METHOD AND SYSTEM FOR MANUFACTURING A STAGE-TRANSITION STRUCTURE FOR AN AEROSPACE TURBINE USING IN-LINE MULTISENSOR METROLOGY

摘要

Technical description: method for manufacturing structural components of an aerospace turbine, which combines processes, materials, tools and machining techniques and is characterised by: a numerically controlled manufacturing cell with tool capacity of at least five critical shafts for machining pieces with special shapes, geometries and dimensions; a multisensor metrology cell for the dimensional capture of the geometry of machined components, which is characterised by intelligent data capture in at least six degrees of freedom, multifactorial modelling and communication with an intelligent analysis server; intelligent analysis of metrological information, characterised by the use of intelligent algorithms and linear regression algorithms in real time for the optimisation of the quality and efficiency of the manufacturing process; and an engineering and design cell characterised by the capacity for design optimisation by means of simulations coordinated with said information analysis devices, generating multistage simulation–analysis cycles in the manufacturing process.