High temperature brush seal tuft testing of metallic bristles versus chrome carbide
Author:
Affiliation:
1. Ohio Aerospace Inst., Cleveland
2. NASA, Lewis Research Center, Cleveland, OH
3. Pratt & Whitney, West Palm Beach, FL
4. Pratt & Whitney, East Hartford, CT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2908
Reference24 articles.
1. Mahler, F., and Boyes, E.,The Application of Brush Seals inLarge CommercialJet Engines,"AIAApaper 95-2617,1995.
2. Steinetz, B.M., and Hendricks, R.C. "Engine Seal Technology Requirements to Meet NASA's Advanced Subsonic Technology Program Goals," AIAApaper 94-2698,1994.
3. Flower, R."Brush Seal Development System," AIAApaper 90-2143,1990.
4. Chupp, R.E., andNelson, Lt.P."Evaluation of Brush Seals forLimited-Life Engines,"AIAA paper 90-2140,1990.
5. Holle,G.F.,andKrishnan,MJR."GasTurbine Engine Brush Seal Applications," AIAApaper 90-2142,1990.
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