1、

Because of Various kind of reason, a most of boiler exist problem of positive pressure combustion or a large furnace in run.

由于各种原因,多数锅炉在运行中存在着正压燃烧或炉膛负压值太大等问题。

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3、

This paper analyzes the coal mixed match, boiler combustion and sliding pressure operating of steam turbines, building the fuzzy math model of coal mixed match, boiler combustion advanced control model based on parameter prediction and steam turbine advanced operating model based on sliding pressure operation.

本文通过对燃煤掺配、锅炉燃烧、汽轮机滑压运行进行系统分析,建立了混煤掺配的模糊数学技术模型、基于参数预测的锅炉燃烧优化控制模型和基于滑压运行的汽轮机优化运行模型。

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5、

Based on the characteristics of pulse combustion and actual situation that air gas flow can not be measured accurately, pulse combustion furnace temperature discrete optimization model and air gas pressure control model.

基于脉冲式燃烧的特点和空煤气流量无法准确测得的现实情况给出了脉冲燃烧炉温控制离散化优化模型和空煤压力控制模型。

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6、

Testing results given, the effect of the evil conditions is studied emphatically on the maximum combustion pressure, exhaust temperature and turbocharger surge.

文章给出了试验结果,并着重研究了它们对爆发压力、排气温度以及增压器喘振的影响。

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7、

The combustion rate of propellant at any pressure can be obtained by one test of closed burner method, and closed burner method will be an effective tool to study new style propellant working under high pressure.

密闭燃烧器法一次测试可测出全部压强下推进剂燃速,可成为高压高燃推进剂研制的有效工具。

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8、

Through fault simulation, main factors which influence the performance of Two-stroke diesel engine were analyzed. And when faults gradually deepen, main performance factors of diesel engine including effective power, fuel consumption rate, IMEP, maximum combustion pressure was also analyzed.

通过故障模拟,分析了影响低速二冲程柴油机性能的主要因素,及在故障逐渐加深时,柴油机主要性能参数(有效功率、燃油消耗率、平均指示压力和最大爆发压力等)变化规律。

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9、

This paper presents the development of the liquid propellant rocket engine technology from the viewpoint of combustion chamber pressure, thrust level and power cycle.

本文从燃烧室压力、系统工作循环方式以及最大推力三个方面叙述了世界各国液体火箭发动机的技术水平。

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10、

It's verified that a series of intense pressure impulses can occur in the combustion chamber after the thrust reversal nozzles of the solid rocket motor are suddenly opened.

实验表明,突然打开固体火箭发动机反向喷管后,燃烧室中可能出现强烈的压力冲击,这种压力冲击来自喷管喉部节流和形成准稳态流动之前的非定常过程。

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11、

The signal-to-noise ratios of both the cylinder cover vibration signal and the responding cylinder pressure signal of the training samples are effectively enhanced by time statistic average method, and Kaiser differentiator improves the identification of timing of combustion.

时域统计平均有效提高了信号的信噪比,对柴油发动机气缸压力的恢复获得了很好的结果;Kaiser差分器有效提高了对燃烧始点的辨识。

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12、

Identification of Cylinder Pressure of Internal Combustion Engines Using Time Series Method

用时间序列方法识别内燃机缸内气体压力

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13、

In this system the crankshaft rotating angle, where the peak combustion pressure occurs, is taken to be a feed back signal, so that the ignition timing of the engine is able to be controlled.

该控制系统利用最高燃烧压力点的曲轴转角作为反馈信号,实现其对发动机点火正时的控制。

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14、

Combustion fuel gas apparatus LPG vapor pressure tester

燃烧燃料排气测定器液化石油气蒸气压力测定仪

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16、

According to experimental results, a simplified analysis method dependence on linear inclination slope calculated of signal regression was proposed for pressure fluctuate normalized singals at different combustion condition and a useful classified combustion condition could be obtained from| K|.

提出了一种通过压力脉动信号分析燃烧状态的简单有效方法,该方法对归一化后压力脉动信号作线性回归并计算回归直线斜率K,根据K值对燃烧状态进行分类判断。

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17、

Analysis of New Pulverized Coal Combustion Technology of Super Critical Pressure Boiler

超临界和超超临界锅炉煤粉燃烧新技术分析

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18、

A mathematical model describing combustion in a high pressure liquid hypergolic bipropellant ( UDMH/ H2O4) rocket engine combustor has been developed.

本文提出了一个高压液体双组元自燃推进剂火箭发动机燃烧室计算模型。

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19、

Combustion Control of Base Bleed Unit at Pressure Transition

底排装置在压力跃变条件下的燃烧控制

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20、

The theoretical combustion temperature and explosive pressure are calculated with different air concentration for three kinds of urban gas.

计算了常用的3种城市燃气不同空气系数下的理论燃烧温度和爆炸压力。

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