Composite wear pad for exhaust nozzle
A composite wear pad for being coupled to a slider block of a convergent nozzle of a gas turbine engine includes a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin. The composite wear pad also includes a first rod coupled to the high heat capacity composite at a first axial end of the composite wear pad such that a first end thickness. The composite wear pad also includes a second rod coupled to the high heat capacity composite at a second axial end of the composite wear pad such that the first axial end and the second axial end of the composite wear pad each have an end thickness that is greater than a middle thickness of the composite wear pad.
1. A system comprising:
a nozzle section of a gas turbine engine, the nozzle section comprising a convergent flap and a static structure, wherein the static structure comprises a slider track that converges radially inward relative to a central longitudinal axis of the gas turbine engine from forward to aft;
a slider block coupled to the convergent flap and configured to slide along the slider track of the static structure to change a position of the slider block both axially and radially, wherein the slider block defines a first slot having a first outer distance and a first inner distance that is greater than the first outer distance; and
a composite wear pad having a first axial end having a first end thickness that is greater than the first outer distance of the slider block such that the composite wear pad resists axial separation in response to the first axial end being positioned within the first slot.
2. The system of claim 1 , wherein the composite wear pad further includes a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin.
3. The system of claim 2 , wherein the composite wear pad includes a first rod having a cylindrical shape and positioned on the first axial end of the composite wear pad.
4. The system of claim 3 , wherein the composite wear pad encloses a curved surface of the first rod.
5. The system of claim 2 , wherein the composite wear pad includes a first rod having a triangular prism shape and positioned on the first axial end of the composite wear pad.
6. The system of claim 2 , wherein the resin includes a high temperature thermosetting polyimide resin.
7. The system of claim 1 , wherein:
the slider block further defines a second slot having a second outer distance and a second inner distance that is greater than the second outer distance; and
the composite wear pad further includes a second axial end having a second end thickness that is greater than the second outer distance of the slider block such that the composite wear pad will resist axial separation in response to the second axial end being positioned within the second slot.
8. A system comprising:
a nozzle section of a gas turbine engine, the nozzle section comprising a convergent flap and a static structure, wherein the static structure comprises a slider track that converges radially inward relative to a central longitudinal axis of the gas turbine engine from forward to aft;
a slider block coupled to the convergent flap and configured to slide along the slider track of the static structure to change a position of the slider block both axially and radially, wherein the slider block defines a first slot and a second slot; and
a composite wear pad including:
a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin,
a first rod coupled to the high heat capacity composite at a first axial end of the composite wear pad such that the first axial end of the composite wear pad can be received by the first slot, and
a second rod coupled to the high heat capacity composite at a second axial end of the composite wear pad such that the second axial end of the composite wear pad can be received by the second slot.
9. The system of claim 8 , wherein the resin includes a high temperature thermosetting polyimide resin.
10. The system of claim 8 , wherein:
the high heat capacity composite has a middle thickness;
the first axial end of the composite wear pad has an end thickness; and
the first slot has an outer distance and an inner distance that is greater than the outer distance such that the first axial end of the composite wear pad will resist axial separation from the slider block in response to the first axial end being positioned within the first slot.
11. The system of claim 8 , wherein the first rod and the second rod each have a cylindrical shape.
12. The system of claim 8 , wherein the high heat capacity composite surrounds the first rod and the second rod.
13. The system of claim 8 , wherein the first rod and the second rod each have a triangular prism shape.