英语释义

1. an engine designed to power an aircraft
The company plans to build an aeroengine facility in the county, intending to invest $100 million to establish an assembly and test facility for its civil aerospace operations.
— Richmond (Virginia) Times Dispatch, 19 Dec. 2008 Note: Aeroengines will sometimes be used for other types of vehicles, such as boats, if a builder sees a need for unusual performance specifications.

片语

Aero-engine material航空发动机材料

aero-engine performance航空发动机性能

aero-engine components发动机零部件

aero-engine aerodynamics[航]

aero-engine manufacturing航空发动机制造

aero-engine technologies航机技术

aircraft engine[航] 航空发动机；[航] 飞机发动机

aero-engine bearing航空发动机轴承

aero-engine mechanic航空发动机机械师

civil aero-engine民用航空发动机

英汉例句

• By this measurement way we can ensure that the error is very small, and the requirement in testing the blade of aero-engine turbine can be satisfied.

  实验结果表明，采用该测量方法可以保证检测误差小，测量结果直观等特点。从而较好地满足了航空发动机中对叶片壁厚检测的要求。

• The severe safety accidents are induced because the fatigue cracks in fan blade of the aero-engine generally result in the malfunctions of the engine components.

  航空发动机风扇叶片常常因为疲劳裂纹而引起整个结构的损坏，导致重大的安全事故。

• Based on collaborative working platform, full lifecycle management for aero-engine developing projects can be provided.

  基于协同工作平台提供对航空发动机研制项目的全生命周期管理。

• This paper reviews a century of aero-engine development, which can be regarded as a reference to aviation history study.

  本文系统回顾了航空发动机的百年发展，可供航空史研究参考。

• The research of reliable communication is always the key point on aero-engine distributed control system.

  通讯的可靠性研究一直是航空发动机分布式控制系统研究的关键问题。

• The mechanism and impact of aero-engine bearing's skidding damage are analyzed.

  分析了航空燃气涡轮发动机主轴承产生滑蹭损伤的机理与危害。

• In recent years, with the development of aeronautical science and technology, the aero-engine digital control system has been continuously developed and improved.

  近年来，随着航空科学技术的不断发展，对航空发动机数控系统的要求也不断提高。

• Then, based on the plenty analysis of the fundamental aero-engine maintenance task, the breakdown structure of the aero-engine maintenance cost is put forward.

  在分析民用航空发动机基本维修工作的基础上提出了发动机维修成本的组成结构。

• Turbine starter is a very important composing part for aero-engine, its work capability directly affects the reliability of aero-engine in start.

  涡轮起动机是航空发动机的重要组成部分，其工作性能直接影响发动机的起动可靠性。

• According to the calculating methods of current rotor structure dynamic characteristics, a general calculating program of analyzing aero-engine rotor system is developed.

  结合现有的转子结构动力特性计算方法，开发出分析航空发动机转子系统动力特性的通用计算程序。

• BAE is less dependent on big 「platform」 sales than it used to be and now sees itself as a provider of 「through-life support」 for complex systems, much like the aero-engine industry.

  BAE已不再像过去那样依赖大的「平台」销售，它现在更将自己看作是复杂系统的「终身支持」提供商，这很像航空引擎业。

• The effect of advanced fuel temperature on the high altitude ignition performance in the prechamber taken from an existent aero-engine at simulated high altitude facility was studied.

  在高空模拟实验器上，利用已有的航空发动机预燃室点火器，研究了燃油预热增温对高空低压点火性能的影响。

• An integration system is set up to meet the need for information integration in the process of mold design and manufacture and detection of aero-engine turbo blade by investment casting.

  为满足航空发动机涡轮叶片精铸模具设计、制造、叶片铸件检测流程对信息集成的需求，提出构建精铸模具集成设计系统平台。

• Rotor dynamic design is one of the most important aspects of aero-engine design.

  对于航空发动机的设计，转子动力学设计是一个重要的环节。

• According to the statistics data, the maintenance cost of the aero-engine accounts for more than 30 percent of the total operating cost of airlines, which reveals much controllable margin.

  据统计，航空发动机维护成本占据航空公司直接运营成本的三分之一强，有很大的控制余量。

• The review is absolutely necessary matter and phase in the developing process of an aero-engine. The pertinent and effective review is a great help to the aero-engine being developed.

  评审是航空发动机研制过程中一个必不可少，至关重要的阶段，组织缜密、有效地评审对于降低研制风险、缩短周期、减少反复将起到不可或缺的作用。

• Movable bailie pressure distortion generator is an important device in aero-engine stability assessment tests.

  可移动插板式压力畸变发生器是现代航空发动机稳定性评定试验中的一项关键设备。

• So in this paper, research work on the assessment methods of fatigue life reliability analysis of aero-engine components and its application were made.

  本文拟研究航空发动机零构件寿命可靠性试验评估方法及在工程中的应用。

• In this paper, the optimal PID control system for aero-engine was designed using LQR (Linear-Quadratic Regulator) approach.

  本文采用基于LQR的PID控制算法，设计某型号涡扇发动机控制系统。

• Through experiment, the result shows that the method has the advantage of faster learning rate, higher calculating precision, that it can be used to make certain of aero-engine theoretic speed.

  通过试验验证，结果表明该方法具有学习速度快、计算精度高等特点，将其应用于确定航空发动机的给定转速是行之有效的。

• Develop the general version management ante-type system which faces to the design process of aero-engine blade products.

  开发面向设计过程的航空发动机叶片广义版本管理原型系统。

• A new neural network adaptive control scheme is presented and its applications to aero-engine control system are researched.

  本文研究神经网络自适应控制方法及其在航空发动机控制中应用。