Page 132 - The Jet Engine
P. 132

Starting and ignition





        METHODS OF STARTING                               engine provides sufficient power for the engine
                                                          turbine to take over.
        3. The starting procedure for all jet engines is
        basically the same, but can be achieved by various  Electric
        methods. The type and power source for the starter  5. The electric starter is usually a direct current
        varies in accordance with engine and aircraft require-  (D.C.) electric motor coupled to the engine through a
        ments. Some use electrical power, others use gas,  reduction gear and ratchet mechanism, or clutch,
        air or hydraulic pressure, and each has its own   which automatically disengages after the engine has
        merits. For example, a military aircraft requires the  reached a self-sustaining speed (fig. 11-2).
        engine to be started in the minimum time and, when
        possible, to be completely independent of external  6. The electrical supply may be of a high or low
        equipment. A commercial aircraft, however, requires  voltage and is passed through a system of relays and
        the engine to be started with the minimum         resistances to allow the full voltage to be progres-
        disturbance to the passengers and by the most     sively built up as the starter gains speed. It also
        economical means. Whichever system is used,       provides the power for the operation of the ignition
        reliability is of prime importance.
                                                          system.  The electrical supply is automatically
        4. The starter motor must produce a high torque   cancelled when the starter load is reduced after the
        and transmit it to the engine rotating assembly in a  engine has satisfactorily started or when the time
        manner that provides smooth acceleration from rest  cycle is completed.  A typical electrical starting
        up to a speed at which the gas flow through the   system is shown in fig. 11-3.















































        Fig. 11-2  An electric starter.

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