Geared gas turbine engine with improved breather air venting
Aspects of the disclosure are directed to a gas turbine engine, having a fan that rotates about a central longitudinal axis. The gas turbine engine may comprise a nacelle having an outer wall that radially circumscribes the fan. The gas turbine engine may further comprise a fan drive gear system that drives the fan, and a rotating shaft that is coupled to and drives the fan drive gear system. The gas turbine engine may further comprise an air vent line in fluid communication with a bearing compartment to remove air from the bearing compartment and provide the removed air to a deoiler that removes oil droplets from the removed air and provides deoiler filtered air. A vent output line receives the deoiler filtered air and discharges the deoiler filtered air along a radially interior surface of the nacelle outer wall.
1. A gas turbine engine, comprising:
a fan that rotates about a central longitudinal axis;
a nacelle having an outer wall that radially circumscribes the fan;
a fan drive gear system that drives the fan;
a rotating shaft that is coupled to and drives the fan drive gear system;
an air vent line in fluid communication with a bearing compartment to remove air from the bearing compartment and provide the removed air to a deoiler that removes oil droplets from the removed air and provides deoiler filtered air; and
a vent output line that receives the deoiler filtered air and discharges the deoiler filtered air along a radially interior surface of the nacelle outer wall,
where fan air static air pressure adjacent to the nacelle outer wall is less than bearing compartment static air pressure such that deoiler filtered air exiting the vent output line remains radially proximate to the nacelle outer wall as it mixes with fan air,
where the vent output line includes a vent line exit that is flush with the interior surface of the nacelle outer wall and through which the deoiler filtered air is discharged,
where the vent output line exit discharges the deoiler filtered air at an acute angle with respect to fan air flowing adjacent to the nacelle outer wall.
2. The gas turbine engine of claim 1 , further comprising an accessory gear box where the deoiler is located adjacent to the accessory gear box.
3. The gas turbine engine of claim 1 , where the vent output line passes through a strut extending between a fan case and a nacelle outer wall.
4. The gas turbine engine of claim 1 , where the vent output line includes a plurality of line exits that are flush with the interior surface of the nacelle outer wall and through which the deoiler filtered air is discharged.