| 摘要 |
The present invention relates to a system for monitoring the health of mechanical and structure components of a machine. For example, the present invention is capable of monitoring the operational integrity of critical components of critical components of an aircraft such as the gearbox of a helicopter. The present invention is based on the principle of detecting a traceable substance when the substance is released from the component being monitored in the event of predetermined condition being satisfied, such as exceeding the operational temperature of the component, or a fault in the component occurring, such as a crack being formed.
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