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The aircraft landing gear is a complex multi-degree of freedom dynamic system, and may encounter vibration or dynamic response problems induced by braking action. The vibratory modes can be induced by brake and tire-ground frictional characteristics, antiskid operation, brake design features, landing gear design features, and tire characteristics. The impact of this vibration can range from catastrophic failure of critical system components or entire landing gears, to fatigue of small components, to passenger annoyance. It is therefore important that the vibration is assessed during the design concept phase, and verified during the development and testing phases of the system hardware.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2016-11-16 |
| ICS | 49.045 : Structure and structure elements
|
| Number of pages | 36 |
| Replace | SAE AIR 1064C:2006-03-17 |
| Set | AEROPAKS10U-10 |
| Year | 2016 |
| Document history | SAE AIR 1064C:2006-03-17 |
| Country | USA |
| Keyword | SAE 1064;SAE AIR1064D;SAE AIR1064D;SAE AIR 1064 |