tail rotor

For a conventional helicopter, the tail rotor is one of primary sources for helicopter noise.

尾桨是直升机的主要噪声源, 降低尾桨噪声对控制直升机的噪声水平具有重要意义.

Application of Dynamic Analysis In Helicopter Tail Rotor Failure Analysis

动力学分析在某直升机尾桨故障分析中的应用

CFD Analysis for the Ducted Tail Rotor Based on Momentum-Source Method

基于动量源方法的涵道尾桨CFD分析

The machined self lubricating composite tail rotor gears will stand up to the most aggressive 3D flying.

悬停状态下直升机尾桨/尾梁耦合动力稳定性分析加工自润滑复合材料尾桨齿轮都会挺身而出最具侵略性3D飞行。

These conclusions can be used to estimate the helicopter tail rotor noise and help to guide tail rotor noise reduction design.

这些结论为预估直升机的尾桨噪声和指导降低噪声尾桨设计提供了依据。

Numerical Simulation on Interaction of the Free Wake of Helicopter Main and Tail Rotor

直升机主、尾桨自由尾迹相互干扰的数值模拟

Experiment Research of Bearingless Tail Rotor Configuration Effect on Tail Rotor Performance and Load

无轴承尾桨构型对性能、载荷的影响实验研究

Research on Helicopter Spherical Flexible Tail Rotor Joint Fatigue Test Technology

直升机球柔性尾桨桨毂连接件疲劳试验技术研究

Stainless laminated strips has usually been selected as a load-bearing structure in main rotor hub and tail rotor hub of a helicopter.

拉扭条结构件是直升机主桨毂、尾桨毂通常采用的一种结构承载受力件。

Last, by contrastive analysis between the results of the isolated tail rotor noise and the experiment, the computation model is being proven.

最后将孤立尾桨噪声的计算结果和试验结果进行了对比分析，验证了计算模型。

A Method for Predicting Ducted Tail Rotor Power Required in Hovering Flight

直升机悬停时涵道尾桨的需用功率计算

Difference of prepreg technique and the tail rotor rigidity were the key resulting in product life decline.

预浸料工艺性能的差异及桨叶刚度不足是造成产品寿命下降的主要原因。

The flow field characteristic of a helicopter ducted tail rotor in hovering were analyzed using CFD method in this paper.

本文采用CFD方法分析了悬停状态下涵道尾桨的流场特性。

The durable semi-enclosed tail rotor gearbox protects the tail rotor gears while at the same time allowing easy inspection.

耐用半封闭式尾桨变速箱保护尾桨齿轮同时也可以很容易地查阅。

According to Flight Lieutenant Jim Hobkirk who escorted the royals, Prince George 'was very interested in the tail rotor'.

据皇室陪同人员、空军上尉Jim Hobkirk说，小王子对这个高高的直升机尾旋翼非常感兴趣。

Design Technology for Flexible Component of Bearing-Less Tail Rotor

复合材料无轴承尾桨柔性元件设计计算分析

Last beam rear there are two all-metal tail rotor blades.

尾梁后部有两个桨叶的全金属尾桨.

This article describes dynamic stress measurement of x-type of helicopter tail rotor tunnel test in several principal aspects.

本文介绍x型直升飞机尾桨吹风试验动应力测量工作的几个主要方面。

The Synergy N 9 tail rotor system is ready for hard 3 D.

协同N9号尾桨打制三维准备.

The single rotor helicopter with tail rotortype to become now the most common body-type helicopter.

这种单旋翼带尾桨直升机构型成为现在最常见的直升机构型.

We have a tail rotor de-ice caution light.

我们的机尾结冰警示灯报警。

The design and manufacture of stainless laminated strips of helicopter tail rotor hub

直升机尾桨毂拉扭条的设计与制造

An experimental and analytical investigation on the aerodynamic characteristics of a helicopter scissors tail rotor has been made.

对剪刀式尾桨的气动特性进行了实验和分析研究。

Improvement in fatigue property of helicopter tail rotor

直升机尾桨抗疲劳性能的改进

CFD Analysis for the Ducted Tail Rotor in Forward Flight

前飞状态涵道尾桨气动特性CFD分析

This paper introduces a method of making selection of helicopter tail rotor parameter optimization using computer optimum techniques.

本文介绍采用计算机优化技术进行直升机尾桨参数优化选择的方法。

CFD Simulation and Validation of Ducted Tail Rotor Numerical Simulation and Validation of Wake Field of Submarine with Stern Appendage

涵道尾桨的CFD模拟与验证带附体潜艇尾流场的数值模拟与验证

Calculating Method for Constant Load Noise of Helicopter Tail Rotor

直升机尾桨定常载荷噪声的工程计算方法

In the transmission system of the helicopter, it is very important to transmit power to the tail rotor.

直升机动力传动系统中，尾传动系统是其重要的组成部分。

The helicopter has a five-blade main rotor and a four-blade tail rotor.

直升飞机有一个五浆叶主旋翼和一个四浆叶尾旋翼。