Oil baffle for gas turbine fan drive gear system
A turbine engine includes a housing supporting compressor, turbine sections, and an epicyclic gear train including a carrier. Sun gear and intermediate gears are arranged about and intermeshing with the sun gear. The intermediate gears are supported by the carrier. A baffle includes a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubrication on the at least one of the sun gear and intermediate gears.
1. A turbine engine comprising:
a housing supporting compressor and turbine sections; and
an epicyclic gear train including:
a carrier;
a sun gear and intermediate gears arranged about and intermeshing with the sun gear, the intermediate gears supported by the carrier; and
a baffle supported relative to the carrier, the baffle including opposing arcuate surfaces, each arcuate surface providing a concavity arranged adjacent to a nearby intermediate gear, the baffle including a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubrication on the at least one of the sun gear and intermediate gears.
2. The turbine engine according to claim 1 , comprising a ring gear intermeshing with the intermediate gears and an output shaft interconnected to the ring gear, and an input shaft interconnected to the sun gear.
3. The turbine engine according to claim 2 , wherein the carrier is fixed relative to a housing, the output shaft drives a turbo fan, and the input shaft supports a compressor hub having compressor blades.
4. The turbine engine according to claim 1 , wherein the carrier includes spaced apart walls with circumferentially spaced mounts interconnecting the walls, the mounts providing circumferentially spaced apart apertures between the mounts at an outer circumference of the carrier, the intermediate gears extending through the apertures to intermesh with a ring gear.
5. The turbine engine according to claim 4 , comprising a housing supporting a torque frame that is secured to the mounts.
6. A turbine engine comprising:
a housing supporting compressor and turbine sections; and
an epicyclic gear train including:
a carrier, wherein the carrier includes spaced apart walls with circumferentially spaced mounts interconnecting the walls, the mounts providing circumferentially spaced apart apertures between the mounts at an outer circumference of the carrier;
a sun gear and intermediate gears arranged about and intermeshing with the sun gear, the intermediate gears supported by the carrier, the intermediate gears extending through the apertures to intermesh with a ring gear; and
a baffle supported relative to the carrier including a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubrication on the at least one of the sun gear and intermediate gears, wherein the lubrication passage includes a primary passage extending laterally between the walls and first and second passages in communication with the primary passage and respectively terminating near the sun gear and intermediate gears.
7. The turbine engine according to claim 6 , comprising a tube extending through a hole in one of the walls, the tube in communication with the primary passage.
8. An epicyclical gear train for a turbine engine comprising:
a sun gear, and intermediate gears arranged about and intermeshing with the sun gear;
a carrier for supporting the intermediate gears; and
one or more baffles secured within the carrier, the baffles including opposing arcuate surfaces, each arcuate surface providing a concavity arranged adjacent to a nearby intermediate gear, the baffles including respective lubrication passages near at least one of the sun gear and the intermediate gears for directing a lubrication thereon.
9. The epicyclical gear train for a turbine engine according to claim 8 , wherein the baffles are secured to the carrier with respective fasteners.
10. The epicyclical gear train for a turbine engine according to claim 8 , wherein the baffles are integral with carrier.