rear frames 49 Reheat-jetpipe mounting rails Wing Front and rear spars of hockey-stick form Wing halves bolted through forged centre rib Main wing-box skin machined from 0.2in light-alloy plate T-section intermediate-spar booms pre-attached to skins Rib/spar structure inside box bolted in Warren-girder lattice Detachable leading-edge sec- tions Compass unit in starboard leading edge Aerodynamic sawcut slots Navigation lights Corrugated - sandwich skin in wheel bays 50 51 52 53 54 55 56 57 58 59 A At A2 A3 A4 AS A6 Cl C2 C3 C4 C5 C6 C7 C8 C9 CIO CM CI2 CI3 CI4 CI5 CI6 CI7 Air conditioning Ram intake to cabin-air heat exchanger at duct bifurcation Cold-air unit and water boiler on starboard flank Water header tank Water extractor Conditioned air duct to cock- pit Cockpit pressure test con- nection Flying controls and cockpit Aileron p.f.c.u. (powered flying-control unit) Rudder p.f.c.u. Tailplane p.f.c.u. Ultra amplifiers (tailplane and autostabilizer system) Tailplane spigot Tailplane - drive triangular frame Aileron mass-balance Aileron control push/pull tubes Triple-roller guides Aileron autostabilizer actua- tor Rudder feel unit Rudder autostabilizer actua- tor Rudder trim actuator Control column Rudder pedals Engine power control panel Canopy external locking controls CI8 E2B standby magnetic com- pass CI9 "Canopy unlocked" warning lights C20 High-intensity cockpit light- ing C2I Starboard airbrake shown open C22 Plain flaps D De-Icing Dl Hot-air anti-icing around intake lip D2 Rain dispersal duct D3 Side-panel demisting ducts D4 Canopy top-panel demisting ducts D5 Demisting-air flexible bel- lows O6 Canopy-air desiccant packs D7 Embedded electro-thermal windscreen elements El E2 E3 E4 E5 E6 E7 E8 E9 EIO El l EI2 EIJ Ma-,, t ion Peisi ne>:t< venti Face- Alter Parat Survi Ham ride Emer take Ernei hand Cane striki Firev Hon aniur Grav botti FLIGHT, 13 July 1961 47 ejec- con- air- 1 -legs >ver- i in- tison and (tit- ssion F Fl F2 F3 F4 F5 F6 F7 F8 F» FIO Fl l F I 2 F I3 F I 4 FI5 FI6 Fuel system Integral fuel cells in wing Collector tank with booster pumps Fuel recuperator Recuperator control valve Fuel transfer valves Air line to recuperator Defuelling valves behind rear spar Pressure-fuelling adaptor in fuselage "Tanks ful l" green lights panel Low-pressure fuel pipe Ventral tank (jettisonable in emergency) Multi-bolt inspection panel Tank aerodynamic fin Flap fuel Detachable Flight Refuelling probe Tank pressurizing intake/ vent in sawcutslot Power systems H H I H 2 H 3 H 4 H5 H6 H 7 H 8 H 9 H I O H I I H I 2 HI3 H I 4 HI5 Electrical Varley 28V battery behind canopy Battery test socket Neoprene drain tubes No 2 battery in spine amid- ships External a.c./d.c. receptacles in wheel well Main accessory-drive unit, driven by b!eed-air turbine Gearbox and oil filler Rotax 28V d.c. generator English Electric20kVA alternator Cooling-air intake to acces- sory-drive unit Turbine exhaust from (H6) Teddington magnetic ampli- fier on door External cable duct past No 1 engine Artificial horizon power sup- ply control/inverter Electrical duct Continued overleaf This drawing by our artist Arthur bowbeer depicts the essential fea- tures of a Lightning F.I A all- weather fighter. Arrayed along the bottom of these pages are details of the Airpass radar and weapon loads 1961%20-%200946.pdf 1961%20-%200947.pdf