发动机的双语例句-发动机造句-发动机的相关例句-第6页-简答网英语词典

1、

Let us show you to see the engine to test.

让我们指给你看要测试的发动机.

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2、

They tinkered with the engine.

他们修了修发动机。

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3、

They tinkered with the engine…

他们修了修发动机。

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4、

Please don't tinker with my car engine.

请不要乱弄我的汽车发动机.

《现代英汉综合大词典》

5、

Let's implement it in our tiling engine.

让我们在我们的盖瓦发动机中实现它.

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6、

He allowed the engine to tick over for 5 minutes to make it warm up gradually.

他让发动机空转5分钟使其逐渐预热.

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7、

Engine performance is expressed in terms of brake thermal efficiency.

发动机的性能表现在刹车的热效率.

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8、

Rocket motor cases and the specially designed production equipment therefor.

四、火箭发动机的壳体及为其专门设计的生产设备.

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9、

In the process of actual test drive, 1.5 l engine on the throttle response is very sensitive.

实际试驾过程中, 1.5l发动机对油门响应十分灵敏.

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10、

Technical school degree or above, majoring in engine, automotive, marine engineering or related discipline.

技校学位或以上, 主修在发动机, 汽车, 船舶工程或相关学科.

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11、

This design introduces the automobile engine blocks by powder metallurgy technic.

此次设计介绍的是用粉末冶金法制取汽车发动机正时销座的过程.

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12、

However, it won't arrive until 2012, when it will a choice of TSI and TDI engines.

无论如何, 它在2012年前还不会问市,届时, 它的到来将配备TSI或 TDI的发动机,二者二选其一.

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13、

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。

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14、

Zirconia Powders for Air Engine Coatings

航空发动机用氧化锆喷涂粉末

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15、

Repair for honeycomb structure of air engine

航空发动机蜂窝结构的修理

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16、

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

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17、

Numerical simulation of the compressed air engine system

压缩空气发动机系统的数值模拟

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18、

Rotary air engine rotary piston engine of trochoidal type

旋转式热空气发动机

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19、

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。

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20、

As a system, there must be some functional relation between the input and output of the aero engin.

发动机作为一个系统，其各主要输入和输出参数之间必然存在着一定的函数关系。

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