1) straight-clam curve engine
直蚌线发动机
1.
To build the virtual prototype model of straight-clam curve engine,three kinds of software,ADAMS,SOLIDWORKS,COSMOSMOTION,are used.
探讨了刚柔结合多体机械系统动力学仿真的方法,利用SOLIDWORKS,AD-AMS,COSMOSMOTION,三种软件,建立了直蚌线发动机虚拟样机模型,通过动态仿真计算,得到了该发动机的主要运动部件的运动规律;在此基础上,结合ANSYS软件,以柔性前曲轴和后曲轴分别代替刚性前曲轴和后曲轴,再次仿真计算,得到了这两个关键部件在周期性作用力作用下的危险时刻,危险部位,为该发动机的进一步精确的优化提供了依据。
2) free-piston engine
直线发动机
1.
The dynamics and thermodynamics of the free-piston engine was analyzed.
建立了直线发动机的动力学及燃烧模型,通过Matlab/Simulink建模仿真,研究了直线发动机的运行特性,并定性分析了各主要设计、控制参数对系统性能的影响。
3) linear reciprocating generator
直线振动发电机
1.
Performance of novel linear reciprocating generator with external permanent magnet;
新型永磁体外置式直线振动发电机性能研究
2.
Optimization design of linear reciprocating generator based on particle swarm algorithm;
基于粒子群算法的直线振动发电机优化设计
4) Linear generator
直线发电机
1.
Research on linear generator using for high-speed maglev train;
高速磁浮列车用直线发电机研究
2.
Calculation of electromotive force of linear generator used in magnetic levitation vehicle;
磁悬浮列车中直线发电机感应电动势的计算
3.
During its optimization design, perfor- mances of the two sub-systems of linear synchronous motor and linear generator have to be taken into integral considerations.
在对悬浮电磁铁进行优化设计时,需要综合考虑直线同步电机和直线发电机这2个子系统的性能。
5) linear alternator
直线发电机
1.
In this paper,a prototype of a thermoacoustic Stirling electrical power generator(TASEPG) is introduced,which contains a thermoacoustic Stirling heat engine and a linear alternator.
本文介绍了一台由热声斯特林发动机及其驱动的直线发电机组成的热声斯特林发电系统原理样机。
2.
Thermoacoustic power generation technology,which uses a linear alternator to obtain electrical power by conve- rting acoustic work transformed by thermoacoustic engines from heat (including solar energy,geothermal energy and so on),is a novel heat-to-electricity approach.
针对热声发动机驱动直线发电机的热声发电技术中的直线发电机的特性进行了理论研究,考察了驱动频率、负载电阻和活塞直径对发电机性能的影响。
3.
The modeling and simulation of a novel development of the free piston linear alternator were presented.
建立了自由活塞式内燃发电机模型,所建模型主要由自由活塞式内燃机与直线发电机两部分组成。
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条