The CNG engine a Variable Nozzle Turbo ( VNT ) turbocharging intercooling system.

Turbo code is a code with excellent channel performance.

Turbo码是一种具有优异性能的纠错编码.

Multi-category faults were common in turbo-pump and other machines.

在涡轮泵等机械设备的故障诊断中,多类故障诊断是经常出现的问题.

The abnormal frequency operation capability of large turbo-generator is reviewed.

讨论大型 汽轮 发电机应具有的频率异常运行能力.

This concept evolved after the introduction of turbo jets in 1958.

1958年引进喷气机后逐渐形成此概念.

Turbo code is a channel code with excellent channel performance. Its decoding applies iterative decoding.

Turbo码是一种性能优异的信道编码, 其译码采用了迭代译码的方法.

The vehicle variable geometry turbocharger ( VGT ) with pneumatic and symmetric nozzle ring vane was researched.

对应用气动型与对称型喷嘴环叶片的车用 可变 几何涡轮增压器进行了研究.

Applying Variable Twin Turbo Technology, a small turbocharger first cuts in at low engine speeds.

应用可变双涡轮增压技术, 一个小涡轮增压器首次削减在发动机低转速.

Oslash ; Liaise directly with customer's engineering departments regarding necessary data to establish the turbocharger match.

直接与客户的技术部门保持沟通,获取必要的数据,建立增压器的良好匹配.

This depends largely on your turbocharger of a correct understanding, use and maintenance.

这在很大程度上取决于您对涡轮增压器的正确认识 、 使用和维护.

Governor , Turbocharger Fuel injection pump, Fuel injection repairing.

调速器,增压器,高压油泵, 油头修理.

After arrival at the port of discharge planning open no. 1 turbocharger.

计划抵达卸货港后打开1号涡轮增压器进行检查.

The supercharger and the turbocharger complement one another ideally in the way they operate.

机械增压和涡轮增压补充另外一个理论的运转方式.

There are many tradeoffs involved in designing a turbocharger for an engine.

在为引擎设计涡轮增压机时,有许多因素的利弊需要权衡.

Weld up one support for the turbocharger.

在增压器焊上一根支撑.

The turbocharger is bolted to the exhaust manifold of the engine.

涡轮增压机连接到引擎的排气管.

turbocharged engines

涡轮增压发动机

A turbocharger helps at high altitudes, where the air is less dense.

涡轮增压机在高原上会带来极大帮助, 因为高原上空气稀薄.

I. Name of Project: Gasoline Engine and Diesel Engine Turbocharger Production Line.

项目名称: 汽油机和柴油机涡轮增压器生产线.

Remove turbocharger oil feed line.

拆卸透平增压器输油管路.

The method is applied to a turbofan engine control system, and is demonstrated to be feasibility.

应用于某型航空涡扇发动机控制系统设计, 仿真结果表明了其可行性.