Loading...
Please wait, while we are loading the content...
Similar Documents
High temperature turbine engine structure (Document No: 20080004017)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1994 |
| Description | A high temperature ceramic/metallic turbine engine includes a metallic housing which journals a rotor member of the turbine engine. A ceramic disk-like shroud portion of the engine is supported on the metallic housing portion and maintains a close running clearance with the rotor member. A ceramic spacer assembly maintains the close running clearance of the shroud portion and rotor member despite differential thermal movements between the shroud portion and metallic housing portion. |
| File Size | 753932 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080004017 |
| Archival Resource Key | ark:/13960/t75t8k00m |
| Language | English |
| Publisher Date | 1994-01-18 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Patents Atmospheric Temperature Ceramics High Temperature Turbine Engines Rotors Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
