An integrated method for optimization of a welded portion of a high pressure compressor rotor as a single object is developed. The minimum mass criterion is used in the optimization method; limitations are imposed in accordance with strength and stiffness requirements. An example is given of optimization of a typical welded portion of a high pressure compressor rotor resulting in mass reduction and increase of cyclic durability.
Optimization of a Welded Portion of the High Pressure Compressor Rotor
Russ. Aeronaut.
Russian Aeronautics ; 63 , 1 ; 117-125
2020-01-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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