Experimental 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° 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 plasma sprayed with abrasive particles. The relationship between the size of these particles and their abrading effectiveness is considered.
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October 1984
Research Papers
Blade Tip Geometry—A Factor in Abrading Sintered Seal Material
J. Wolak,
J. Wolak
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
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A. F. Emery,
A. F. Emery
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
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S. Etemad,
S. Etemad
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
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S. R. Choi
S. R. Choi
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
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J. Wolak
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
A. F. Emery
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
S. Etemad
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
S. R. Choi
Department of Mechanical Engineering, University of Washington, Seattle, WA 98195
J. Tribol. Oct 1984, 106(4): 527-533 (7 pages)
Published Online: October 1, 1984
Article history
Received:
March 25, 1983
Online:
October 29, 2009
Citation
Wolak, J., Emery, A. F., Etemad, S., and Choi, S. R. (October 1, 1984). "Blade Tip Geometry—A Factor in Abrading Sintered Seal Material." ASME. J. Tribol. October 1984; 106(4): 527–533. https://doi.org/10.1115/1.3260976
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