CMC combustor deflector
Combustor dome assemblies having combustor deflectors are provided. For example, a combustor dome assembly comprises a combustor dome defining an opening; a ceramic matrix composite (CMC) deflector positioned adjacent the combustor dome on an aft side of the assembly; a fuel-air mixer defining a groove about an outer perimeter thereof; and a seal plate including a key. The CMC deflector includes a cup extending forward through the opening in the combustor dome that defines one or more bayonets and a slot. The bayonets are received in the fuel-air mixer groove, and the seal plate key is received in the CMC deflector slot. In another embodiment, where the seal plate may be omitted, a spring is positioned between the fuel-air mixer and the CMC deflector to hold the CMC deflector in place with respect to the combustor dome. Methods of assembling combustor dome assemblies having CMC deflectors also are provided.
1. A combustor dome assembly having a forward side and an aft side, the combustor dome assembly comprising:
a combustor dome defining an opening;
a ceramic matrix composite (CMC) deflector positioned adjacent the combustor dome on the aft side of the combustor dome assembly; and
a fuel-air mixer positioned adjacent the combustor dome on the forward side of the combustor dome assembly,
wherein a spring is positioned between the fuel-air mixer and the CMC deflector to hold the CMC deflector in place with respect to the combustor dome.
2. The combustor dome assembly of claim 1 , wherein the fuel-air mixer defines a pocket for receipt of the spring.
3. The combustor dome assembly of claim 1 , wherein the spring loads the CMC deflector into the fuel-air mixer.
4. The combustor dome assembly of claim 1 , wherein the CMC deflector includes a cup extending forward through the opening in the combustor dome, wherein the cup defines one or more bayonets, wherein the fuel-air mixer defines a groove about an outer perimeter of the fuel-air mixer, and wherein the one or more bayonets are received in the groove.
5. The combustor dome assembly of claim 1 , wherein the spring is a Belleville washer.
6. The combustor dome assembly of claim 1 , wherein at least a portion of the CMC deflector extends forward through the opening in the combustor dome, and wherein at least a portion of the fuel-air mixer extends aft through the opening in the combustor dome.
7. A combustor dome assembly having a forward side and an aft side, the combustor dome assembly comprising:
a combustor dome defining an opening;
a ceramic matrix composite (CMC) deflector positioned adjacent the combustor dome on the aft side of the combustor dome assembly, the CMC deflector including a cup extending forward from a CMC deflector body through the opening in the combustor dome; and
a fuel-air mixer positioned adjacent the combustor dome on the forward side of the combustor dome assembly,
wherein a spring is positioned between the fuel-air mixer and the CMC deflector to hold the CMC deflector in place with respect to the combustor dome, and
wherein a forward end of the CMC deflector body flares radially inward to form a flare cone, and
wherein the flare cone extends adjacent an aft end of the fuel-air mixer.
8. The combustor dome assembly of claim 7 , wherein the flare cone extends between the aft end of the fuel-air mixer and an opening defined through the fuel-air mixer.
9. The combustor dome assembly of claim 7 , wherein the cup is integrally formed with a remainder of the CMC deflector from a CMC material.
10. The combustor dome assembly of claim 7 , wherein the cup defines one or more bayonets and a cup slot, wherein the fuel-air mixer defines a plurality of fuel-air mixer slots, each fuel-air mixer slot corresponding to each of the one or more bayonets, each said fuel-air mixer slot configured for a respective one of the one or more bayonets to pass therethrough, wherein the cup of the CMC deflector defines a deflector opening, wherein the aft end of the fuel-air mixer is positioned within both the opening of the combustor done and the deflector opening.
11. The combustor dome assembly of claim 10 , further comprising:
a seal plate including a key, the key received in the cup slot.
12. The combustor dome assembly of claim 7 , wherein the flare cone contacts the aft end of the fuel-air mixer.
13. The combustor dome assembly of claim 7 , further comprising:
a seal plate positioned adjacent the forward side of the combustor dome assembly, the seal plate including an annular wall extending aft through the opening in the combustor dome and defining an opening through the seal plate.
14. The combustor dome assembly of claim 7 , wherein the fuel-air mixer is attached to the combustor dome by welding or brazing.