Fatigue Damage Spectrum calculation in a Mission Synthesis procedure for Sine-on-Random excitations

13th International Conference on Motion and Vibration Control; 12th International Conference on Recent Advances in Structural Dynamics

Angeli, Andrea^1 ; Cornelis, Bram^2 ; Troncossi, Marco^1

DIN - Dept. of Engineering for Industry, University of Bologna, Italy^1

Siemens Industry Software NV, Leuven, Belgium^2

关键词: Accumulated fatigue damage;    Electronic component;    Random excitations;    Sinusoidal components;    Spectrum calculation;    Synthesis procedure;    Time-domain approach;    Vibration environment;   

Others  :  https://iopscience.iop.org/article/10.1088/1742-6596/744/1/012089/pdf
DOI  :  10.1088/1742-6596/744/1/012089

来源: IOP

【 摘 要 】

In many real-life environments, certain mechanical and electronic components may be subjected to Sine-on-Random vibrations, i.e. excitations composed of random vibrations superimposed on deterministic (sinusoidal) contributions, in particular sine tones due to some rotating parts of the system (e.g. helicopters, engine-mounted components,...). These components must be designed to withstand the fatigue damage induced by the "composed" vibration environment, and qualification tests are advisable for the most critical ones. In the case of an accelerated qualification test, a proper test tailoring which starts from the real environment (measured vibration signals) and which preserves not only the accumulated fatigue damage but also the "nature" of the excitation (i.e. sinusoidal components plus random process) is important to obtain reliable results. In this paper, the classic time domain approach is taken as a reference for the comparison of different methods for the Fatigue Damage Spectrum (FDS) calculation in case of Sine-on-Random vibration environments. Then, a methodology to compute a Sine-on-Random specification based on a mission FDS is proposed.