保持燃油流动量均匀。
The fuel flow may include a plume having an angular span.
燃料流可包括具有角跨度的羽 流。
The performance of fuel flow across the nozzle orifice is reported.
文中还介绍了喷嘴流通特性。
Air is introduced at the bottom and act as countercurrent to fuel flow.
空气会在底部和作为燃料流逆流。
A component on the engine for controlling fuel flow for starting and engine operation.
发动机上的一个部件。在发动机起动和运转时控制燃油流量。
The hot fuel flow flight test of Z11MB1 helicopter is first carried out in our country.
直11MB1型机热油飞行试验是风险试飞科目，在国内直升机上首次进行。
At same time, several software sensors of air flow and fuel flow are designed based on regression.
同时根据回归分析方法建立了多个风量软测量模型和给煤量软测量模型。
Finally, the application of the sensor is discussed in measuring fuel flow of an aeronautical engine.
最后给出传感器标定结果，并讨论了在航空发动机燃油测量中的应用。
Check the fuel flow through the system to locate the reason for inadequate fuel supply, correct as require.
检查流过系统的燃油流量以定位燃油供应不足的原因，视需要修正。
Fuel flow indicator of no. 3 engine out of operation (fluctuating) but we found no. 3 engine working normally.
第三发燃油油量显示失效(摆动)，但发动机工作正常。
Therefore, a cooperation method of the frequency and fuel flow should be used for pulse detonation engine control.
所以对于脉冲爆震爆震发动机应采用调节爆震频率和燃气填充相结合的控制策略。
With all the key structural parameters, the fuel flow can be validated according to the traditional experimental equation.
根据输油泵的关键结构参数，按照传统的经验公式进行了输油量的计算校核。
This paper deals with a new optimal method of coordinating air and fuel flow rate with a view to attaining efficient combustion and.
从理论和实践上论述了工业锅炉最佳风煤(或油、气)配合以实现经济燃烧与节能的新观点和新方法。
CROSSFEED, An interconnection between fuel manifolds for fuel flow from one side of the airplane to an adjacent engine or one on the other side.
交输，燃油支管之间的交连设备。 可使燃油从飞机一侧流向邻近的发动机或在机身另一侧的发动机。
Menhwhile, this paper also describes features of air-assisted and liquid-assisted fuel flow metering methods and how they complement each other.
本文还叙述了流量气测法和流量液测法的特点和相互补充的情况。
This paper deals with a new optimal method of coordinating air and fuel flow rate with a view to attaining efficient combustion and. energy-saving.
从理论和实践上论述了工业锅炉最佳风煤(或油、气)配合以实现经济燃烧与节能的新观点和新方法。
Then in order to suppress smoke and save energy, adjustments of fuel flow, injectors, valve clearance and cylinder compression, etc, are performed.
从供油量、喷油器、气门间隙和气缸压力等方面进行调整，以达到消烟节能的目的。
A transient measurement method of the fuel flow using turbine flowmeter in aeroengine trial is introduced. The error sources of transient measure are a...
介绍了涡轮流量计在航空发动机试车燃油流量瞬态测量中的应用，指出了瞬态测量误差的主要来源以及测量时的注意事项。
The results show that the cell potential along fuel flow change little at high current density when low fuel or products concentration area does not appear.
结果表明：在高电流密度情况下，当燃料沿燃料通道方向流动未出现低燃料浓度区或产物浓度区时，电池电势在燃料流动方向上变化不大；
The pump system provides the additional fuel flow necessary to overcome this leanness and maintains smooth engine operation during rapid low-speed acceleration.
加速装置为这种情况提供额外的燃油，从而客服这种问题，使发动机在加速过程中平顺工作。
A transient measurement method of the fuel flow using turbine flowmeter in aeroengine trial is introduced. The error sources of transient measure are also analyzed.
介绍了涡轮流量计在航空发动机试车燃油流量瞬态测量中的应用，指出了瞬态测量误差的主要来源以及测量时的注意事项。
These components are installed between the customer supplied regulation and metering station and the gas fuel flow meter installed just prior to the fuel gas module.
这些部件安装于用户提供的调压计量站和安装在燃气组件前的气体燃料流量计之间。
This latter function is necessary to prevent one form of vapor lock: a stoppage of fuel flow caused by an insufficient amount of atmospheric pressure inside the tank.
特别要防止汽油收缩时，由于油箱内的大气压力不足导致供油中断。
The model inputs include the fuel flow, the nozzle area, the altitude and Mach number, and model outputs include the rotor speed, the temperature and the air pressure.
模型的输入量包括燃油流量、喷口面积、高度及马赫数，输出量则包括高、低压转子的转速及各截面的温度和压力。
The fuzzy-PID control used in temperature control, with temperature departures and the changes and as its input and fuel flow as output, could satisfy the control demand.
对温度用模糊PID控制，以温度偏差和温度偏差变化为输入，燃料流量为输出，这个模糊控制器能满足控制要求。
According to the turboshaft engine's starting fuel flow, starting characteristics was calculated and compared with the engine test data to verify the accuracy of the model.
按照某涡轴发动机起动供油规律，利用建立的数学模型计算了此发动机起动性能，并和发动机试验结果进行比较，以验证模型建立的准确性。
Through feed pump performance tests and the linear regression analysis of test results, the regression equation was established, thus can predicate the fuel flow accurately.
通过输油泵性能测试，对试验数据应用线性回归方法分析，确定回归方程，对输油泵流量进行预测。
The change rules of aerodynamic parameters including lift coefficient, drag coefficient and pitch moment coefficient have been analyzed when Angle of attack and fuel flow rate is changed.
考虑了不同飞行攻角、不同燃料流率下气动参数，包括升力系数、阻力系数和俯仰力矩系数的变化规律。
The response was compared with that obtained through simulation realized by the use of MATLAB and the actual process on different steam flow, feed water flow, fuel flow and control method.
并运用MATLAB仿真工具，针对锅炉水位和汽压调节对象仿真模型在不同的蒸汽负荷、不同给水量、不同燃油量和不同控制方式下的动、静态情况进行仿真研究。
The model static parameters are calculated by unit stable running operating point, and the model dynamic parameters are derived by turbine disturbance and fuel flow disturbance experiments.
模型采用机组稳定运行工况点的数据确定静态参数，利用汽轮机调门开度扰动和燃料量扰动实验确定动态参数。
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