Gas turbine engine with dove-tailed TOBI vane

1. A combustor assembly for a gas turbine engine comprising:

a TOBI module including a TOBI housing, the TOBI housing having a slot; and

a vane including a dovetail removably received within the slot, wherein the TOBI housing includes an axially extending TOBI nozzle array, the TOBI housing includes a plenum, and a cooling passage fluidly connects the plenum to the vane, the TOBI housing includes passages configured to provide cooling fluid to the vane, the TOBI housing includes a first passageway further connecting the TOBI nozzle to the plenum, wherein the TOBI housing includes a second passage configured to fluidly connect a cavity external to the TOBI nozzle to the plenum.

2. A gas turbine engine comprising:

a combustor section including a combustor assembly;

a turbine section having a first fixed stage;

wherein the combustor assembly includes a TOBI module having an annular TOBI housing, the TOBI housing having multiple circumferentially arranged slots, a circumferential array of vanes providing the first fixed stage, each vane including a dovetail removably received within a respective one of the slot;

wherein the TOBI housing includes a plenum, a circumferential array of axially extending TOBI nozzles, a first passageway, and one or more cooling passages through one or more openings, the plenum being arranged radially between the upper slots and the lower nozzles; and

wherein a nozzle of the array of nozzles is fluidly connected to the plenum via the first passageway, and a vane of the array of vanes is fluidly connected to the plenum via the one or more cooling passages that communicate cooling fluid from the plenum to cooling passageways within the vane.

3. The gas turbine engine according to claim 2 , wherein the combustor assembly includes a combustor housing and a diffuser case secured to the TOBI housing.