High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles
| 项目名称： | High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles |
| 摘要： | The objectives of this project are to: (1) design a sapphire optical lever microphone via multiphysics analytical modeling; (2) develop thermocompression fabrication methods for the formation of devices with moving parts out of sapphire and platinum; (3) develop techniques for ultrafast laser micromachining of sapphire for sensor and packaging fabrication; (4) fabrication and packaging of pressure sensors optimized for low-noise and high-sensitivity while possessing minimal drift associated with changes in relative humidity, temperature, etc.; (5) characterize sensors in a simulated, high temperature, pressurized laboratory environment; and (6) implement a hypersonic flow facility (such as Arnold Engineering Development Center, etc.) and/or a gas turbine (such as the Capstone C60 microturbine at the University of Florida, etc.). |
| 状态： | Completed |
| 资金： | 836326.00 |
| 资助组织： | Federal Aviation Administration |
| 项目负责人： | Davidian, Ken；Demidovich, Nicholas |
| 执行机构： | Florida State University, Tallahassee<==>University of Florida, Gainesville |
| 开始时间： | 20110214 |
| 实际结束时间： | 20140531 |
| 主题领域： | Aviation；Vehicles and Equipment |
相关文献
- High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles-FSU
- High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles-UF
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