| タイトル | Advanced composite elevator for Boeing 727 aircraft, volume 2 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830008059 |
| 著者（英） | Grant, W. D.; Desper, O. E.; Harvey, S. T.; Chovil, D. V.; Mccarty, J. E.; Jamison, E. S.; Syder, H. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1980-11-01 |
| 言語 | eng |
| 内容記述 | Preliminary design activity consisted of developing and analyzing alternate design concepts and selecting the optimum elevator configuration. This included trade studies in which durability, inspectability, producibility, repairability, and customer acceptance were evaluated. Preliminary development efforts consisted of evaluating and selecting material, identifying ancillary structural development test requirements, and defining full scale ground and flight test requirements necessary to obtain Federal Aviation Administration (FAA) certification. After selection of the optimum elevator configuration, detail design was begun and included basic configuration design improvements resulting from manufacturing verification hardware, the ancillary test program, weight analysis, and structural analysis. Detail and assembly tools were designed and fabricated to support a full-scope production program, rather than a limited run. The producibility development programs were used to verify tooling approaches, fabrication processes, and inspection methods for the production mode. Quality parts were readily fabricated and assembled with a minimum rejection rate, using prior inspection methods. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 83N16330
NAS 1.26:159258
NASA-CR-159258 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/163773 |
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