blade tip

A New Type of Composite Material Rotor Blade Tip Structure

一种新型复合材料旋翼桨尖结构形式

Experimental Study of the Effect of Blade Tip Clearance on Turbine Performance

间隙尺寸对涡轮叶栅气动性能影响的实验研究

The flow in blade tip region under different clearance conditions

不同间隙条件下的叶顶区流动

Application of CAD in Blade Tip Grounding Tool Design

CAD技术在磨叶片叶尖工具中的应用

Repairing Technology of High Pressure Turbine Blade Tip Crack for an Aero-Engine

某型发动机高压涡轮叶片叶尖裂纹修复工艺研究

Studies of Flow and Heat Transfer Characteristic on the HPT Blade Tip

高压涡轮转子叶片端面的流动与换热特性研究

Numerical simulation of film cooling in rotating blade tip

旋转涡轮叶片端部气膜冷却的数值计算

Development of Rotating Linear Cascade Facility for Simulating Blade Tip Clearance Flow

模拟叶尖间隙流的转动平面叶栅实验方案

Effect of temperature and rotational speed on radial clearance of turbine blade tip

温度与转速对涡轮叶尖径向间隙的影响

PIV investigation of blade tip flow in open axial fan

开式轴流风扇叶尖流动的PIV实验研究

Effect of different incidences on turbine cascades flow in blade tip clearance

冲角变化对涡轮叶栅内间隙流动的影响

Optical fiber sensor for blade tip clearance measurement

叶片叶尖间隙测量的光纤传感器

Blade Tip - timing Measurement for Turbine Blade Vibration

汽轮机叶片振动的叶端定时测量法

The theory and the characteristics of the force caused by the blade tip clearance are analyzed .

分析了叶轮偏心引起转子失稳的机理和特点。

One of these primary methods is adjusting the distance between the engine casing and blade tip .

其中，调整发动机转子叶尖间隙的距离就是提升其性能的主要方法之一。

Blade tip clearance detection is an important part in the aircraft engines ' research and maintenance work .

航空发动机叶尖动态间隙检测是航空发动机研制和维护的重要组成部分。

Application of superheterodyne FM reception in measurement of blade tip clearance

超外差调频接收技术在叶尖间隙测量中的应用

Experimental investigation of the vibration suppression in a blade tip seal by air injection or pumping

喷射或抽取气流抑制叶顶密封气流激振的实验研究

Recommend a saw blade tip profile abrasive band arc grinder

推荐一种锯片刀头仿形砂带磨弧机

Metallographic Analysis of Grinding Burn of Spindle Blade Tip

锭尖磨削烧伤的金相分析

Verification Test of Troubleshooting Concept for an Aeroengine Compressor Rotor Blade Tip Crack Failure

某型发动机压气机转子叶片叶尖裂纹故障排除方案试验验证

Effects of rotor blade tip clearance on total aerodynamic performance in a radial inflow turbine

叶轮顶部间隙对向心透平总体性能影响的研究

Analysis of the flow through the blade tip clearances of axial pumps by CFD

轴流泵叶顶间隙流动的计算流体动力分析

Effect of Blade Tip Corners on Performance of Ducted Propellers

叶梢尖角对导管桨性能的影响

The gas exciting force caused by blade tip clearance may cause rotors unsteady under certain condition .

转子偏心引起的气流激振力在一定条件下可能诱发转子失稳。

The blade tip eddy in axial fan without external duct is observed and caught during experiment .

实验中观测并捕捉到了无外风筒时轴流通风机内的叶尖涡。

3D LDV measurements of rotor blade tip vortex in hover

利用三维激光测速方法研究悬停状态下的桨尖涡

Among them , ascending the load will add the leakage from blade tip and cause the separation easier .

其中，压气机级负荷的提升将导致叶顶泄漏更加严重，叶片分离更加容易。

Regions of high viscous effects have been found to be located near the shroud rather than the blade tip .

发现高黏度效应区域位于上端壁附近而不是在叶片顶部。

Research on turbofan engine HP-compressor rotor-12 blade tip clearance control

某型发动机高压12级转子叶尖间隙控制研究