CMC airfoil with wishbone shaped fiber layup structure forming portion of platform and root
An airfoil includes a CMC airfoil wall that defines a platform, a root that extends radially from the platform, and an airfoil section that extends radially from the platform opposite the root. The CMC airfoil wall includes a wishbone-shaped fiber layup structure. The wishbone-shaped fiber layup structure includes first and second arms that merge into a single leg. The first and second arms are comprised of a network of fiber tows, and the single leg includes fiber tows from each of the first and second arms that are interwoven in the single leg. The single leg forms a portion of the root, and the first and second arms extend in opposite directions from the single leg and form a portion of the platform.
1. An airfoil comprising:
a ceramic matrix composite (CMC) airfoil wall defining a platform, a root extending radially from the platform, and an airfoil section extending radially from the platform opposite the root, the CMC airfoil wall including first and second wishbone-shaped fiber layup structures,
each of the first and second wishbone-shaped fiber layup structures including:
first and second arms that merge into a single leg,
the first and second arms being comprised of a network of fiber tows,
the single leg including fiber tows from each of the first and second arms that are interwoven in the single leg, the single leg forming a portion of the root, and
the first and second arms extending in opposite directions from the single leg and forming a portion of the platform, wherein
the first arm of the first wishbone-shaped fiber layup structure extending axially forwardly from the single leg of the first wishbone-shaped fiber layup structure, and the first arm of the second wishbone-shaped fiber layup structure extends axially aftly from the single leg of the second wishbone-shaped fiber layup structure,
the second arm of the first wishbone-shaped fiber layup structure extends axially aftly from the single leg of the first wishbone-shaped fiber layup structure, and the second arm of the second wishbone-shaped fiber layup structure extends axially forwardly from the single leg of the second wishbone-shaped fiber layup structure, and
a tip of the second arm of the first wishbone-shaped fiber layup structure is adjacent a tip of the second arm of the second wishbone-shaped fiber layup structure to define a gap therebetween.
2. The airfoil as recited in claim 1 , wherein the CMC airfoil wall includes radially inner and outer reinforcement fiber plies between which the second arm of the first wishbone-shaped fiber layup structure and the second arm of the of the second wishbone-shaped fiber layup structure are disposed, and the radially inner and outer reinforcement fiber plies each bridge the gap.
3. The airfoil as recited in claim 2 , wherein the single leg of the first wishbone-shaped fiber layup structure defines an axially forward face of the root, and the single leg of the second wishbone-shaped fiber layup structure defines an axially aft face of the root.
4. The airfoil as recited in claim 1 , wherein the second arm of each of the first and second wishbone-shaped fiber layup structure splits into a pair of fingers, and the airfoil section extends between the pair of fingers.
5. A gas turbine engine comprising:
a compressor section;
a combustor in fluid communication with the compressor section; and
a turbine section in fluid communication with the combustor, the turbine section having and an airfoil including:
a ceramic matrix composite (CMC) airfoil wall defining a platform, a root extending radially from the platform, and an airfoil section extending radially from the platform opposite the root, the root having a fir-tree profile, the CMC airfoil wall including first and second wishbone-shaped fiber layup structures,
each of the first and second wishbone-shaped fiber layup structures including:
first and second arms that merge into a single leg,
the first and second arms being comprised of a network of fiber tows,
the single leg including fiber tows from each of the first and second arms that are interwoven in the single leg, the single leg forming a portion of the root, and
the first and second arms extending in opposite directions from the single leg and forming a portion of the platform, the first arm of the first wishbone-shaped fiber layup structure extending axially forwardly from the single leg of the first wishbone-shaped fiber layup structure, the first arm of the second wishbone-shaped fiber layup structure extending axially aftly from the single leg of the second wishbone-shaped fiber layup structure, the second arm of the first wishbone-shaped fiber layup structure extending axially aftly from the single leg of the first wishbone-shaped fiber layup structure, and the second arm of the second wishbone-shaped fiber layup structure extending axially forwardly from the single leg of the second wishbone-shaped fiber layup structure, and a tip of the second arm of the first wishbone-shaped fiber layup structure is adjacent a tip of the second arm of the second wishbone-shaped fiber layup structure to define a gap therebetween.
6. The gas turbine engine as recited in claim 5 , wherein the CMC airfoil wall includes radially inner and outer reinforcement fiber plies between which the second arm of the first wishbone-shaped fiber layup structure and the second arm of the of the second wishbone-shaped fiber layup structure are disposed, and the radially inner and outer reinforcement fiber plies each bridge the gap.
7. The gas turbine engine as recited in claim 6 , wherein the single leg of the first wishbone-shaped fiber layup structure defines an axially forward face of the root, and the single leg of the second wishbone-shaped fiber layup structure defines an axially aft face of the root.
8. The gas turbine engine as recited in claim 5 , wherein the second arm of each of the first and second wishbone-shaped fiber layup structure splits into a pair of fingers, and the airfoil section extends between the pair of fingers.
9. The gas turbine engine as recited in claim 5 , wherein the turbine section includes a disk that defines a slot that has a geometry that corresponds to the fir-tree profile such that the root interlocks with the slot.