Page 138 - The Jet Engine
P. 138

Starting and ignition





                                                          give outputs which may vary according to require-
                                                          ments.  A high value output (e.g. twelve joule) is
                                                          necessary to ensure that the engine will obtain a sat-
                                                          isfactory relight at high altitudes and is sometimes
                                                          necessary for starting. However, under certain flight
                                                          conditions, such as icing or take-off in heavy rain or
                                                          snow, it may be necessary to have the ignition
                                                          system continuously operating to give an automatic
                                                          relight should flame extinction occur. For this
                                                          condition, a low value output (e.g. three to six joule)
                                                          is preferred because it results in a longer life of the
                                                          igniter plug and ignition unit. Consequently, to suit all
                                                          engine operating conditions, a combined system
                                                          giving a high and low value output is favoured. Such
                                                          a system would consist of one unit emitting a high
                                                          output to one igniter plug, and a second unit giving a
                                                          low output to a second igniter plug. However, some
                                                          ignition units are capable o! supplying both high and
                                                          low outputs, the value being pre-selected as
                                                          required.
        Fig. 11-8  Air impingement starting.














































        Fig. 11-9  A gas turbine starter.

        128
   133   134   135   136   137   138   139   140   141   142   143