| タイトル | Composite engine duct fabrication |
| 著者（英） | Wilson, A. J.; Stotler, C. L.; Pratt, R. D. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1983-01-01 |
| 言語 | eng |
| 内容記述 | The trimonomer polyimide resin reinforced with graphite fibers, PMR15, is lower in weight (by 20 percent) and less expensive than titanium. The duct walls are of solid laminate and are made of woven T300 graphite cloth. The original concept for the duct involved a solid shell of T300/PMR15 made up of seven plies of cloth tapered to eleven plies at each end. The bosses and built-up areas around the cutouts are also of T300/PMR15. The end flages riveted to the shell, however, are of titanium. A buckling test demonstrated the ability of the composite analytical design techniques employed to predict the buckling strength of the composite shell. Engines tests are described, noting that the successful repair of a hole demonstrated an important advantage over titanium. The development work now being done to eliminate the titanium end flanges is described, noting that an all-composite duct is in prospect. The savings estimated with a titanium-flanged composite duct are $16,891,000 (1982 dollars) and $35,504,000 (then-year dollars); the savings possible with an all-composite duct are put at $27,025,000 (1982 dollars) and $56,806,000 (then-year dollars). |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 83A39941 |
| 権利 | Copyright |
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