Embedded optical probe for gas turbine engine
An optical probe for a gas turbine engine includes a housing. Also included is a plurality of optical fibers, a portion of each of the optical fibers secured to fiber holders. Further included is an optical head disposed within the housing and having channels extending in a longitudinal direction of the optical head, the fiber holders disposed within the channels. Yet further included is a cap disposed within the housing and operatively coupled to the optical head, the plurality of optical fibers extending through the cap. Also included is an inner tube operatively coupled to the cap, the plurality of fibers extending through the inner tube.
1. An optical probe for a gas turbine engine comprising:
a housing;
a plurality of optical fibers, a portion of each of the optical fibers secured to fiber holders;
an optical head disposed within the housing and having channels extending in a longitudinal direction of the optical head, the fiber holders disposed within the channels;
a cap disposed within the housing and operatively coupled to the optical head, the plurality of optical fibers extending through the cap;
an inner tube operatively coupled to the cap, the plurality of fibers extending through the inner tube; and
an outer tube surrounding a portion of the inner tube to define an annulus therebetween, that allows for cooling air to be routed therethrough or to purge the interior of the housing, the outer tube operatively coupled to the housing.
2. The optical probe of claim 1 , wherein the outer tube is brazed to the housing.
3. The optical probe of claim 1 , wherein an axial position of the optical head is fixed with an optical head retention pin extending through the housing and into the optical head.
4. The optical probe of claim 1 , wherein the optical head defines a plurality of holes proximate the fiber holders to secure the fiber holders thereto with an adhesive.
5. The optical probe of claim 1 , wherein a forward end of the optical head is disposed within a view window defined by the housing.
6. The optical probe of claim 5 , further comprising a mirror operatively coupled to the housing within the view window.
7. The optical probe of claim 6 , wherein the mirror is operatively coupled to the housing with a mirror retention pin extending through the housing and into the mirror.
8. The optical probe of claim 1 , wherein the cap is welded to the optical head.
9. The optical probe of claim 1 , wherein the cap is brazed to the inner tube.
10. The optical probe of claim 1 , wherein the cap includes channels for fluidly coupling the annulus defined by the inner and outer tubes with an interior of the optical head.
11. A gas turbine engine comprising:
a flow separation wall separating a first flow path from a second flow path; and
an optical probe embedded within the flow separation wall, the optical probe comprising:
a housing, the housing operatively coupled to the flow separation wall;
a plurality of optical fibers, a portion of each of the optical fibers secured to fiber holders;
an optical head disposed within the housing and having channels extending in a longitudinal direction of the optical head, the fiber holders disposed within the channels;
a cap disposed within the housing and operatively coupled to the optical head, the plurality of optical fibers extending through the cap;
an inner tube operatively coupled to the cap, the plurality of fibers extending through the inner tube; and
an outer tube surrounding a portion of the inner tube to define an annulus therebetween, that allows for cooling air to be routed therethrough or to purge the interior of the housing, the outer tube operatively coupled to the housing.
12. The gas turbine engine of claim 11 , wherein the housing includes at least one flange and a main body portion, the main body portion defining an interior of the housing.
13. The gas turbine engine of claim 12 , wherein the at least one flange is welded to the flow separation wall.
14. The gas turbine engine of claim 11 , wherein the optical probe is completely embedded within the flow separation wall.
15. The gas turbine engine of claim 11 , wherein the cap is welded to the optical head.
16. The gas turbine engine of claim 11 , wherein the cap is brazed to the inner tube.
17. The gas turbine engine of claim 11 , wherein the cap includes channels for fluidly coupling the annulus defined by the inner and outer tubes with an interior of the optical head.