Aircraft overheat detection using optical fiber technology for system health monitoring by determining a physical characteristic associated with a location
Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
1. A health monitoring system of an aircraft, the system comprising:
a first fiber optic cable routed through at least one zone of the aircraft;
an optical transmitter configured to provide an optical signal to the first fiber optic cable;
an optical receiver configured to receive an optical response from the first fiber optic cable; and
a controller operatively connected to the optical receiver and configured to determine for the at least one zone a physical characteristic and a location associated with the physical characteristic based on the optical response, store a plurality of values of the physical characteristic and the location associated with the physical characteristic over a time period in a memory to generate trend data, and communicate the trend data to maintenance personnel to facilitate determination that a maintenance action is required.
2. The system of claim 1 , wherein the first fiber optic cable includes fiber Bragg gratings.
3. The system of claim 2 , wherein the controller is configured to control the optical transmitter and determine the physical characteristic for the at least one zone using time division multiplexing (TDM) and/or wavelength division multiplexing (WDM).
4. The system of claim 1 , further comprising:
a second fiber optic cable routed through the at least one zone parallel to the first fiber optic cable;
wherein the controller is configured to provide a reference signal to the second fiber optic cable and receive a reference response from the second fiber cable.
5. The system of claim 4 , wherein the controller is configured to determine the physical characteristic based upon the reference response, the optical response, and coherent optical frequency domain reflectometry (COFDR).
6. The system of claim 5 , wherein the first and second fiber optic cables include fiber Bragg gratings.
7. The system of claim 1 , wherein the optical transmitter is configured to produce laser pulses with a constant amplitude, and wherein the controller implements Incoherent Optical Frequency Domain Reflectometry (IOFDR) with a step frequency or swept frequency methodology.
8. The system of claim 1 , wherein the controller is configured to control the optical transmitter to provide the optical signal as a single laser pulse at a fixed wavelength, and wherein the controller is configured to determine the physical characteristic of the at least one zone using optical time domain reflectometry (OTDR).
9. The system of claim 1 , wherein the optical transmitter is connected to provide the optical signal to a first end of the first fiber optic cable and the optical receiver is connected to receive the optical response from a second end of the first fiber optic cable, and wherein the system further comprises:
a probe transmitter connected to the second end of the first fiber optic cable and configured to provide a probe signal to the second end of the first fiber optic cable; and
a probe receiver connected to the first end of the first fiber optic cable and configured to receive the probe signal from the first end of the first fiber optic cable;
wherein the controller is configured to determine the physical characteristic of the at least one zone based on a frequency difference between the optical response and the probe response using Brillouin optical time domain analysis (BOTDA).
10. The system of claim 1 , wherein the at least one zone is one of a bleed air duct, cross-over bleed air duct, wheel well, wing box, air conditioning system, anti-icing system or nitrogen generation system.
11. The system of claim 1 , wherein the physical characteristic is a temperature or a strain.
12. A method of monitoring the health of an aircraft, the method comprising:
emitting, by an optical transmitter, an optical signal to a first fiber optic cable, wherein the first fiber optic cable is routed through at least one zone of the aircraft;
receiving, by an optical receiver, a response signal from the first fiber optic cable based upon the optical signal;
determining for the at least one zone, using a controller, a physical characteristic and a location associated with the physical characteristic;
storing, in a memory, a plurality of values of the physical characteristic and the location associated with the physical characteristic for the at least one zone;
determining a trend for the physical characteristic and the location associated with the physical characteristic based on the plurality of values; and
communicating the trend for the physical characteristic and the location associated with the physical characteristic to maintenance personnel to facilitate determination that a maintenance action is required.
13. The method of claim 12 , wherein the first fiber optic cable includes fiber Bragg gratings, and wherein emitting, by the optical transmitter, the optical signal comprises emitting the optical signal using a tunable, swept-wavelength laser; and wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic based on wavelength division multiplexing (WDM).
14. The method of claim 12 , wherein the first fiber optic cable includes fiber Bragg gratings, and wherein emitting, by the optical transmitter, the optical signal comprises emitting the optical signal using a broadband laser; and wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic based on time division multiplexing (TDM).
15. The method of claim 12 , wherein emitting, by the optical transmitter, the optical signal comprises emitting laser pulses having a constant amplitude using a step frequency methodology; and wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic based on optical frequency domain reflectometry (IOFDR).
16. The method of claim 12 , wherein emitting, by the optical transmitter, the optical signal comprises emitting laser pulses having a constant amplitude using a swept frequency methodology; and wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic based on optical frequency domain reflectometry (IOFDR).
17. The method of claim 12 , further comprising:
providing a reference signal to a second fiber optic cable configured to run parallel to the first fiber optic cable through the at least one zone; and
receiving a reference response from the second fiber cable based on the reference signal;
wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic based upon the reference response, the optical response, and coherent optical frequency domain reflectometry (COFDR).
18. The method of claim 17 , wherein the first and second fiber optic cables include fiber Bragg gratings.
19. The method of claim 12 , wherein emitting, by the optical transmitter, the optical signal comprises emitting the optical signal as a single laser pulse at a fixed wavelength, and wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic of the at least one zone using optical time domain reflectometry (OTDR).
20. The method of claim 12 , wherein emitting, by the optical transmitter, the optical signal comprises emitting the optical signal to a first end of the first fiber optic cable, and wherein receiving, by the optical receiver, the response signal comprises receiving the optical response from a second end of the first fiber optic cable, and wherein the method further comprises:
providing, by a probe transmitter, a probe signal to the second end of the first fiber optic cable; and
receiving, by a probe receiver, a probe response from the first end of the first fiber optic cable;
wherein determining, using the controller, the physical characteristic of the at least one zone comprises determining the physical characteristic of the at least one zone based on a frequency difference between the optical response and the probe response using Brillouin optical time domain analysis (BOTDA).