Acoustic event monitoring for triggering of health scan of a structure
First Claim
1. A system for monitoring an aircraft structure, the system comprising:
- an optical fiber network extending along an aircraft structure;
an optical emitter optically coupled to the optical fiber network and configured to generate an optical signal and to transmit the generated optical signal to the optical fiber network;
a series of optical acoustic transducers optically coupled to the optical fiber network and mechanically coupled to the aircraft structure at a series of acoustic sensor locations, each of the series of optical acoustic transducers configured to receive the generated optical signal, to generate an optical response signal indicative of a detected passive acoustic condition at a respective acoustic sensor location, and to transmit the generated optical response signal to the optical fiber network;
an optical detector optically coupled to the optical fiber network and configured to receive the transmitted optical response signals generated by the series of optical acoustic transducers; and
a controller configured to generate a trigger signal configured to trigger an active health monitor scan, if a triggering one of the received optical response signals is indicative of a triggering acoustic event, the controller further configured to determine, based on a relative timing of the triggering one of the received optical response signals, a specific one of the acoustic sensor locations associated with a specific one of the series of optical acoustic transducers that generated the triggering one of the optical response signals associated with the generated trigger signal.
1 Assignment
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Accused Products
Abstract
Apparatus and associated methods relate to generating a trigger signal in response to detection of a triggering acoustic event sensed by one of a distributed network of optical acoustic sensors mechanically coupled to an aircraft structure. Each of the optical acoustic sensors is configured to generate an optical response signal indicative of an acoustic condition detected by the optical acoustic sensor. A controller receives the optical response signals and generates, if a triggering one of the optical response signals is indicative of a triggering acoustic event, a trigger signal. The controller also determines a location of the specific one of the distributed network of optical acoustic sensors that generated the triggering one of the optical response signals. In some embodiments, the trigger signal is sent to a Health & Usage Monitoring System configured to perform a health scan, in response to receiving the trigger signal, of the aircraft structure.
17 Citations
20 Claims
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1. A system for monitoring an aircraft structure, the system comprising:
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an optical fiber network extending along an aircraft structure; an optical emitter optically coupled to the optical fiber network and configured to generate an optical signal and to transmit the generated optical signal to the optical fiber network; a series of optical acoustic transducers optically coupled to the optical fiber network and mechanically coupled to the aircraft structure at a series of acoustic sensor locations, each of the series of optical acoustic transducers configured to receive the generated optical signal, to generate an optical response signal indicative of a detected passive acoustic condition at a respective acoustic sensor location, and to transmit the generated optical response signal to the optical fiber network; an optical detector optically coupled to the optical fiber network and configured to receive the transmitted optical response signals generated by the series of optical acoustic transducers; and a controller configured to generate a trigger signal configured to trigger an active health monitor scan, if a triggering one of the received optical response signals is indicative of a triggering acoustic event, the controller further configured to determine, based on a relative timing of the triggering one of the received optical response signals, a specific one of the acoustic sensor locations associated with a specific one of the series of optical acoustic transducers that generated the triggering one of the optical response signals associated with the generated trigger signal. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A method for monitoring health of an aircraft structure, the method comprising:
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extending an optical fiber network along an aircraft structure; generating, an optical signal; transmitting the generated optical signal to the optical fiber network; detecting, via a series of optical acoustic transducers mechanically coupled to the aircraft structure at a series of acoustic sensor locations along the optical fiber network, passive acoustic conditions at the series of acoustic sensor locations; receiving, via the series of optical acoustic transducers, the transmitted optical signal; generating, in response to receiving the transmitted optical signal via the series of optical acoustic transducers, optical response signals indicative of the detected passive acoustic conditions; transmitting, via the series of optical acoustic transducers, the generated optical response signals to the optical fiber network; receiving, via an optical detector, the transmitted optical signals; generating, via a controller, a trigger signal configured to trigger an active health monitor scan, if a triggering one of the received optical response signals is indicative of a triggering acoustic event; and determining, based on a relative timing of the triggering one of the received optical response signals via the controller, a specific one of the acoustic sensor locations associated with a specific one of the series of optical acoustic transducers that generated the triggering one of the optical response signals associated with the generated trigger signal. - View Dependent Claims (13, 14, 15, 16, 17, 18, 19, 20)
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Specification