Design of an adaptive fixturing system for aerospace component machining
An aircraft engine has numerous components like fuel lines, combustion chamber, turbine and compressor rotor stator blades and honeycomb segments, where constant maintenance and repair need to be carried out in escalating the life time of these parts. The part families of turbine Outer Air Seal (...
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Format: | Theses and Dissertations |
Language: | English |
Published: |
2016
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Online Access: | http://hdl.handle.net/10356/68655 |
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Institution: | Nanyang Technological University |
Language: | English |
Summary: | An aircraft engine has numerous components like fuel lines, combustion chamber,
turbine and compressor rotor stator blades and honeycomb segments, where constant
maintenance and repair need to be carried out in escalating the life time of these parts.
The part families of turbine Outer Air Seal (OAS) normally have different stages and
have unique common features for datuming as well as repairing. In order to perform
repair operations on these parts, a significant amount of time has to be spent in design
and fabrication of dedicated fixtures for the particular stage which eventually increases
the fixtures count.
After a detailed review on the various flexible fixturing systems, vacuum based fixtures
were found to be more suitable when compared to the other systems. Vacuum fixtures
offers high degree of flexibility, low set up time and effective clamping ability on the
OAS parts. The fixturing method consists of a common base plate designed in such a
way that it could be easily fastened on any machining bed in different orientations for
chiseling and milling operations. Due to the dimensional constrain of the OAS stages,
individual vacuum chucks were designed accordingly in such a way it can be easily
mounted on to the base plate using dowel pins and fasteners. Vacuum suction and
mechanical clamps were employed to clamp the workpiece rigidly on the vacuum
chuck. The fixture components were analyzed using FEA packages, to determine the
exactness of fixturing dimensions and boundary conditions assumed. This design
methodology reduced the tooling count from six to one. The set up time is reduced
considerably and the initial tooling cost is reduced by 43% when compared to the
existing fixturing method. |
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