1) engine sprocket
发动机链轮
2) motor sprocket,tor sprocket
电动机链轮
3) the driving chain wheel of the scrapping conveyor
刮板机驱动链轮
4) turbine engine
涡轮发动机
1.
Numerical evaluation on infrared radiant intensity of exhaust system of turbine engine without afterburning;
非加力涡轮发动机排气系统红外辐射强度的数值计算
2.
Mathematics model of underwater turbine engine system;
水下涡轮发动机动力推进系统数学模型
3.
Closed-loop control of turbine engine system in super deep operation condition;
超大航深涡轮发动机系统的闭环控制
5) cylindrical cam motor
凸轮发动机
1.
The torpedo cylindrical cam motor with inclining rollers was studied.
以滚轮斜置式鱼雷凸轮发动机为研究对象,运用共轭曲面啮合理论对凸轮工作曲面方程、接触角方程以及诱导主曲率进行了分析,并通过实例验证,为该型发动机的设计、生产提供了理论依据。
2.
Operating conditions of cam and roller tribo-pair has important influence on the operation of the torpedo cylindrical cam motor with inclining rollers.
凸轮-滚轮摩擦副的工作状况对滚轮斜置式鱼雷凸轮发动机的正常工作有着重大影响作用。
6) cam engine
凸轮发动机
1.
Based on the virtual prototype technology and 3-dimension modeling software UG,the correlatively parameterized modeling and assembling for torpedo cam engine are developed using the top-down design idea to transmit the key parameters modified in the top control system to the detailed parts,thus to update the assembled model with the correlative parameters.
基于虚拟样机技术并利用3D建模软件UG对鱼雷活塞式凸轮发动机进行了相关参数化建模和装配,建模中采用了自顶向下的设计思想,使关键参数能够在控制结构顶层中做修改且被向下传播到细节零件,使得相关联参数能够驱动装配体的更新,在此基础上用MSC。
2.
In order to further study the operational mechanism of torpedo cam engine with inclining rollers, this paper presents a method of calculating the parameters of the contact point between the cam and the roller, and preliminarily analyses the loading condition between the roller and the cam.
为了深入研究鱼雷滚轮斜置式凸轮发动机的工作机理,推导了求取该类发动机凸轮接触点参数的方法,对其凸轮与滚轮之间的作用力以及凸轮转矩做了初步分析,并将该类发动机与传统非斜置式发动机进行了比较。
3.
To evaluate the performance of cam engine with the counter-position placement,such a thermodynamic model based on the kinematic and dynamic analysis is developed and the corresponding program with the Runge-Kutta method is established.
为了分析评估对置式凸轮发动机的性能状态,在该发动机关键部件运动学与动力学分析基础上,建立发动机热力学模型,利用改进的龙格-库塔算法进行热力学模型求解与性能仿真。
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