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Materials for advanced turbine engines. volume 1; power metallurgy rene 95 rotating turbine engine parts
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shamblen, C. E. Gorsler, R. W. Mosier, J. S. Pfouts, W. R. Peebles, R. E. |
| Copyright Year | 1979 |
| Description | An attempt was made to improve methods for producing powder metallurgy aircraft gas turbine engine parts from the nickel base superalloy known as Rene 95. The parts produced were the high pressure turbine aft shaft for the CF6-50 engine and the stages 5 through 9 compressor disk forgings for the CFM56/F101 engines. A 50% cost reduction was achieved as compared to conventional cast and wrought processing practices. An integrated effort involving several powder producers and a major forging source were included. |
| File Size | 58220392 |
| Page Count | 364 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800019998 |
| Archival Resource Key | ark:/13960/t6sz13r0q |
| Language | English |
| Publisher Date | 1979-06-01 |
| Access Restriction | Open |
| Subject Keyword | Metallic Materials Forging Hot Pressing Heat Resistant Alloys Cost Reduction Powder Metallurgy Engine Parts Turbine Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
