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Continued Investigation of Leakage and Power Loss Test Results for Competing Turbine Engine SealsSeal leakage decreases with increasing surface speed due to reduced clearances from disk centrifugal growth. Annular and labyrinth seal leakage are 2-3 times greater than brush and finger seal leakage. Seal leakage rates increase with increasing temperature because of seal clearance growth due to different coefficients of thermal expansion between the seal and test disk. Seal power loss is not strongly affected by inlet temperature. Seal power loss increases with increasing surface speed, seal pressure differential, mass flow rate or flow factor, and radial clearance. The brush and finger seals had nearly the same power loss. Annular and labyrinth seal power loss were higher than finger or brush seal power loss. The brush seal power loss was the lowest and 15-30% lower than annular and labyrinth seal power loss.
Document ID
20080003830
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Delgado, Irebert R.
(Army Research Lab. Cleveland, OH, United States)
Proctor, Margaret P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Publication Information
Publication: 2006 NASA Seal/Secondary Air System Workshop; Volume 1
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
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