CMC component arrangement and method of manufacture
A method of manufacturing a component includes forming an inner wrap about a mandrel. The inner wrap has first and second walls joined by a base portion and an outer wall. A rod is arranged at each of the first and second walls. An outer wrap is formed about the inner wrap and the rods to form a body. Features are formed in the first and second walls.
1. A method of manufacturing a component, comprising:
forming an inner wrap about a mandrel, the inner wrap having first and second walls joined by a base portion and an outer wall;
arranging a rod at each of the first and second walls;
forming an outer wrap about the inner wrap and the rods to form a body;
forming features in the first and second walls; and
machining the body to form a blade outer air seal segment.
2. The method of claim 1 , comprising removing the mandrel and the rods.
3. The method of claim 1 , comprising densifying the body.
4. The method of claim 3 , wherein the densifying comprises injecting an infiltrant into the body to fill voids formed by the rods.
5. The method of claim 1 , wherein the machining comprises removing at least 50% of the outer wall.
6. The method of claim 1 , wherein the machining comprises removing a portion of the first and second walls to form a trailing edge platform.
7. The method of claim 1 , wherein the machining is performed by an ultrasonic machine.
8. The method of claim 1 , wherein the inner and outer wraps are formed from fibrous braided or woven plies.
9. The method of claim 8 , wherein the inner wrap is formed from at least two plies.
10. The method of claim 8 , wherein the body has between 5 and 15 plies.
11. The method of claim 1 , wherein the rods extend along an axial length of the first and second walls.
12. The method of claim 1 , wherein each of the rods has a diameter of at least 0.040 inches (1.016 mm).
13. The method of claim 1 , wherein at least one of the rods comprises an inner rod and an outer rod, wherein the outer rod is removed before the step of forming features in the first and second walls.
14. The method of claim 1 , wherein one rod is arranged at the first wall and configured to form a protrusion, and two rods are arranged at the second wall and configured to form a groove.
15. The method of claim 1 , wherein the outer wrap and the inner wrap are formed from a ceramic matrix composite material.
16. The method of claim 1 , wherein the rods are cylindrical.
17. A method of manufacturing a component, comprising:
forming an inner wrap about a mandrel, the inner wrap having first and second walls joined by a base portion and an outer wall;
arranging a rod at each of the first and second walls;
forming an outer wrap about the inner wrap and the rods to form a body; and
forming features in the first and second walls, wherein one rod is arranged at the first wall and configured to form a protrusion, and two rods are arranged at the second wall and configured to form a groove.
18. The method of claim 17 , wherein at least one of the rods comprises an inner rod and an outer rod, wherein the outer rod is removed before the step of forming features in the first and second walls.
19. The method of claim 17 , wherein the rods extend along an axial length of the first and second walls.
20. A method of manufacturing a component, comprising:
forming an inner wrap about a mandrel, the inner wrap having first and second walls joined by a base portion and an outer wall;
arranging a rod at each of the first and second walls;
forming an outer wrap about the inner wrap and the rods to form a body; and wherein the outer wrap and the inner wrap are formed from a ceramic matrix composite material; and
forming features in the first and second walls.