Page 424 - (DK) The Ultimate Visual Dictionary 2nd Ed.
P. 424

SEA AND AIR

       Helicopters



                                     HELICOPTERS USE ROTATING BLADES for lift, propulsion, and steering.
                                     The first machine to achieve sustained, controlled flight using rotating
                         blades was the autogiro built in the 1920s by the Spaniard Juan de la Cierva. His machine
                         had unpowered blades above the fuselage that relied on the flow of air to rotate them and
                         provide lift as the autogiro was driven forward by a conventional propeller. Then, in 1939,
                         the Russian-born American Igor Sikorsky produced his VS-300, the forerunner of modern
                         helicopters. Its engine-driven blades provided lift, propulsion, and steering. It could take
                         off vertically, hover, and fly in any direction, and had a tail rotor to prevent the helicopter
                         body from spinning. The introduction of gas turbine jet engines to helicopters in 1955
           BELL 47G-3B1
                        produced quieter, safer, and more powerful machines. Because of their versatility in flight,
       helicopters are today used for many purposes, including crop spraying, traffic surveillance, and transporting
       crews to deep-sea oil rigs, as well as acting as gunships, air ambulances, and air taxis.

                                                                       Droop stop
                                                                            Main rotor hub
                                               Blade counterweight
                                                                                   Blade-root attachment


            BELL 47G-3B1                           Main rotor mast         Stabilizer-bar weight
                               Direct-vision panel
                                                        Fuel vent pipe    Protective gaiter
                 Frameless                              Fuel tank        Fuel tank cradle        Tail-rotor
                 plastic canopy                                                                  drive shaft
                                                                                    Exhaust pipe
                   Radio
                                                                                      Air intake pipe
               Instrument
               panel                                                                     Electric fuel pump
            Cyclic-
            pitch lever
            Battery
            Battery
            overspill
             Electrical
             inverter
          Pitot head
                                                                                                  Breather
                                                                                                  pipe
           Anti-collision
           beacon                                                                             Oil tank
         Landing light                                                                   Carburetor hot-air
                                                                                         intake pipe
               Landing skid                                                            Air filter
                                               Navigation              Ground
            VHF omni-range antenna             light                   handling   Valve-rocker cover
                                                                       wheel
                            Ventilator             Electric power
                                                   socket        Lycoming six-cylinder engine
                              Collective-pitch
                              lever           Riveted light-alloy forward
                                              fuselage section

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