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NASA-LLIS-0663
Lessons Learned – Welding Practices for 2219 Aluminum and Inconel 718
Year: 2000
Abstract: Practice:
Gas Tungsten Arc Welding and Variable Polarity Plasma Arc Welding are preferred for joining 2219 Aluminum, and Electron Beam Welding is preferred for joining Inconel 718 in critical aerospace flight applications.
Gas Tungsten Arc Welding and Variable Polarity Plasma Arc Welding are preferred for joining 2219 Aluminum, and Electron Beam Welding is preferred for joining Inconel 718 in critical aerospace flight applications.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:16:54Z | |
| date available | 2017-09-04T15:16:54Z | |
| date copyright | 03/06/2000 | |
| date issued | 2000 | |
| identifier other | MLCEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/16226 | |
| description abstract | Practice: Gas Tungsten Arc Welding and Variable Polarity Plasma Arc Welding are preferred for joining 2219 Aluminum, and Electron Beam Welding is preferred for joining Inconel 718 in critical aerospace flight applications. | |
| language | English | |
| title | NASA-LLIS-0663 | num |
| title | Lessons Learned – Welding Practices for 2219 Aluminum and Inconel 718 | en |
| type | standard | |
| page | 11 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext |