Seal assembly for gas turbine engine
AssigneeUnited Technologies Corporation
InventorsWinston Gregory Smiddy, Paul M. Lutjen
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AssigneeUnited Technologies Corporation
InventorsWinston Gregory Smiddy, Paul M. Lutjen
Estimating the term…
A seal assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a seal that has a seal body having a sealing portion that extends from an engagement portion. The sealing portion has a seal face that extends circumferentially between first and second mate faces. The seal body defines an internal cavity that extends circumferentially between the first and second mate faces, and the engagement portion has an impingement face opposite the seal face that defines a plurality of apertures to the internal cavity. A housing is mounted to the seal such that the impingement face is exposed to define a plenum between the housing and the impingement face. The housing defines a plurality of cooling passages, and each of the plurality of cooling passages define a passage axis that is oriented such that a projection of the passage axis intersects the seal body. A method of sealing is also disclosed.
A seal assembly for a gas turbine engine comprising:
A gas turbine engine comprising:
A method of sealing of a gas turbine engine, comprising:
Dependencies are inferred from the claim text.