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, the CMC deflector including a cup integrally formed with a remainder of the deflector from a CMC material, the cup extending forward through the opening in the combustor dome, the cup defining one or more bayonets and a cup slot;
a fuel-air mixer defining a groove about an outer perimeter of the fuel-air mixer, the one or more bayonets received in the groove; and
a seal plate including a key, the key received in the 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 fuel-air mixer comprises an aft end positioned within both the opening of the combustor dome and the deflector opening, wherein the aft end of the fuel-air mixer flares radially outward to form a flare cone that contacts the CMC deflector, and wherein each said fuel-air mixer slot corresponding to the one or more bayonets is defined through the flare cone.
2. The combustor dome assembly of claim 1 , wherein the seal plate is attached to the combustor dome.
3. The combustor dome assembly of claim 1 , wherein the fuel-air mixer is attached to the seal plate.
4. The combustor dome assembly of claim 1 , wherein the CMC deflector includes a flare cone, and wherein the flare cone covers the plurality of fuel-air mixer slots in the fuel-air mixer on the aft side of the combustor dome assembly.
5. The combustor dome assembly of claim 1 , wherein the seal plate includes a seal plate wall extending aft through the opening in the combustor dome, the seal plate wall positioned between the combustor dome and the cup of the CMC deflector.
6. The combustor dome assembly of claim 5 , wherein the cup is positioned between the seal plate wall and an aft end of the fuel-air mixer.
7. The combustor dome assembly of claim 1 , wherein the cup of the CMC deflector defines at least three bayonets.
8. A method of assembling the combustor dome assembly of claim 1 , the method comprising:
assembling the combustor dome with the combustor;
inserting the seal plate from the forward side of the combustor dome assembly;
attaching the seal plate to the combustor dome;
inserting the CMC deflector from the aft side of the combustor dome assembly, the CMC deflector having the one or more bayonets;
inserting the fuel-air mixer from a forward side of the combustor dome assembly, the fuel-air mixer defining the groove for receipt of the one or more bayonets;
rotating the fuel-air mixer to engage the one or more bayonets; and
attaching the fuel-air mixer to the seal plate.
9. The method of claim 8 , further comprising positioning the key of the seal plate in the cup slot defined in the CMC deflector.
10. The method of claim 8 , wherein the combustor dome assembly comprises a plurality of seal plates and a plurality of CMC deflectors, and wherein each seal plate of the plurality of seal plates is inserted and attached to the combustor dome before any of the plurality of CMC deflectors is inserted into the combustor dome assembly.
11. The method of claim 10 , wherein the combustor dome assembly comprises a plurality of fuel-air mixers, wherein each of the plurality of fuel-air mixers is inserted next to each one of the plurality of CMC deflectors.