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ANALYSIS AND PREDICTION OF INTERFERENCE IN ASSEMBLING CURVED BEVEL GEARS 被引量:1
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作者 Gong Daoxiang (Chongqing University) Shigeyuki Shimachi(Iwate University, 020,Japan)Masana Kato( Tohoku University,980,Japan) 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 1996年第1期79-83,共3页
The phenomena of interference in the course of assembling curved bevel gears are ana. lysed and the corresponding prediction program of interference is established taking KlingInberg bevel gear as an exmple.... The phenomena of interference in the course of assembling curved bevel gears are ana. lysed and the corresponding prediction program of interference is established taking KlingInberg bevel gear as an exmple. The factors influencing interferenee are discussed and the coneept ofcritical cutter radius is proposed. Finally, a simplified approximate function between the critical cutter ra- dius and the other factors is derived,and the designing method of avoiding interferenee is provided. The analysis and caiculation are proved to consistent with a case of actual product. 展开更多
关键词 Gear Curved bevel gear Assembly interference Design parameter effect
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A method for aircraft magnetic interference compensation based on small signal model and LMS algorithm 被引量:4
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作者 Zhou Jianjun Lin Chunsheng Chen Hao 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2014年第6期1578-1585,共8页
Aeromagnetic interference could not be compensated effectively if the precision of parameters which are solved by the aircraft magnetic field model is low. In order to improve the compensation effect under this condit... Aeromagnetic interference could not be compensated effectively if the precision of parameters which are solved by the aircraft magnetic field model is low. In order to improve the compensation effect under this condition, a method based on small signal model and least mean square(LMS) algorithm is proposed. According to the method, the initial values of adaptive filter's weight vector are calculated with the solved model parameters through small signal model at first,then the small amount of direction cosine and its derivative are set as the input of the filter, and the small amount of the interference is set as the filter's expected vector. After that, the aircraft magnetic interference is compensated by LMS algorithm. Finally, the method is verified by simulation and experiment. The result shows that the compensation effect can be improved obviously by the LMS algorithm when original solved parameters have low precision. The method can further improve the compensation effect even if the solved parameters have high precision. 展开更多
关键词 Adaptive filter Aeromagnetic survey Aircraft magnetic interference Least mean square algorithm Magnetic interference compensation Model parameter
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