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Combustor liner construction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wagner, W. B. Craig, H. M. |
| Copyright Year | 1983 |
| Description | A combustor liner is fabricated from a plurality of individual segments each containing counter/parallel Finwall material and are arranged circumferentially and axially to define the combustion zone. Each segment is supported by a hook and ring construction to an opened lattice frame with sufficient tolerance between the hook and ring to permit thermal expansion with a minimum of induced stresses. |
| File Size | 360487 |
| Page Count | 5 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840016509 |
| Archival Resource Key | ark:/13960/t6353gp8v |
| Language | English |
| Publisher Date | 1983-11-15 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Panels Turbocompressors Structural Members Cooling Temperature Effects Temperature Gradients Gas Turbine Engines Linings Cooling Systems Segments Combustion Chambers Thermal Stresses Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
