Page 174 - The Jet Engine
P. 174

Thrust reversal





        11. The clamshell doors are operated by pneumatic  Cold stream reverser system
        rams through levers that give the maximum load to  15. The cold stream reverser system (fig. 15-4) can
        the doors in the forward thrust position; this ensures  be actuated by an air motor, the output of which is
        effective sealing at the door edges, so preventing  converted to mechanical movement by a series of
        gas leakage.  The door bearings and operating     flexible drives, gearboxes and screwjacks, or by a
        linkage operate without lubrication at temperatures of  system incorporating hydraulic rams.
        up to 600 deg. C.
                                                          16. When the engine is operating in forward thrust,
        Bucket target system                              the cold stream final nozzle is 'open' because the
        12. The bucket target system is hydraulically     cascade vanes are internally covered by the blocker
        actuated and uses bucket-type doors to reverse the  doors (flaps) and externally by the movable
                                                          (translating) cowl; the latter item also serves to
        hot gas stream.  The thrust reverser doors are    reduce drag.
        actuated by means of a conventional pushrod
        system.  A single hydraulic powered actuator is   17. On selection of reverse thrust, the actuation
        connected to a drive idler, actuating the doors   system moves the translating cowl rearwards and at
        through a pair of pushrods (one for each door).   the same time folds the blocker doors to blank off the
                                                          cold stream final nozzle, thus diverting the airflow
        13. The reverser doors are kept in synchronization  through the cascade vanes.
        through the drive idler. The hydraulic actuator incor-
        porates a mechanical lock in the stowed (actuator  Turbo-propeller reverse pitch system
        extended) position.                               18. As mentioned in para. A, reverse thrust action is
                                                          affected on turbo-propeller powered aircraft by
        14. In the forward thrust mode (stowed) the thrust  changing the pitch of the propeller blades through a
        reverser doors form the convergent-divergent final  hydro-mechanical pitch control system (fig. 15-5).
        nozzle for the engine.                            Movement of the throttle or power control lever







































        Fig. 15-5  A propeller pitch control system.

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