原文传递
Icing Sensor Probe
| 题名： | Icing Sensor Probe |
| 作者： | Emery, Edward; Kok, Gregory L. |
| 关键词： | sensor；probe；measurement；lightweight；characteristics；technology；particle；proportion；bandwidth；development |
| 摘要： | Aircraft icing is a serious safety problem for the general aviation and some commuter transport airplanes. There has been tremendous growth in the commuter aviation industry in the last few years, Since these type of aircraft generally operate at lower altitudes they consequently spend a far greater proportion of their time operating in icing conditions. For the past thirty years airborne and ground based facilities have relied primarily on two types of cloud physics instrumentation to measure the characteristics of icing clouds hot wire liquid water content probes and laser based particle sizing probes for the measurement of water droplet size. The instrumentation is severely limited by the technology that was developed during the 1970's and is quite large in size. The goal of this research is to develop one instrument with a wide bandwidth, better response time, higher resolution, user selectability, and small and lightweight. NASA Glenn Research Center, Droplet Measurement Technology, and Meteorology Society of Canada have developed a collaborative effort to develop such an instrument. This paper describes the development and test results of the prototype Icing Sensor Probe. |
| 报告类型： | 科技报告 |
相关文献
- Prospects for the Acquisition of Icing Data from Operational Aircraft
- Continuous measurement of aircraft wing icing
- Five-Hole Flow Angle Probe Calibration for the NASA Glenn Icing Research Tunnel
- Overview of Mount Washington Icing Sensors Project
- A STUDY OF SENSOR FUSION TECHNOLOGY FOR TRAFFIC INFORMATION SERVICES EMPLOYING WIDE RANGE COMMUNICATION MEDIA.
- Irregularly Sampled Transit Vehicles Used as a Probe Vehicle Traffic Sensor
检索历史
应用推荐
