nacelle

1. As a rule these energy conversion components are accommodated in a machinery housing-referred to as a nacelle.
   这些能量转化组件通常放置在称为机舱的机器外罩中。
2. Strength and mode analysis of wind turbine nacelle chassis with finite element method
   风力发电机组机舱底座强度与模态分析
3. Characteristics and influence factors of total pressure distortion are studied based on tests conducted on a disturbed board installed in the nacelle inlet.
   在吊舱进气道进口安装扰流板进行试验，研究扰流板进气畸变的影响因素及总压畸变特征。
4. Design and Calculation of Nacelle Cover of 3D Sandwich Composites for Wind Power
   3D夹层结构复合材料风电用机舱罩设计计算
5. It introduces the principle of the automatic temperature control system of nacelle for airplane, describes the design of this system, and analyzes the hardware and software of the system.
   介绍了飞机吊舱自动温度控制系统的原理，并对飞机吊舱自动温度控制系统的设计方法进行了阐述，同时对自动温度控制系统的软硬件实现过程进行了分析。
6. Dense smoke coming out of No.4 engine cowling ( engine nacelle), fire suspected.
   第四号发动机整流罩冒浓烟，可能着火。
7. Simulation Study of Helicopter Nacelle Ventilation Cooling System Considering of Downwash Flow
   基于旋翼下洗流场的直升机动力舱通风冷却系统仿真
8. Numerical Complex Flowfield Simulation of Wing/ body/ Pylon/ Nacelle Configuration
   机翼-机身-挂架-短舱复杂流场数值模拟
9. A luffing extension-jib was installed on top of the carriage with a telescopic nacelle.
   在方舱上安装由液压系统控制的可升降伸缩旋转吊臂；在吊臂顶端安装有可折叠吊篮。
10. For these reasons it is imperative in all cases to take the entire wt into consideration-in other words, the drive train with rotor blades, nacelle and tower.
    由于这些原因，任何情况下都必须将整个风力发电机，即传动系统、风轮叶片、机舱和塔架考虑进去。
11. Numerical Simulation Study on Flow Field and Temperature Field of Accessory Nacelle on a Helicopter
    直升机附件舱流场和温度场的数值仿真研究
12. Different nacelle with deeper ross-section and intake over propeller shaft.
    发动机舱、螺旋桨轴处的进气口有一些不同。
13. Different nacelle with deeper ross-section and intake over propeller shaft. inspection certificate of imported motor vehicles
    发动机舱、旋桨轴处的进气口有一些不同。进口机动车辆检验证明
14. Application of Direct Current Torque Motor on the Azimuth Control System of Nacelle
    直流力矩电动机在气球吊篮方位控制系统中的应用
15. Aircraft nacelle comprises engine, engine casing and accessories.
    飞机发动机短舱包容了发动机、机匣、以及各种发动机附件。
16. Electromagnetic Compatibility problem of antenna system in airborne nacelle jammer is studied in this paper. Many methods used in computational electromagnetics, such as Spectral Domain Approach etc, are applied in the predicting analysis and the design of antenna system.
    本文结合机载吊舱式干扰机的研制，深入研究了吊舱式干扰机天线系统EMC问题，将谱域法等计算电磁学当中的混合方法应用于天线系统EMC预测分析和设计。
17. A full digital control system with PC/ 104 in nacelle decoupling mechanism is introduced.
    介绍用PC/104实现高空气球吊篮反捻机构的全数字控制系统。
18. The nacelle was simplified to a rigid body with general motion.
    机舱简化为刚体，具有刚体一般运动。
19. The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment.
    气球吊篮姿态控制系统是吊篮在空中保持姿态稳定、进行姿态调整的关键部件。
20. The finite elements model of the nacelle is created using the non-structure grids by the finite volume method.
    该文利用有限体积法，应用非结构网格，建立了×型直升机发动机舱的有限元模型；
21. A finite difference method for computing the axisymmetric, transonic flows over nacelle is presented in this paper.
    本文考虑轴对称跨音速进气道外流场的有限差分计算方法。
22. The principle of the airborne nacelle jammer used for the test of the new type surface to air missile weapon system is summarized.
    综述了某新型武器系统检验用机载吊舱式干扰机的原理。
23. A linear programming-based dynamic inverse attitude and velocity control method was developed for tiltrotor aircraft operating in helicopter mode with a small degree of nacelle tilting.
    为了研究倾转旋翼飞机短舱倾转过程中的飞行控制问题，提出了一种基于线性规划的动态逆方法，以实现直升机模态下短舱小角度倾转时的姿态和速度控制。
24. The calculation models of flow and heat transfer of helicopter nacelle are created;
    在此基础上，建立了某型直升机短舱流动和换热的计算模型，数值计算了直升机工作在地面最大状态下短舱内部的流动和换热。
25. Results of the calculation show that pylon and nacelle have significant effect on the supercritical wing aerodynamic characteristics.
    计算表明，短舱、挂架对超临界机翼的气动特性有显著的影响。
26. The aeroelastic response of a coupled rotor/ nacelle/ tower system was analyzed using the finite element method based on Hamilton's principle.
    发展了一种理论方法的计算程序，研究耦合转子/机舱/塔架系统气弹响应问题。
27. The cooling research of nacelle
    发动机短舱冷却的计算研究
28. The principle of the airborne nacelle jammer is summarized in this paper.
    针对机载吊舱式干扰机的研制特点，总结和说明了该干扰机的特点和设计的原理。
29. Based on the developed dynamic equations of the coupled rotor, nacelle and wing structures, a MATLAB program was compiled to conduct the model trimming and response computation.
    根据所建立的旋翼、短舱和机翼耦合系统的动力学方程，建立了耦合结构气弹响应的计算方法，用MATLAB编制程序，进行模型配平和响应计算。
30. The shape and internal structure of the nacelle are very complex, Geographical simplification is necessary at first step.
    由于其外形及内部件结构复杂，论文进行了简化并保留机舱外形、热源体及体积较大的内部件。

noun

1. a streamlined enclosure for an aircraft engine