aircraft engine的例句大全

d-s theory and application in fault diagnosis of aircraft engine oil system

D-S证据理论及其在滑油故障诊断中的应用

structural design of mid-span shrouds for aircraft engine fan blades

航空发动机风扇叶片凸肩的结构设计

The MATLAB achievement of aircraft engine bearing rollers fault testing

飞机发动机轴承滚动体故障诊断的MATLAB实现

This computer enhanced photo shows what a Cushman scooter would look like with a1/ 3 scale Rolls Royce Merlin V-12 aircraft engine tucked under the gas tank.

这台电脑增强照片显示，一个库什曼滑板车看起来就像一个1/3的规模劳斯莱斯梅兰V型12架飞机发动机藏下的油箱。

knowledge base building in the expert system of aircraft engine spectrometric oil analysis

航空发动机滑油光谱专家系统知识库建立

2010-01-17 avic commercial aircraft engine co. ( avic/ acae) recently started building a research and development center to develop engines for domestic-made jumbo jets in shanghai.

2010年01月17日中国航空工业集团商用飞机发动机有限公司的研发基地近日在上海开始建设，它将打造民用飞机的“中国心”。

the metal shell of the aircraft engine

飞机发动机的金属外壳

The Welding and Patch Welding of the Thermal Intensity Alloy Assembly in Aircraft Engine

航空发动机中热强合金组件的焊接与补焊

Studying Frequency Veering Characteristics of Aircraft Engine Blade with Beam Function Combination Method

航空发动机叶片频率转向特性研究

Take the example of three point contact ball bearing applied on the spindle of advanced aircraft engine, its dn value and work temperature are very high, often causing the contact thermal failures.

如先进航空发动机主轴采用的三点接触球轴承，其dn值和工作温度非常高，经常造成摩擦副发生热失效。

The measurement of impact-scraping load displacement curve of sealing coating used in aircraft engine can be done with the electronic impact-scraping tester developed by ourselves.

利用自制的电子冲击刮削试验机，测试封严涂层的冲击刮削载荷-位移曲线。

The influence of the pressure and temperature distortion to the engine stability is one of important target to evaluate aircraft engine. The fan and compressor is the most sensitive part to the air current.

压力和温度畸变对发动机稳定性影响的评定是当代航空燃气涡轮发动机适用性战术指标的重要内容之一。

To turn off ( an aircraft engine) while in flight.

关引擎在飞行中关掉（飞机的一个引擎）

Method of failure reporting, analysis and corrective action system model for aircraft engine

航空发动机故障报告、分析和纠正措施系统模型的构建

According to the total pressure and temperature distortion question in the aircraft engine using process, this article closely track overseas development tendency and develop one mathematics physical model to evaluate the compressor system stability.

本文根据当前航空发动机使用过程中遇到的总压和温度畸变问题，紧密跟踪国外发展趋势，发展了一种在发动机环境下评定航空燃气涡轮发动机压缩系统稳定工作边界的数学物理模型。

Stability Analysis of Experimental AMB Prototype for Aircraft Engine

实验用航空发动机磁悬浮轴承样机的稳定性分析

A turboprop handles a larger airflow than any other aircraft engine and so ( at low speeds) generates the largest thrust for any given rate of fuel consumption.

一个涡桨可以比其他的飞机发动机多处理一些气流，因此在低速时，无论给定的燃料占总量的比例是多少，都会产生最大的推力。

In this paper, the effect of the contents of the impurity elements such as oxygen, iron, nitrogen in TC11 titanium alloy on the performance of aircraft engine disk by isothermal forging was analysed.

分析了TC11钛合金中氧、铁、氮等杂质元素含量对应用等温锻造工艺生产的航空发动机盘件的性能影响。

Protective Coating of Modified Silicon Sol on the surface of Magnesium Alloy in Aircraft Engine

发动机镁合金件改性硅溶胶防护涂层的研究

This essay, according to the Huygens Superposition the theorem makes a qualitative analysis of the distributing character of dipole sound field and mainly introduces the formation and function of the aircraft engine ground trial active noise reduction system which is designed by us.

本文根据惠更斯叠加原理，定性分析了偶极子声场分布的特点，简要介绍了我们研制的喷气飞机地面试车主动式降噪系统的组成及其功用。