Page 41 - The Jet Engine
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Compressors

















































                     Fig. 3-17 A pneumatically operated bleed valve system.

                      32. For casing designs the need is for a light but  damage. Earlier designs specified aluminium alloys
                      rigid construction enabling blade tip clearances to be  but because of its inferior ability to withstand damage
                      accurately maintained ensuring the highest possible  its use has declined. Titanium may be used for stator
                      efficiency.  These needs are achieved by using   vanes in the low pressure area but is unsuitable for
                      aluminium at the front of the compression system  the smaller stator vanes further rearwards in the
                      followed by .alloy steel as compression temperature  compression system because of the higher
                      increases. Whilst for the final stages of the    pressures and temperatures encountered.  Any
                      compression system, where temperature require-   excessive rub which may occur between rotating and
                      ments possibly exceed the capability of the best  static components as a result of other mechanical
                      steel, nickel based alloys may be required. The use  failures, can generate sufficient heat from friction to
                      of titanium in .preference to aluminium and steel is  ignite the titanium. This in turn can lead to expensive
                      now more common; particularly in military engines  repair costs and a possible airworthiness hazard.
                      where its high rigidity to density ratio can result in
                      significant weight reduction. With the development of  34. In the design of rotor discs, drums and blades,
                      new manufacturing methods component costs can    centrifugal forces dominate and the requirement is
                      now be maintained at a more acceptable level in  for metal with the highest ratio of strength to density.
                      spite of high initial material costs.            This results in the lightest possible rotor assembly
                                                                       which in turn reduces the forces on the engine
                      33. Stator vanes are normally produced from steel  structure enabling a further reduction in weight to be
                      or nickel based alloys, a prime requirement being a  obtained. For this reason, titanium even with its high
                      high fatigue strength when "notched" by ingestion  initial cost is the preferred material and has replaced

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