发动机的例句大全

Let's take a look at the gas engine.

让我们看一看燃气发动机.

Check the engine tail pipe on metal particles and visible damage.

检查发动机尾喷管无金属颗粒和损坏.

Oil is seeping from the engine.

油从发动机中渗出.

Hola, buenos d í as. Mi choche no funciona , creo que es el motor.

嗨, 你好! 我的汽车不好使了, 我相信是发动机的问题.

In high-speed driving, the muted effects of this engine satisfactory.

在高速行驶中, 这款发动机的静音效果让人满意.

No significant change of the engine response to fuel step was found.

而在一定的不同矢量角作用下,发动机的阶跃响应过程调节参数无明显变化.

The research and establishment of graphics library of aero-engine rotor system structure scheme

航空发动机转子系统结构方案图形库的研究与建立

The improvement of surface properties of engine aluminum alloy pistons and outer garments of the electric radiation tubes in some carburizing furnaces was achieved by the micro-arc oxidation technology and investigated.

采用微弧陶瓷化技术对发动机铝活塞及电辐射管热强钢外套管进行表面改性研究。

The gas-film sealing technology is a kind of advanced structure for the sealing of the main axis of aeroplane engine.

航空发动机轴间气膜密封技术是一种先进的结构。

Repair Technique and its General Situation of Aeroplane Engine Bearing

发动机轴承修理技术及其概况

Zirconia Powders for Air Engine Coatings

航空发动机用氧化锆喷涂粉末

Repair for honeycomb structure of air engine

航空发动机蜂窝结构的修理

Study on wear particle size distribution of air engine with its application to wear monitoring

发动机磨粒统计分布规律与磨损状态监测研究

Numerical simulation of the compressed air engine system

压缩空气发动机系统的数值模拟

Rotary air engine rotary piston engine of trochoidal type

旋转式热空气发动机

Based on this, the synthetical control of the geometric and the surface quality of parts is established in the processing course, This is the new effective method of improving the reliability and service life of the thin-wall parts of complicated shap under high-load in aircraft engine.

以此为基础，在加工过程中，对零件的几何质量和表面层质量进行了综合控制。研究表明，该方法是提高飞行器发动机中高负载复杂形状薄壁零件可靠性和寿命的有效新途径。

EPDM ( Ethylene Propylene Diene Monomer) is used as the insulation on chamber wall of SPRM. It is a good protective material of charring type. During being heated it formed the charring and pyrolytic layers.

作为固体火箭发动机燃烧室壁面绝热层的EPDM是一种炭化型热防护材料，受热时形成炭化层和热解层，在燃气和粒子冲蚀下不断减薄并带走热量，有效地保护燃烧室壁。

Taking aft-end igniter design for a rocket motor for example, design methods for ignition sequence, amorce quantity estimation and nozzle closure were described respectively.

以某型号发动机尾部点火设计为研究对象，对点火序列设计、点火药量的估算、喷管堵片的设计方法进行了阐述。

Based on the experimental formula of fore-ignition design, the initial amorce mass of a small solid rocket motor with end-and-lateral burning grain and aft-ignition manner was estimated firstly.

采用头部点火设计经验公式对端面-侧面燃烧、尾部点火的小型固体火箭发动机点火药量进行了初步估算。

Method of amorce mass estimation for solid rocket motor

固体火箭发动机的一种点火药量估算方法