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- W2364741021 abstract "It is well know that the best way to manage the life of aircraft is to monitor fatigue consumption of each aircraft, which is very popular among western countries. However, it has not been applied in China, due to the shortage of reliable fatigue meters. With more and more new types of aircraft going to service, the situation has changed. It is possible now to manage the life of aircraft by monitoring its fatigue damage consumption, as each of new type of aircraft is equipped with flight parameter recorder. One of the most important aspects for monitoring aircraft fatigue consumption is to find a suitable method for calculating fatigue damage by using recorded flight parameters. Although many methods are available for calculating fatigue damage, none of those has been accepted. As the Miner theory is expressed in a very simple mathematics formula, it choice material constant m because there are big difference among the calculated results by using different value of the m.A method based on the relative Miner theory for calculating fatigue damage of aircraft is presented. A systematical study is carried out by calculating more than 30?000 hours of flight data recorded from 60 aircrafts of two types, from which a conclusion is drawn that the order of fatigue damage values calculated by this method for all aircrafts in one fleet are same no matter what value of material constant m is chosen. Therefore it is proven that this method is a valuable tool for monitoring aircraft fatigue consumptions." @default.
- W2364741021 created "2016-06-24" @default.
- W2364741021 creator A5081500655 @default.
- W2364741021 date "2004-01-01" @default.
- W2364741021 modified "2023-09-23" @default.
- W2364741021 title "ENGINEERING ANALOGY METHOD FOR CALCULATING STRUCTURAL FATIGUE DAMAGE OF AIRCRAFT" @default.
- W2364741021 hasPublicationYear "2004" @default.
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