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Ceramic matrix composite turbine engine vane (Document No: 20090002573)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 2008 |
| Description | A vane has an airfoil shell and a spar within the shell. The vane has an outboard shroud at an outboard end of the shell and an inboard platform at an inboard end of the shell. The spar has a first chamber essentially along the suction side and a second chamber along the pressure side opposite the first chamber. |
| File Size | 722750 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20090002573 |
| Archival Resource Key | ark:/13960/t8qc50m7n |
| Language | English |
| Publisher Date | 2008-11-18 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Suction Patents Ceramic Matrix Composites Shrouds Inventions Vanes Airfoils Turbine Engines Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |