Design of Typical Aviation Titanium Alloy Benchmark

Peng Fei Ma; Sheng Zhang Wang; Wei Zhao

doi:10.4028/www.scientific.net/MSF.836-837.536

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Dynamic Characteristic Analysis of CNC Turret Punch Servo Beam
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Design of Typical Aviation Titanium Alloy Benchmark
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The Design of Automatic System for the Calibration of Testing Temperature Cutter with Thin Film Thermocouple
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HomeMaterials Science ForumMaterials Science Forum Vols. 836-837Design of Typical Aviation Titanium Alloy...

Design of Typical Aviation Titanium Alloy Benchmark

Abstract:

As technology develops, the aviation structures become more and more complex and consist of more difficult-to-machine features. In order to evaluate the cutting tool performance, it is necessary to design a testing thin-walled benchmark with some typical difficult-to-machine features which are extracted from complex integrated components used in aviation. Firstly, the models with different typical features were designed and optimized using UG NX. Then, based on the analysis of process of typical features, the specific processing strategies of testing benchmarks were proposed. Finally, the process was analog simulated with CAM to evaluate whether it was qualified for machining. The results would make preparations for the evaluation of different cutting tool performance.

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Periodical:

Materials Science Forum (Volumes 836-837)

Pages:

536-542

DOI:

https://doi.org/10.4028/www.scientific.net/MSF.836-837.536

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Online since:

January 2016

Authors:

Peng Fei Ma, Sheng Zhang Wang, Wei Zhao*

Keywords:

Benchmark, Process Optimization, Thin-Walled Structures, Titanium Alloy

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* - Corresponding Author

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