Synchronized air modulating system
A system for modulating air flow in a gas turbine engine is provided. The system may include a seal wall comprising an opening, a seal door configured to slideably engage the seal wall, and an actuator configured to move the seal door over the opening. In various embodiments, the system may include a surface forward of the seal door. The seal door may be configured to seal a passage through the surface and the opening of the seal wall. A track may be disposed under the seal door. The track may comprise cobalt. Rollers may be coupled to the seal door with the rollers on the track. The seal door may comprise a nickel-chromium alloy. A sync ring may be coupled to the seal door. The actuator may be coupled through the sync ring to the seal door.
1. A system for modulating air flow in a gas turbine engine, comprising:
a seal wall comprising a planar surface and an opening extending through the seal wall;
a seal door configured to sealably engage the opening, the seal door further configured to translate in a rectilinear direction along the planar surface between a first position to cover the opening and a second position to uncover the opening; and
an actuator configured to translate the seal door in the rectilinear direction and along the planar surface between the first position and the second position.
2. The system of claim 1 , wherein the seal door comprises a nickel-chromium alloy.
3. The system of claim 1 , wherein the seal door slideably engages the seal wall.
4. A sealing configuration for an air flow path of a heat exchanger of a gas turbine engine, the sealing configuration comprising:
a port extending through a planar surface and configured to receive air from a first conduit associated with the heat exchanger;
a movable plate configured to translate in a rectilinear direction along the planar surface to seal the port, wherein the movable plate is further configured to modulate air flow from the first conduit to a second conduit by translational movement of the moveable plate in the rectilinear direction along the planar surface; and
a drive element configured to translate the movable plate with respect to the port in the rectilinear direction along the planar surface, wherein the drive element translates the movable plate for at least one of modulating air flow from the first conduit to the second conduit and sealing the port.
5. The sealing configuration of claim 4 , wherein the port is a passageway in a structure of the gas turbine engine for receiving bypass air flow.
6. The sealing configuration of claim 4 , wherein the movable plate is a sliding plate configured to slide relative to the port.
7. The sealing configuration of claim 4 , wherein the movable plate is pressure sealed to the port by air received from the first conduit.
8. The sealing configuration of claim 4 , further comprising a control element configured to provide continuous control of the movable plate and the drive element.
9. The sealing configuration of claim 4 , wherein the drive element and one or more elements for retaining the movable plate are mounted near the port.
10. The sealing configuration of claim 4 , wherein a portion of the movable plate is configured to engage with the drive element.