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Project Goals
  • Development of standard procedure for definition of process parameter windows for the manufacture of critical aero engine components

  • Develop methods whereby components manufactured within the process parameter window can be validated to meet demands of design and surface integrity requirements

  • Provide manufacturing with a new methodology that will allow significant reduction in recurring validation costs

  • Develop a novel standard procedure for adaptive control that is based on process monitoring techniques and will take account of factors responsible for producing variable part quality

  • Provide aero engine manufacture with a methodology that can be adapted to individual company procedures that will allow the design and manufacture of critical components to be optimised