GE Aircraft Engines
In construction of several different stages of stator compressor fin assemblies used in a number of GE aircraft engines, the placement of each fin in relation to the assembly needs to be ascertained very precisely. The fixtures used for this measurement process were completely redesigned to increase the rate at which these measurements can be taken as well as improve the ergonomics. Analyses were conducted to validate the design and a prototype fixture was constructed for evaluation.
Worcester Polytechnic Institute
Major Qualifying Project
Access to this report is limited to members of the WPI community. Please contact a project advisor or their department to request access
Restricted-WPI community only