一种主被动复合隔振器设计研究
[Abstract]:In order to solve the defects of the traditional passive vibration isolation method in controlling the vibration of marine diesel engine and meet the higher and higher requirements of ship vibration, a new type of active and passive composite isolator is designed and developed in this paper. In this paper, it is designed on the basis of the traditional passive double-layer passive vibration isolation system, and a secondary force source device is added to output the excitation force to the intermediate mass of the system, and the secondary excitation force is controlled by the appropriate control algorithm. The external energy is input to the controlled vibration system to reduce the transmission rate of the system force in order to achieve the predetermined goal of vibration control. The active and passive composite isolator is mainly composed of upper and lower two layers of vibration isolator, which is used as the intermediate platform of intermediate mass, as well as four inertial electromagnetic actuators and power amplifiers installed on the intermediate platform. The research work of this paper revolves around the design of inertial electromagnetic actuator and the overall structure design of active and passive composite isolator in active and passive composite isolator. The principle of vibration isolation is deeply analyzed and the part drawings of each part are designed. After processing and production of each part of the parts, and finally assembled into a prototype. The main work of this paper is as follows: 1. Based on the basic principle of vibration isolation, this paper focuses on the characteristics of two-layer vibration isolation system and double-layer active control vibration isolation system, and provides the necessary theoretical basis for the design of passive composite isolator. 2, The design of magnetic circuit of inertia electromagnetic actuator is completed. ND-Fe-B rare earth permanent magnet material is selected as permanent magnet in actuator magnetic circuit and 10 # steel is selected as soft magnetic material. The effects of yoke iron thickness, magnetic cylinder thickness and magnetic cylinder length on the magnetic circuit characteristics of the designed ND-Fe-B permanent magnet are analyzed in detail by using Ansoft electromagnetic field finite element analysis software. The important components of inertia electromagnetic actuator spring and fan are calculated. According to the results of simulation and calculation, the parts of inertial electromagnetic actuator are designed in detail by using AutoCAD software, and the two-dimensional effect model of inertial electromagnetic actuator is established by Pro/e modeling software. After the machining of each part, the inertial electromagnetic actuator is assembled, and its performance is tested in detail. The test results show that the four inertial electromagnetic actuators have good performance and can be used as the secondary excitation force of the active vibration control system. 3, The nitrile rubber (NBR) with Shaw hardness of 60~70HS was determined as the material of the upper and lower two layers of vibration isolation rubber, and according to the size of the active and passive composite isolator, the vibration isolation rubber assembly of the upper and lower layers was designed. The deformation of the rubber assembly under the condition of bearing 5 tons of static load is calculated. Through theoretical calculation and comparison of the calculation results of Ansys, it is shown that the deformation of the vibration isolation rubber assembly designed in this paper is completely within the allowable range. Finally, the design of other components of the active and passive composite isolator is completed, and the three-dimensional model is established according to the juice setting drawings. After the processing of each part, the active and passive composite isolator is assembled. Adequate preparation has been made for the active vibration control test.
【学位授予单位】:哈尔滨工程大学
【学位级别】:硕士
【学位授予年份】:2014
【分类号】:TB535.1;U664.121
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