1.
Analysis of Key Technologies of Turbine Structural Design for High Bypass Ratio Turbofan Engine
大涵道比涡扇发动机涡轮结构设计关键技术分析
2.
As an example, the development of a high bypass ratio turbofan engine was used to demonstrate how the constraints restrict design cycle parameters.
以发展大涵道比涡扇发动机为例,说明了约束条件对设计循环参数的限制。
3.
Numerical Analysis on Matching between Internal and External Bypass and Fan of Aero-engine;
涡扇发动机风扇及内外涵道匹配的数值分析
4.
MIXER INVESTIGATION OF TURBOFAN ENGINE WITH PULSE DETONATION AFTERBURNERS
涡扇-脉冲爆震组合发动机内外涵掺混器研究
5.
Aerodynamic Design and Analysis for Low Pressure Turbine of a Large Scale Turbofan Engine;
某大型涡扇发动机低压涡轮气动设计与分析
6.
Dual-mode Optimization Asymmetry Fuzzy Logic Controller Design for X Aeroengine MFP
某涡扇发动机主燃油通道模糊控制器设计
7.
dual-flow turbojet engine
内外涵涡轮喷气发动机
8.
double-flow engine
内外涵(涡轮喷气)发动机
9.
An airplane with such an engine.
由涡轮风扇发动机提供动力的飞机
10.
Field Repairing Technology of Fan Blades for a Turofan Engine
某型涡扇发动机风扇叶片外场抢修技术研究
11.
Cutaway of the PW 4000112-in(284.48cm) gas turbine engine ,showing fan bypass section.
涡轮发动机剖面图，展示风扇旁路部分。
12.
Performance Deterioration and Control of Military Turbofan Engine
军用航空涡扇发动机性能衰减及控制
13.
An Effective Measure of Enlargement Airstart Envelope for Turbofan Engine--Summary of Assisted Airstart for Aeroengine Starter
1项扩大涡扇发动机空中起动包线的有效措施——浅论航空发动机起动机辅助空中起动
14.
Application of Support Vector Machine in Fault Diagnosis of Aeroengine Test
支持向量机的涡扇发动机试车故障诊断
15.
Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles
高空长航时无人机用涡扇发动机技术分析
16.
Computation and assessment of aerodynamic stability of turbofan engine for missile
弹用涡扇发动机气动稳定性计算与评定
17.
Overview of Advanced Technology for Geared Turbofan Engine (GTF)
齿轮传动涡轮风扇(GTF)发动机先进技术综述
18.
Ideal Starting Procedure Analysis and Optimization Control Investigation for Turbofan Engine
涡扇发动机理想起动过程分析与控制问题探讨