全机采用不锈钢设计，卫生，易清洗。
All stainless steel structure, hygienic and easy for cleaning.
全机使用灵活轻便，加工面光滑平直。
With flexible and convenient operations. the surfaces processed with the machine appear smooth and straight.
全机机速采用变频调速。
全机采用进口电脑控制。
全机完全取掉皮带及离合器传动，传动效率高。
The loom haven't belt and clutch transmission, transmission efficiency is very high.
全机采用超高速整流子，保证低噪音，及瞬态。
Ultra high speed Rectifiers throughout ensure lower noise and top performance of transient response.
全机集中控制，马达连动调速，安全装置齐备。
The whole machine is centralized control, speed adjustment by motor continuous action, complete safety device.
采用镶有特殊材料的咬牙，全机传递纸张精度提高。
Using the gripper inlaid with special materials, advance the whole machine deliver precision.
全机采用高强度铝合金结构梁组成，超强结构耐久不变形。
The whole machine is composed of high strength aluminum beam structure, super structure, durable without deformation.
以人机对话方式进行各种功能设置，让全机实现人性化智能操作。
All functions set is in the way of man-computer friendly intelligent operation is realized in the whole machine.
以人机对话方式进行各种功能设置，让全机实现人性化智能操作。
All functions set is in the way of man-computer and friendly intelligent operation is realized in the whole machine.
以人机对话方式进行各种功能设置，让全机实现人性化智能化操作。
All functions set is in the way of man-computer, intelligent operation is realized in the whole machine.
全机钢制之机体结构，稳固耐用。长期使用不因粉碎物质影响机械性能。
The body structure of the whole machine is made by steel, solid and durable. The long-term use is not due to crushing material influence the mechanical properties.
全机采用精密线性滑轨配合意大利减速马达，达到流畅运转自如的目的。
This machine adopts precise linear sliding track in accordance with Italian reduction motor to make operation easier and smoother.
换模时非常方便快速，只要用扳手松开，全机可旋转提供上下模的效率。
Using a wrench to loose swing robot to change module, also the entire machine can be revolved to benefit the efficiency of changing module.
在直升机研制阶段，预测全机振动响应是控制直升机振动水平的关键技术。
Accurate prediction of helicopter vibration response is the key techniques for controlling helicopter vibration level during the phase of helicopter development.
质朴坚固的构造、细致合理的设计，使全机所需作业空间缩小，操作灵活简便。
The plain firm structure, the careful reasonable design, cause entire machine to need the working space to reduce, operation nimble simple.
着陆载荷研究：通过撬式起落架功量计算分析，落震试验论及全机着陆载荷特性。
By means of calculation and falling vibration test for ski landing set the characteristics of landing load is discussed in research of landing load.
针对边条弯扭及改变双立尾展向位置对全机纵横向气动特性的影响进行了试验研究。
An experimental study of the effects of the twin vertical fins position and twist strake wing on a fighter aerodynamic characteristics was performed in the wind tunnel.
从理论上计算分析出由于安装阻尼减振装置，在全机各典型部位的减振优化设计的效果。
Theoretically calculate and analyses the effect for dynamical optimize design of the type place of the aircraft due to setting damp reduce thingamy.
通过求解全机纵向运动状态方程，分析了全机模型带与不带机翼边条时纵向动态响应问题。
Aircraft longitudinal dynamic response of the system with and without LEX is analyzed by solving the state equation of aircraft longitudinal motion.
定时器是雷达系统的重要部分，它为雷达全机提供所需的各种主脉冲定时信号和波门定时信号。
Timer is an important part of Radar system, it affords system all the AP timing signals and wave gate timing signals.
静强度载荷研究：通过机体结构强度计算及全机静力试验，论及静载荷下全机的强度与刚度品质；
By means of calculating structure strength of the frame and doing static test of the frame quality of strength and rigidity of the frame are discussed in research of static strength loads.
直升机旋翼系统动部件飞行载荷测量是全机飞行载荷测量的关键，也是直升机寿命可靠性工作的基础。
Helicopter flight load test of rotor system dynamic components is the key part of flight load test of the whole aircraft, and is also the basis of helicopter life reliability calculations.
该模型包含了起落架系统特性和全机气动力特性，根据飞机总体设计参数可仿真给出其起飞性能指标。
On the basis of the vehicle oriented parameters and the aerodynamic characteristics, the history of takeoff is emulated. Simulation studies show that the model is useful in the aircraft design.
新飞机研制必须经全机悬空静力试验验证其结构的强度是否满足强度规范和CCAR 23适航条例要求。
During the design of a new aircraft, the suspended static test must be carried out to test whether its structure can satisfy the need of strength specification and CCAR23 air worthiness test.
民用飞机的维修任务规划包括全机各组成部分的故障影响及可靠性分析、维修工作确定及其间隔优化等内容。
Maintenance task concepts of the civil aircraft include failure effect and reliability analysis of every component, determination maintenance task and optimization interval et al.
民用飞机的维修任务规划包括全机各组成部分的故障影响及可靠性分析、维修工作确定及其间隔优化等内容。
Maintenance task concepts of the civil aircraft include failure effect and reliability analysis of every component, determination maintenance task and optimization interval et al.
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