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Non-Contacting Finger Seals Static Performance Test Results at Ambient and High Temperatures
Author(s) -
Margaret P. Proctor
Publication year - 2016
Publication title -
52nd aiaa/sae/asee joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2016-4921
Subject(s) - leakage (economics) , lift (data mining) , seal (emblem) , concentric , materials science , labyrinth seal , rotor (electric) , turbine , structural engineering , composite material , mechanics , mechanical engineering , engineering , computer science , mathematics , physics , geometry , art , data mining , economics , visual arts , macroeconomics
The non-contacting finger seal is an advanced seal concept with potential to reduce specific fuel consumption in gas turbine engines by 2 to 3 percent with little to no wear of the seal or rotor. Static performance tests and bind-up tests of eight different non-contacting finger seal configurations were conducted in air at pressure differentials up to 689.4 kPa and temperatures up to 922 K. Four of the seals tested were designed to have lift pads concentric to a herringbone-grooved rotor which generates hydrodynamic lift when rotating. The remaining seals were tested with a smooth rotor; one seal had a circumferential taper and one had an axial taper on the lift pad inner diameter to create hydrodynamic lift during rotation. The effects of the aft finger axial thickness and of the forward finger inner diameter on leakage performance were investigated as well and compared to analytical predictions.

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