タイトル | Aging commuter aeroplanes: Fatigue evaluation and control methods |
著者(英) | Emmerson, A. J. |
著者所属(英) | Civil Aviation Authority |
発行日 | 1992-07-01 |
言語 | eng |
内容記述 | The loss of reliability in aircraft is caused by two broad classes of problems. There are those problems which are self evident and hazardous rather than catastrophic. These are the problem areas where characteristically there have been multiple overhauls, repairs, and replacements, and where aging really means the results of repair ineffectiveness that accumulates. The other class of the problem is the insidious and potentially catastrophic class. It includes the progressive deterioration of items that are not maintained, and often cannot be maintained because the deterioration cannot be seen. It includes the loss of physical properties in adhesives and other organic compounds, corrosion, and the response of repeated loads. Dealt with here is a currently unnecessarily troublesome aspect of that response. Although we must remain concerned about those types of aircraft which have been certified under a design standard or operational rule which embodies the elementary fail-safe concept and which have not been subjected to a subsequent structural audit, the focus here is on types of aircraft for which fatigue and damage tolerance evaluation was not required as a condition of certification. |
NASA分類 | STRUCTURAL MECHANICS |
レポートNO | 92N30132 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/230892 |
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