Aircraft fluted core radome and method for making the same |
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| 申请号 | US3795559D | 申请日 | 1971-10-01 | 公开(公告)号 | US3795559A | 公开(公告)日 | 1974-03-05 |
| 申请人 | BOEING CO; | 发明人 | HORN V; KANGAS H; | ||||
| 摘要 | A COMPLEX CONTOURED FLUTED CORE RADOME STRUCTURE FOR AIRCRAFT UTILIZING A RELATIVELY HIGH TEMPERATURE AND HIGH PRESSURE CURE CYCLE FOR LAMINATED FIBER MATERIAL. THE METHOD FURTHER INCLUDES THE UTILIZATION OF REMOVABLE AND REUSABLE FLEXIBLE SILICONE RUBBER MANDRELS ADAPTABLE TO COMPLEX CONTOUR CONFIGURATIONS. THE USE OF THE FLEXIBLE SILICONE RUBBER MANDRELS PERMITS THE USE OF HIGH CURING PRESSURES TO COMPLETELY AND UNIFORMLY FILL THE FLUTES OF THE FLUTED CORE PANEL STRUCTURE AND PRODUCE A STRUCTURAL PRODUCT WITH VERY LOW VOID CONTENT WHICH IS NECESSARY FOR MEETING THE RADAR ELECTRICAL REQUIREMENTS COMBINED WITH IMPROVED MECHANICAL PROPERTIES FOR THE STRUCTURAL REQUIREMENTS. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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