A swirler, such as for swirling air in a fuel injector of a gas turbine engine, includes a swirler body with opposed inlet and outlet ends with a swirler wall extending therebetween along a longitudinal axis. The inlet end of the swirler body defines an inlet opening. A plurality of swirl slots is defined through a portion of the swirler wall that converges toward the longitudinal axis in a direction from the inlet opening toward the outlet end of the swirler body. The swirl slots are radially off-set with respect to the longitudinal axis for imparting swirl on a flow passing from the inlet opening, through the swirl slots, and past the outlet end of the swirler body.
1. A fuel injector comprising:
an injector body with opposed inlet and outlet ends with a liquid flow circuit passing through the injector body in a direction parallel to a longitudinal axis of the injector body, the liquid flow circuit extending from the inlet end of the injector body to the outlet end of the injector body, wherein an inner air circuit is defined through the injector body along the longitudinal axis of the injector body; and
a swirler mounted to the injector body having a swirler body with opposed inlet and outlet ends with a swirler wall extending within the inner air circuit and between the opposed inlet and outlet ends of the swirler body along the longitudinal axis, the inlet end of the swirler body defining an inlet opening, wherein a plurality of swirl slots are defined through a portion of the swirler wall that converges toward the longitudinal axis in a direction from the inlet opening toward the outlet end of the swirler body, wherein the plurality of swirl slots are each radially off-set with respect to the longitudinal axis for imparting swirl on a flow passing from the inlet opening, through the plurality of swirl slots, and past the outlet end of the swirler body, wherein the only flow path though the swirler wall is through the plurality of swirl slots.
2. The fuel injector as recited in claim 1 , wherein a portion of the inner air circuit defined between the swirler wall and a wall of the inner air circuit of the injector body has a cross-sectional area that increases in a direction along the longitudinal axis towards the outlet end of the swirler body.
3. The fuel injector as recited in claim 2 , wherein the plurality of swirl slots feed into the portion of the inner air circuit defined between the swirler wall and the wall of the inner air circuit.
4. The fuel injector as recited in claim 1 , wherein each of the swirl slots are elongated in a respective direction along the swirler wall.
5. The fuel injector as recited in claim 4 , wherein each respective direction is oblique axially and circumferentially relative to the longitudinal axis.
6. The fuel injector as recited in claim 1 , wherein the swirler wall defines an axial cross-sectional profile that is bullet-shaped.
7. The fuel injector as recited in claim 1 , wherein the swirler wall defines an axial cross-sectional profile that is trapezoidal and wherein the outlet end of the swirler body includes a planar portion of the swirler wall that is substantially perpendicular to the longitudinal axis.
8. The fuel injector as recited in claim 1 , wherein each swirl slot is a cylindrical bore through the swirler wall.
9. The fuel injector as recited in claim 1 , wherein the swirler wall is a converging-diverging swirler wall.