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Powder metallurgy rene 95 rotating turbine engine parts, volume 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wilbers, L. G. Redden, T. K. |
| Copyright Year | 1981 |
| Description | A Rene 95 alloy as-HIP high pressure turbine aft shaft in the CF6-50 engine and a HIP plus forged Rene 95 compressor disk in the CFM56 engine were tested. The CF6-50 engine test was conducted for 1000 C cycles and the CFM56 test for 2000 C cycles. Post test evaluation and analysis of the CF6-50 shaft and the CFM56 compressor disk included visual, fluorescent penetrant, and dimensional inspections. No defects or otherwise discrepant conditions were found. These parts were judged to have performed satisfactorily. |
| File Size | 4867587 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830007141 |
| Archival Resource Key | ark:/13960/t9d55g16r |
| Language | English |
| Publisher Date | 1981-01-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Compressor Rotors Rotating Disks Rene 95 Cost Reduction Fluorescence Mechanical Properties Engine Tests Manufacturing Powder Metallurgy Isothermal Processes Turbine Engines Shafts Machine Elements Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
