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Smart skin technology development for measuring ice accretion, stall, and high AOA aircraft performance. Part 1 Capacitive ice detector development
| 题名： | Smart skin technology development for measuring ice accretion, stall, and high AOA aircraft performance. Part 1 Capacitive ice detector development |
| 作者： | Pruzan, Daniel A.; Khatkhate, Ateen A.; Gerardi, Joseph J.; Hickman, Gail A. |
| 关键词： | development；technology；measur；forman；smart；perform；accr；apac；ring；etec |
| 摘要： | A reliable way to detect and measure ice accretion during flight is required to reduce the hazards of icing currently threatening present day aircraft. Many of the sensors used for this purpose are invasive (probe) sensors which must be placed in areas of the airframe where ice does not naturally form. Due to the difference in capture efficiency of the exposed surface, difficulties result in correlating the ice accretion on the probe to what is happening on a number of vastly different airfoil sections. Most flush mounted sensors in use must be integrated into the aircraft surface by cutting or drilling the aircraft surface. An alternate type of ice detector which is based on a NASA patent is currently being investigated at Innovative Dynamics, Inc. (IDI). Results of the investigation into the performance of different capacitive type sensor designs, both rigid as well as elastic, are presented. |
| 报告类型： | 科技报告 |
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