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High temperature turbine engine structure (Document No: 20080004416)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1991 |
| Description | A hybrid ceramic/metallic fastener (bolt) includes a headed ceramic shank carrying a metallic end termination fitting. A conventional cap screw threadably engages the termination fitting to apply tensile force to the fastener. |
| File Size | 557335 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080004416 |
| Archival Resource Key | ark:/13960/t7wm6671c |
| Language | English |
| Publisher Date | 1991-04-30 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Fasteners Patents 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 |