'The University of Texas at Austin, Bureau of Economic Geology'
Abstract
For aircraft engine manufacturers the technology of AM appears promising. AM provides
the opportunity for a highly flexible and a cost effective part production. Furthermore AM offers
new potentials and possibilities for lightweight designs. The implementation and applications of
AM can be divided in three different strategic application levels. The first level includes
manufacturing simple existing parts; these kinds of parts are already in production. In the second
level, new design tools, such as structural optimization, are used to improve an existing part by
benefiting from the new design freedom but without changing its functionality. The third level
includes novel parts with new functionality.
This paper presents design methods for AM parts for the second and third level:
performance and solution based approach, respectively. Also the safety classification of engine
parts is looked into. Step-by-step design methods are presented, accompanied by case studies that
demonstrate improvement to the initial design: a light weight, topology optimized turbine guide
vane (level two) and an aircraft engine casing design that has an improved tip clearance behavior
under transient operating cycles (level three).Mechanical Engineerin