Nozzles with internal manifolding
A nozzle includes a nozzle body defining a liquid circuit extending from a liquid inlet to a liquid outlet. The liquid circuit includes a plurality of spiral liquid passages spiraling radially inward relative to a spray axis. The spiral liquid passages all lie in a plane normal to the spray axis. A manifold assembly includes a plurality of such nozzles. A manifold ring is in fluid communication with the liquid inlet of each of the nozzles to deliver liquid to the nozzles. The nozzles are circumferentially spaced apart around the manifold ring.
1. A manifold assembly comprising:
a plurality of nozzles wherein each nozzle includes a nozzle body defining a liquid circuit extending from a liquid inlet to a liquid outlet, wherein the liquid circuit includes a plurality of spiral liquid passages spiraling radially inward relative to a spray axis, wherein the spiral liquid passages all lie in a plane normal to the spray axis, wherein each of the spiral liquid passages extends circumferentially more than 270° around the spray axis, and wherein each of the spiral liquid passages has an outlet orifice defining a spray axis that is nearly tangential to a circumferential direction the spay axis; and
a manifold ring in fluid communication with the liquid inlet of each of the nozzles to deliver liquid to the nozzles, wherein the nozzles are circumferentially spaced apart around the manifold ring.
2. A manifold assembly as recited in claim 1 , wherein the manifold ring is a first manifold ring, and further comprising a second manifold ring, wherein the fuel nozzles extend radially between the first and second manifold rings.
3. A manifold assembly as recited in claim 1 , wherein each manifold ring includes bayonet features, wherein the bayonet features of each manifold ring are interlocked with a bayonet feature of a combustor wall or combustor sliding support.
4. A manifold assembly as recited in claim 1 , wherein each of the nozzles includes a heat shield mounted to a downstream face thereof, wherein the heat shields define an upstream combustor dome wall.
5. A manifold assembly as recited in claim 4 , each nozzle includes an inner air circuit passing inboard of the liquid outlet and an outer air circuit passing outboard of the liquid outlet, wherein the inner and outer air circuits are the only pathway for air to pass through the combustor dome wall.
6. A manifold assembly as recited in claim 1 , wherein for each nozzle, each spiral liquid passage defines a respective outlet orifice of the liquid outlet.