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Blade tip geometry - A factor in abrading sintered seal materialExperimental results are presented for the case of titanium blade tip specimens of various geometrical configurations rubbing at 100 m/s against specimens of nickel-chromium sintered powder metal seal material, the latter being fed toward the rotating blades at an incursion rate of 0.0254 mm/s. Blade tips in the form of orthogonal cutting tools with about 85 deg negative rake angles exhibited desirable abrading capabilities, as measured by the tear-free appearance of the grooves they generated in the seal material, little wear of blade tips, low forces of interaction and low seal densification. Similar results have been obtained for blade specimens with tips of small radius of curvature, as well as for square-ended and slanted blade tips that are plasma-sprayed with abrasive particles. The relationship between the size of these particles and their abrading effectiveness is considered.
Document ID
19850031563
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wolak, J.
(Washington Univ. Seattle, WA, United States)
Emery, A. F.
(Washington Univ. Seattle, WA, United States)
Etemad, S.
(Washington Univ. Seattle, WA, United States)
Choi, S. R.
(Washington, University Seattle, WA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Publication Information
Publication: ASME, Transactions, Journal of Tribology
Volume: 106
ISSN: 0742-4787
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ISSN: 0742-4787
Accession Number
85A13714
Distribution Limits
Public
Copyright
Other

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