K. Petersen, F. Pourahmadi, J. Brown, P. Parsons, M. Skinner, J. Tudor
{"title":"硅熔合制备的谐振束压力传感器","authors":"K. Petersen, F. Pourahmadi, J. Brown, P. Parsons, M. Skinner, J. Tudor","doi":"10.1109/SENSOR.1991.148968","DOIUrl":null,"url":null,"abstract":"A resonant pressure sensor has been fabricated which consists of a single-crystal silicon beam located in the center of a single-crystal silicon diaphragm. The beam is excited electrostatically and its motion are detected by piezoresistors. The structure is fabricated with silicon fusion bonding. Overall measurement accuracies of 0.01% have been achieved. This sensor has been designed to meet the exacting standards required for aerospace air data computers and engine control applications where achievable accuracies of 0.1% absolute pressure are required. The principle of operation is imply to measure the change in resonant frequency of a micromachined silicon beam as the pressure exerted on the sensor's diaphragm is changed.<<ETX>>","PeriodicalId":273871,"journal":{"name":"TRANSDUCERS '91: 1991 International Conference on Solid-State Sensors and Actuators. Digest of Technical Papers","volume":"20 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1991-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"89","resultStr":"{\"title\":\"Resonant beam pressure sensor fabricated with silicon fusion bonding\",\"authors\":\"K. Petersen, F. Pourahmadi, J. Brown, P. Parsons, M. Skinner, J. Tudor\",\"doi\":\"10.1109/SENSOR.1991.148968\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A resonant pressure sensor has been fabricated which consists of a single-crystal silicon beam located in the center of a single-crystal silicon diaphragm. The beam is excited electrostatically and its motion are detected by piezoresistors. The structure is fabricated with silicon fusion bonding. Overall measurement accuracies of 0.01% have been achieved. This sensor has been designed to meet the exacting standards required for aerospace air data computers and engine control applications where achievable accuracies of 0.1% absolute pressure are required. The principle of operation is imply to measure the change in resonant frequency of a micromachined silicon beam as the pressure exerted on the sensor's diaphragm is changed.<<ETX>>\",\"PeriodicalId\":273871,\"journal\":{\"name\":\"TRANSDUCERS '91: 1991 International Conference on Solid-State Sensors and Actuators. Digest of Technical Papers\",\"volume\":\"20 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1991-06-24\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"89\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"TRANSDUCERS '91: 1991 International Conference on Solid-State Sensors and Actuators. Digest of Technical Papers\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/SENSOR.1991.148968\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"TRANSDUCERS '91: 1991 International Conference on Solid-State Sensors and Actuators. Digest of Technical Papers","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SENSOR.1991.148968","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Resonant beam pressure sensor fabricated with silicon fusion bonding
A resonant pressure sensor has been fabricated which consists of a single-crystal silicon beam located in the center of a single-crystal silicon diaphragm. The beam is excited electrostatically and its motion are detected by piezoresistors. The structure is fabricated with silicon fusion bonding. Overall measurement accuracies of 0.01% have been achieved. This sensor has been designed to meet the exacting standards required for aerospace air data computers and engine control applications where achievable accuracies of 0.1% absolute pressure are required. The principle of operation is imply to measure the change in resonant frequency of a micromachined silicon beam as the pressure exerted on the sensor's diaphragm is changed.<>