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Develop reusable re-entry and hypersonic vehicle control surface seals to prevent ingestion of hot boundary layer flow. |
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- Limit hot gas flow and heat transfer to underlying low-temperature structures
- Withstand temperatures of 1500-2200+ °F
- Remain resilient for multiple load/heating cycles
- Limit loads against sealing surfaces
- Resist scrubbing damage
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Resilient Flexible Pressure-Activated Seal
Bruce M. Steinetz and Patrick J. Dunlap, Jr.
US Patent No. 7,497,443 Issued: March 3, 2009
High Temperature Seal for Large Structural Movements
Bruce M. Steinetz and Patrick J. Dunlap, Jr.
Patent No. 6,702,300 B1 Issued: March 9, 2004
Resilient Braided Rope Seal
Bruce M. Steinetz and Lawrence A. Kren
Patent No. 6,039,325 Issued: March 21, 2000
1996 Invention of the Year Award Winner
High Temperature, Flexible Fiber-Preform Seal
Bruce M. Steinetz and Paul J. Sirocky
Patent No. 5,082,293 Issued: January 21, 1992
Read more about the Invention of the Year award...
High Temperature, Bellows Hybrid Seal
Bruce M. Steinetz and Paul J. Sirocky
Patent No. 5,332,239 Issued: July 26, 1994
High Temperature, Flexible Pressure-Actuated Brush Seal
Bruce M. Steinetz and Paul J. Sirocky
Patent No. 5,076,590 Issued: December 31, 1991
High Temperature, Flexible Thermal Barrier Seal
Paul J. Sirocky and Bruce M. Steinetz
Patent No. 5,014,917 Issued: May 14, 1991
High Temperature, Flexible Seal
Bruce M. Steinetz and Paul J. Sirocky
Patent No. 4,917,302 Issued: April 17, 1990
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