Active bypass flow control for a seal in a gas turbine engine
An active bypass flow control system for controlling bypass compressed air based upon leakage flow of compressed air flowing past an outer balance seal between a stator and rotor of a first stage of a gas turbine in a gas turbine engine is disclosed. The active bypass flow control system is an adjustable system in which one or more metering devices may be used to control the flow of bypass compressed air as the flow of compressed air past the outer balance seal changes over time as the outer balance seal between the rim cavity and the cooling cavity wears. In at least one embodiment, the metering device may include a valve formed from one or more pins movable between open and closed positions in which the one pin at least partially bisects the bypass channel to regulate flow.
1. An active bypass flow control system for an outer balance seal, comprising:
a stator assembly positioned in proximity to a first stage rotor whereby a compressed air channel is positioned between a portion of the stator assembly and a rotor shaft;
at least one outer balance seal configured to at least reduce a portion of hot gases from flowing into a cooling cavity;
at least one bypass channel extending from an inlet in fluid communication with the compressed air channel upstream of the at least one outer balance seal to an outlet in fluid communication with the compressed air channel downstream from the at least one outer balance seal;
at least one metering device that is adjustable to adjust the flow of cooling fluids through the at least one bypass channel to accommodate a changing flow of compressed air past the at least one outer balance seal as the outer balance seal wears during turbine engine operation; and
wherein the at least one metering device includes at least one valve formed from at least one pin movable between open and closed positions in which the at least one pin at least partially bisects the at least one bypass channel; and
further comprising a sync ring in communication with the at least one pin via at least one valve arm extending from the at least one pin to the sync ring.
2. The active bypass flow control system of claim 1 , wherein the at least one metering device further comprises at least one cam engaged to the at least one pin to move the at least one pin between open and closed positions.
3. The active bypass flow control system of claim 1 , wherein at least one cam is formed from a collar positioned in contact with a head of the at least one pin.
4. The active bypass flow control system of claim 1 , wherein the at least one pin further comprises at least one orifice located in the shaft of the at least one pin and positioned such that the at least one orifice is aligned with the at least one bypass channel when the at least one pin is in the open position.
5. The active bypass flow control system of claim 1 , wherein the at least one valve arm is pivotably attached to the sync ring.
6. The active bypass flow control system of claim 1 , wherein the sync ring is attached to at least one cam engaged to the at least one pin to move the at least one pin between open and closed positions via at least one valve arm.
7. The active bypass flow control system of claim 1 , wherein the sync ring is cylindrical with a plurality of valve arms pivotably attached thereto.
8. The active bypass flow control system of claim 1 , wherein the sync ring further comprises a plurality of cams formed from slots contained within the sync ring.
9. The active bypass flow control system of claim 8 , wherein at least one of the plurality of cams is nonparallel and nonorthogonal to an axis tangential to curved midline of the sync ring.
10. An active bypass flow control system for an outer balance seal, comprising:
a stator assembly positioned in proximity to a first stage rotor whereby a compressed air channel is positioned between a portion of the stator assembly and a rotor shaft;
at least one outer balance seal configured to at least reduce a portion of hot gases from flowing into a cooling cavity;
at least one bypass channel extending from an inlet in fluid communication with the compressed air channel upstream of the at least one outer balance seal to an outlet in fluid communication with the compressed air channel downstream from the at least one outer balance seal;
at least one metering device that is adjustable to adjust the flow of cooling fluids through the at least one bypass channel to accommodate a changing flow of compressed air past the at least one outer balance seal as the outer balance seal wears during turbine engine operation; and
wherein the at least one metering device includes at least one valve formed from at least one pin movable between open and closed positions in which the at least one pin at least partially bisects the at least one bypass channel;
wherein the at least one metering device further comprises at least one cam engaged to the at least one pin to move the at least one pin between open and closed positions;
wherein the at least one cam is formed from a collar positioned in contact with a head of the at least one pin; and
further comprising a sync ring in communication with the at least one pin via at least one valve arm extending from the at least one pin to the sync ring.
11. The active bypass flow control system of claim 10 , wherein the at least one pin further comprises at least one orifice located in the shaft of the at least one pin and positioned such that the at least one orifice is aligned with the at least one bypass channel when the at least one pin is in the open position.
12. The active bypass flow control system of claim 10 , wherein the at least one valve arm is pivotably attached to the sync ring.
13. The active bypass flow control system of claim 10 , wherein the sync ring is attached to at least one cam engaged to the at least one pin to move the at least one pin between open and closed positions via at least one valve arm.
14. The active bypass flow control system of claim 10 , wherein the sync ring is cylindrical with a plurality of valve arms pivotably attached thereto.
15. An active bypass flow control system for an outer balance seal, comprising:
a stator assembly positioned in proximity to a first stage rotor whereby a compressed air channel is positioned between a portion of the stator assembly and a rotor shaft;
at least one outer balance seal configured to at least reduce a portion of hot gases from flowing into a cooling cavity;
at least one bypass channel extending from an inlet in fluid communication with the compressed air channel upstream of the at least one outer balance seal to an outlet in fluid communication with the compressed air channel downstream from the at least one outer balance seal;
at least one metering device that is adjustable to adjust the flow of cooling fluids through the at least one bypass channel to accommodate a changing flow of compressed air past the at least one outer balance seal as the outer balance seal wears during turbine engine operation;
wherein the at least one metering device includes at least one valve formed from at least one pin movable between open and closed positions in which the at least one pin at least partially bisects the at least one bypass channel;
a sync ring in communication with the at least one pin via at least one valve arm extending from the at least one pin to the sync ring;
wherein the at least one valve arm is pivotably attached to the sync ring; and
at least one cam formed from a slot contained within the sync ring.
16. The active bypass flow control system of claim 15 , wherein the at least one pin further comprises at least one orifice located in the shaft of the at least one pin and positioned such that the at least one orifice is aligned with the at least one bypass channel when the at least one pin is in the open position.
17. The active bypass flow control system of claim 15 , wherein the sync ring is cylindrical with a plurality of valve arms pivotably attached thereto and wherein the at least one cam comprises a plurality of cams formed from slots contained within the sync ring.
18. The active bypass flow control system of claim 17 , wherein at least one of the plurality of cams is nonparallel and nonorthogonal to an axis tangential to curved midline of the sync ring.