| 摘要 |
<p>A monitoring system for detecting and indicating typical operating conditions, particularly vibration of an aircraft engine, wherein at least two measuring feelers (A, B), such as accelerometers are exposed to the same conditions, the output signals from said feeler are compared with each other and logical means (21, 29, 35) detect normal conditions when the output signals are equal, system defect conditions when the output signals differ from each other and alarm conditions when the output signals both exceed a safety limit. Such a system greatly increases the reliability and at the same time avoids false alarms.</p> |
