Optical monitoring system for a gas turbine engine
A system for optically monitoring a gas turbine engine includes an optical multiplexer configured to receive multiple images from respective viewports into the gas turbine engine. The optical multiplexer includes a movable reflective device configured to selectively direct at least a portion of each image toward a detector array, and the detector array is directed toward a fixed location on the optical multiplexer.
1. A monitoring system for optically monitoring a gas turbine system, comprising:
an optical multiplexer configured to receive a plurality of images from a respective plurality of viewports into the gas turbine system, wherein the optical multiplexer comprises a movable reflective device situated outside of the gas turbine system and configured to selectively direct at least a portion of each image toward a detector array, wherein the reflective device comprises a mirror or a prism, and wherein the detector array is directed toward a fixed location on the optical multiplexer.
2. The monitoring system of claim 1 , wherein the reflective device is configured to translate between a first position that directs at least a portion of a first image toward the detector array and a second position that directs at least a portion of a second image toward the detector array.
3. The monitoring system of claim 1 , comprising an infrared camera having the detector array, wherein the detector array is configured to detect short-wave infrared images, mid-wave infrared images, or a combination thereof.
4. The monitoring system of claim 1 , comprising a plurality of optical connections configured to convey each image from the respective viewport to the optical multiplexer.
5. The monitoring system of claim 1 , wherein the optical multiplexer comprises a plurality of lenses configured to focus each respective image onto the detector array via the reflective device.
6. The monitoring system of claim 1 , wherein the reflective device is configured to rotate between a first position that directs at least a portion of a first image toward the detector array and a second position that directs at least a portion of a second image toward the detector array.
7. The monitoring system of claim 6 , wherein the monitoring system is configured to rotate the reflective device to the first position for a first duration and to the second position for a second duration.
8. The monitoring system of claim 6 , wherein the monitoring system is configured to continuously rotate the reflective device through the first and second positions.
9. A monitoring system for optically monitoring a gas turbine system, comprising:
a detector array; and
an optical multiplexer configured to receive a first image from a first viewport into the gas turbine system and to receive a second image from a second viewport into the gas turbine system, wherein the optical multiplexer comprises a movable reflective device situated outside of the gas turbine system and configured to selectively move between a first position that directs at least a portion of the first image toward the detector array and a second position that directs at least a portion of the second image toward the detector array, and wherein the reflective device comprises a mirror or a prism;
wherein the detector array is directed toward a fixed location on the optical multiplexer.
10. The monitoring system of claim 9 , comprising an infrared camera having the detector array, wherein the detector array is configured to detect short-wave infrared images, mid-wave infrared images, or a combination thereof.
11. The monitoring system of claim 9 , wherein the detector array is configured to detect multidimensional images.
12. The monitoring system of claim 9 , wherein the monitoring system is configured to monitor the gas turbine system while the gas turbine system is in operation.
13. A monitoring system for optically monitoring a gas turbine system, comprising:
a detector array;
an optical multiplexer configured to receive a first image from a first viewport into the gas turbine system and to receive a second image from a second viewport into the gas turbine system, wherein the optical multiplexer comprises a movable reflective device configured to selectively direct at least a portion of each image toward the detector array; and
a controller configured to instruct the reflective device to move between a first position that directs at least a portion of the first image toward the detector array and a second position that directs at least a portion of the second image toward the detector array;
wherein the detector array is directed toward a fixed location on the optical multiplexer,
wherein the gas turbine system comprises a compressor, a combustor, a turbine, an intake, and an exhaust, and wherein the first and second viewports are positioned to enable viewing of images from at least one of the compressor, the combustor, the turbine, the intake, and the exhaust.
14. The monitoring system of claim 13 , wherein the controller is configured to instruct the reflective device to rotate to the first position for a first duration and to the second position for a second duration.
15. The monitoring system of claim 13 , wherein the controller is configured to instruct the reflective device to continuously rotate through the first and second positions.
16. The monitoring system of claim 13 , wherein the controller is configured to instruct the reflective device to translate to the first position for a first duration and to the second position for a second duration.