Page 75 - The Jet Engine
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7: Accessory drives





                                                              Contents                                       Page



                                                              Introduction                                      65
                                                              Gearboxes and drives                              65

                                                                 Internal gearbox
                                                                 Radial driveshaft
                                                                 Direct drive
                                                                 Gear train drive
                                                                 Intermediate gearbox
                                                                 External gearbox
                                                                 Auxiliary gearbox
                                                              Construction and materials                        69

                                                                 Gears
                                                                 Gearbox sealing
                                                                 Materials






                                                                       GEARBOXES AND DRIVES

                                                                       Internal gearbox
                                                                       3. The location of the internal gearbox within the
                                                                       core of an engine is dictated by the difficulties of
                                                                       bringing a driveshaft radially outwards and the space
                                                                       available within the engine core.
                      INTRODUCTION
                                                                       4. Thermal fatigue and a reduction in engine
                      1. Accessory units provide the power for aircraft  performance, due to the radial driveshaft disturbing
                      hydraulic, pneumatic and electrical systems in   the gasflow, create greater problems within the
                      addition to providing various pumps and control  turbine area than the compressor area. For any
                      systems for efficient engine operation. The high level  given engine, which incorporates an axial-flow
                      of dependence upon these units requires an       compressor, the turbine area is smaller than that
                      extremely reliable drive system.                 containing the compressor and therefore makes it
                                                                       physically easier to mount the gearbox within the
                      2. The drive for the accessory units is typically  compressor section. Centrifugal compressor engines
                      taken from a rotating engine shaft, via an internal  can have limited available space, so the internal
                      gearbox, to an external gearbox which provides a  gearbox may be located within a static nose cone or,
                      mount for the accessories and distributes the    in the case of a turbo-propeller engine, behind the
                      appropriate geared drive to each accessory unit. A  propeller reduction gear as shown in fig. 7-1.
                      starter may also be fitted to provide an input torque
                      to the engine. An accessory drive system on a high  5. On multi-shaft engines, the choice of which
                      by-pass engine takes between 400 and 500         compressor shaft is used to drive the internal
                      horsepower from the engine.                      gearbox is primarily dependent upon the ease of

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