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Seal development for the hsct combustor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jarmon, David C. |
| Copyright Year | 2006 |
| Description | The combuster section of the High Speed Civil Transport (HSCT) requires high temperature seals to minimize leakage between CMC components. The temperature requirements range from 1500 F to 2100 F and the compression requirements range from 10% to 50%. Three distinctly different Nextel braided seals have been developed to seal areas such as the bulkhead heatshields and lean zone outer liner. The seals range from 0.10" dia. rope to triangular braid with 1" sides. |
| File Size | 5671478 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080003278 |
| Archival Resource Key | ark:/13960/t89h0mr84 |
| Language | English |
| Publisher Date | 2006-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Ceramic Matrix Composites Civil Aviation Linings Heat Shielding High Temperature Supersonic Transports Bulkheads Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |