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An Optimized Air-Core Coil Sensor with a Magnetic Flux Compensation Structure Suitable to the Helicopter TEM System

机译：具有适用于直升机TEm系统的磁通补偿结构的优化空心线圈传感器

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Chen Chen; Fei Liu; Jun Lin; Kaiguang Zhu; Yanzhang Wang;
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1. Design of Cable Parallel Air-Core Coil Sensor to Reduce Motion-Induced Noise in Helicopter Transient Electromagnetic System [J] . Fei Liu, Jun Lin, Yanzhang Wang, Instrumentation and Measurement, IEEE Transactions on . 2019,第2期

机译：减少直升机瞬变电磁系统中运动感应噪声的电缆并联空心线圈传感器的设计
2. Investigation and Optimization of the Performance of an Air-Coil Sensor with a Differential Structure Suited to Helicopter TEM Exploration [J] . Chen Chen, Fei Liu, Jun Lin, Sensors . 2015,第9期

机译：适用于直升机TEM探查的具有差分结构的空气线圈传感器的性能研究和优化
3. Reducing Motion-Induced Noise With Mechanically Resonant Coil Sensor in a Rigid Helicopter Transient Electromagnetic System [J] . Liu Fei, Lin Jun, Wang Yanzhang, IEEE Transactions on Industrial Electronics . 2020,第3期

机译：在刚性直升机瞬变电磁系统中使用机械共振线圈传感器降低运动引起的噪声
4. Development of AC exciting magnetic levitation system using an air-core coil [C] . Shinichi Kawano, Yoshihisa Hirane 電気学会全国大会 . 2001

机译：使用空心线圈的AC激励磁悬浮系统的开发
5. Development of an airborne torque (Q) compensation system for the Advanced Systems Research Aircraft (ASRA) and the CH146 Griffon helicopter (CFUTTH). [D] . Alstrom, Robert Bruce. 2002

机译：为高级系统研究飞机（ASRA）和CH146 Griffon直升机（CFUTTH）开发了机载扭矩（Q）补偿系统。
6. An Optimized Air-Core Coil Sensor with a Magnetic Flux Compensation Structure Suitable to the Helicopter TEM System [O] . Chen Chen, Fei Liu, Jun Lin, 2016

机译：具有适用于直升机TEM系统的磁通量补偿结构的优化空芯线圈传感器
7. Investigation and Optimization of the Performance of an Air-Coil Sensor with a Differential Structure Suited to Helicopter TEM Exploration [O] . Chen Chen, Fei Liu, Jun Lin, 2015

机译：适用于直升机透射电镜探测的差动结构空气线圈传感器性能研究与优化
8. Design study of the vertical field coil systems and Air-Core transformer for tokamaks without Conducting shell [R] . H. Watanabe, Y. Funato, S. Magao 1978

机译：无导电壳的托卡马克垂直场线圈系统和空心变压器的设计研究

An Optimized Air-Core Coil Sensor with a Magnetic Flux Compensation Structure Suitable to the Helicopter TEM System

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