Page 134 - The Jet Engine
P. 134

Starting and ignition










































        Fig. 11-4  A triple-breech cartridge starter.


        Cartridge                                         air pump scavenges the starter combustion chamber
        7. Cartridge starting is sometimes used on military  of fumes before each start. Operation of the fuel and
        engines and provides a quick independent method of  air pumps, ignition systems, and cycle cancellation,
        starting.  The starter motor is basically a small  is electrically controlled by relays and time switches.
        impulse-type turbine that is driven by high velocity  An iso-propyl-nitrate starting system is shown in fig.
        gases from a burning cartridge. The power output of  11-5.
        the turbine is passed through a reduction gear and
        an automatic disconnect mechanism to rotate the   Air
        engine.  An electrically fired detonator initiates the  9. Air starting is used on most commercial and
        burning of the cartridge charge. As a cordite charge  some military jet engines. It has many advantages
        provides the power supply for this type of starter, the  over other starting systems, and is comparatively
        size of the charge required may well limit the use of  light, simple and economical to operate.
        the cartridge starters.  A triple-breech starter is  10. An air starter motor transmits power through a
        illustrated in fig. 11-4.                         reduction gear and clutch to the starter output shaft
                                                          which is connected to the engine. A typical air starter
        Iso-propyl-nitrate                                motor is shown in fig. 11-6.
        8. This type of starter provides a high power output
        and gives rapid starting characteristics. It has a  11. The starter turbine is rotated by air taken from
        turbine that transmits power through a reduction gear  an external ground supply, an auxiliary power unit
        to the engine. In this instance, the turbine is rotated  (A.P.U.) or as a cross-feed from a running engine.
        by high pressure gases resulting from the         The air supply to the starter is controlled by an elec-
        combustion of iso-propyl-nitrate. This fuel is sprayed  trically operated control and pressure reducing valve
        into a combustion chamber, which forms part of the  that is opened when an engine start is selected and
        starter, where it is electrically ignited by a high-  is automatically closed at a predetermined starter
        energy ignition system. A pump supplies the fuel to  speed. The clutch also automatically disengages as
        the combustion chamber from a storage tank and an  the engine accelerates up to idling r.p.m. and the

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