宇航计测技术
宇航計測技術
우항계측기술
JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT
2013年
6期
17-19,25
,共4页
转速传感器%电磁感应%伺服系统
轉速傳感器%電磁感應%伺服繫統
전속전감기%전자감응%사복계통
Speed sensor%Electromagnetic induction%Servo sgstem
为了满足伺服燃气源恶劣环境条件下的超高速转速测量要求(高温、高转速、强振动、冲击),设计了高温小型化超高速转速传感器。转速传感器是根据电磁感应原理设计的,采取开磁路结构,解决了测量中所面对的高温、高转速的难题,具有体积小、耐高温、准确度高等特点。
為瞭滿足伺服燃氣源噁劣環境條件下的超高速轉速測量要求(高溫、高轉速、彊振動、遲擊),設計瞭高溫小型化超高速轉速傳感器。轉速傳感器是根據電磁感應原理設計的,採取開磁路結構,解決瞭測量中所麵對的高溫、高轉速的難題,具有體積小、耐高溫、準確度高等特點。
위료만족사복연기원악렬배경조건하적초고속전속측량요구(고온、고전속、강진동、충격),설계료고온소형화초고속전속전감기。전속전감기시근거전자감응원리설계적,채취개자로결구,해결료측량중소면대적고온、고전속적난제,구유체적소、내고온、준학도고등특점。
In order to meet the ultra-high-speed turbine speed measurement requirements ( high temperature, high speed, strong vibration, shock) of the servo gas source under harsh environmental con-ditions, designed the high temperature miniaturization and ultra-high speed rotational speed sensor. The speed sensor is designed according to the principle of electromagnetic induction, taking an open magnetic circuit structure which solves the high-temperature, high-speed problems in the face of measurement. This new senor has the characteristics of small size, standing high temperature and high precision.