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| Loads Decomposition Method for LRM |
| Received:January 15, 2016 Revised:June 15, 2016 |
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| DOI：10.7643/ issn.1672-9242.2016.03.019 |
| KeyWord:integrated modular avionics LRM vibration loads decomposition temperature loads decomposition |
| Author | Institution |
| LU Liang |
The 10th Research Institute of CETC, Chengdu , China |
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| Abstract: |
| Objective Based on the properties of integrated modular avionics equipment, the method of loads decomposition for LRM was studied. Methods By simulation and test method, the temperature and vibration load of LRM were decomposed, and the realization process of both methods was discussed in detail. Result The module loads decomposition method was successfully applied in an engineering project, and the validity of methods was verified. Conclusion The method of LRM module loads decomposition can be used to guide the loads decomposition of other similar integrated modular avionics equipment, and at the same time to promote the reasonable independent environment test and delivery of LRM module. |
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