nozzle pressure的例句大全

because each nozzle pressure varies, so printing plate on the fall in the number of polymer materials also varied.

由于每个喷嘴的水压都有所差别，所以印版上被冲掉的矮分子撮合质料的数目也各不相同。

this principle is to use the ink-jet printing piezo actuator device to be fixed in ink spray nozzle pressure continuous injection.

这栽喷墨打印道理是诳骗压电驱动安设差喷脚洋墨水加以变动不张力，使其不断喷射。

influences of insufficient piston cooling nozzle pressure on diesel engine

活塞冷却喷嘴压力不足对柴油发动机的影响

the vectoring angle increases with the decreasing of the nozzle pressure ratio.

减小喷管落压比可以提高矢量偏转角度。

The affecting factors of the performance parameters of the thrust vectoring nozzle are investigated. And the affect of nozzle pressure ratio, nozzle area ratio and geometric defected angle on the performance parameters is also investigated.

研究了影响矢量喷管性能的因素，研究了压比、面积比以及几何偏角对矢量喷管性能的影响。

As the input power of the film heat source increased, the heat transfer coefficient of spray cooling decreased and tended to decrease significantly under high mass flux and nozzle pressure.

随着薄膜热源的输入功率的升高，其喷雾冷却的换热系数随之减少。当在质量流量及喷嘴压力较高条件下，这种趋势更为明显。

hydraulic pressure, nozzle pressure and cavity pressure sensing locations are shown in figure 11.

光电感应然后就是这个液压式的）液压缸压力、喷嘴压力、模腔压力的感应位置如图11所示。

with increase of nozzle pressure ratio, the infrared radiation from underside of nozzle is reduced.

随着喷管落压比的增加，喷管上方的整体红外辐射降低。

effects of nozzle pressure on disc swirl spun yarn

圆盘式旋流纺的加捻气压对成纱的影响

A measuring method which is named postposition throttle nozzle pressure style pneumatic measuring principle for servo valve's overlap measuring is introduced, and a servo valve's orifice machining quality measuring instrument is developed, which is controlled by computer.

介绍一种后置节流孔压力式气动测量原理用于伺服阀叠合量的气动测量，研制了一台伺服阀阀口加工质量测量仪，并实现了微机自动控制。

The experiment result shows that the area ratio of the nozzle to the throat and the pressure ratio of the work liquid to the gas are the main factors affecting the hydrodynamic performance of the ejector.

研究表明：影响喷射器流体力学性能的主要因素是喷嘴与喉管的面积比及工作流体与吸入气体的压力比。

The particularity of the altitude simulated test of an engine with Laval nozzle was analyzed in brief. The engine thrust determination and correction in altitude test with large deviation of simulated ambient pressure was put forward.

简析了拉瓦尔喷管发动机高空模拟试验的特殊性，提出了大模拟偏差条件下确定和修正拉瓦尔喷管发动机推力的方法。

The effect of operation pressure on the specific impulse of tactical missile solid motors is analyzed from several factors, such as characteristic velocity, thrust coefficient, impulse coefficients of the chamber and nozzle.

从固体发动机的特征速度、推力系数、燃烧室冲量系数和喷管冲量系数等因素出发，分析了发动机工作压强对战术固体火箭发动机比冲的影响。

The relationship model of static head in tundish, atomization pressure on the tip of nozzle and the mass median droplet diameter was established.

本文建立了静压头、雾化压力与雾化熔滴尺寸的模型关系。

The scheme to control launch power is introduced for changeable depth launch of missile. It is to change the aeration area at the nozzle throat of high pressure chamber in launcher.

该文针对导弹变深度发射提出通过改变发射装置高压室喷管喉部的通气面积来实现发射动力可调。

Results show that pintle could change the nozzle throat area and thus the motor pressure and thrust, which provided the capability for thrust control.

结果显示喉栓能够有效改变发动机燃烧室压力和推力，满足发动机推力控制要求。

The characteristic velocity, area of nozzle throat and other parameters are calculated by using the static test results of solid rocket motor ( SRM) and introducing generalized pressure coefficient and thrust coefficient.

利用发动机地面试验结果，引入广义的压强系数和推力系数，计算了发动机的特征速度、喷管喉部面积等参数。

Research on the Method of Calculating Stress intensity Factor of Nozzle Corner Crocks in a Pressure Vessel

压力容器接管角裂纹K1计算方法研究

Development and Application of Rotating Nozzle with High Pressure Water Crevice Seal

高压水间隙密封旋转喷头的研制及应用

The calculation and experiment results show that the maximum lifting pressure performance decreases with the increase in throat diameter of channel of variable section, water flux of low pressure and pressure ratio of steam nozzle, and has its minimum value with water nozzle annular space.

计算及研究表明：极限升压能力随变截面混合腔喉部直径、被升压的低压水流量和蒸汽喷嘴压比增加而降低，随环形水喷嘴间隙的变化出现了最小值；