Vane position sensor installation within a turbine case
A measuring system for sensing vane positions that comprises a turbine, a target, and a sensor. The turbine includes a plurality of articulating vanes, with each vane being coupled to a sync ring that is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring. The target is coupled to a first position of the turbine within a first region that is associated with a first vane of the plurality of articulating vanes. The sensor is coupled via a bracket to a second position of the turbine within the first region. The sensor is configured to detect an orientation of the target that corresponds to a vane position of the first vane.
1. A measuring system for sensing vane positions, comprising: a turbine including a plurality of articulating vanes, wherein each vane coupled to a sync ring, wherein the sync ring is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring; a target coupled to a first position within a first region, wherein the first position is associated with a first vane of the plurality of articulating vanes, wherein the first position is on a portion of the sync ring that is in association with a crank arm of the first vane thereby the target being mounted directly on the sync ring; a sensor coupled via a bracket to a second position within the first region, wherein the sensor is configured to detect an orientation of the target, wherein the orientation of the target corresponds to a vane position of the first vane, wherein the second position is on an outer turbine case wall of the turbine, wherein the bracket is physically coupled via one or more fasteners penetrating the outer turbine case wall.
2. The measuring system of claim 1 , wherein the first region is zone between the turbine case wall of the turbine and a turbine platform of the turbine.
3. The measuring system of claim 1 , wherein the turbine is a jet engine turbine employed by an aircraft.
4. The measuring system of claim 1 , wherein the sensor is selected from one of an eddy current sensor and a capacitive sensor.
5. The measuring system of claim 1 , wherein a metal compression seal is utilized to seal the one or more fasteners penetrating the outer turbine case wall.
6. A apparatus for sensing vane positions, comprising: a target coupled to a first position within a first region of a turbine, wherein the turbine includes a plurality of articulating vanes, wherein each vane coupled to a sync ring, wherein the sync ring is configured to position the plurality of articulating vanes in accordance with a degree of rotation by the sync ring, wherein the first position is associated with a first vane of the plurality of articulating vanes, wherein the first position is on a portion of the sync ring that is in association with a crank arm of the first vane thereby the target being mounted directly on the sync ring; and a sensor coupled via a bracket to a second position within the first region, wherein the sensor is configured to detect an orientation of the target, wherein the orientation of the target corresponds to a vane position of the first vane, wherein the second position is on an outer turbine case wall of the turbine, wherein the bracket is physically coupled via one or more fasteners penetrating the outer turbine case wall.
7. The measuring system of claim 1 , wherein the first region is zone between the turbine case wall of the turbine and a turbine platform of the turbine.
8. The apparatus of claim 6 , wherein the turbine is a jet engine turbine employed by an aircraft.