倾转旋翼机

倾转旋翼机是一种将固定翼飞机和直升机特点融为一体的新型飞行器。

Tiltrotor is a kind of new aerocraft that combines propeller aircrafts and helicopters .

倾转旋翼机过渡飞行阶段控制律设计研究

Design and Research of Control law for TiltRotor in Transition Flight Phase

通过分析模拟平台的运动特点，运用Lagrange动力学方法对倾转旋翼机模拟平台进行建模。

The platform movement characteristics were defined using the Lagrange dynamic 's method .

遥控小型倾转旋翼机飞行控制系统研究

Synthesis of Remote Control System of a Small Tilt Rotor Aircraft

倾转旋翼机模型参考自适应双重控制系统研究

Research of Dual Model Reference Adaptive Control System for Tilt-Rotor Aircraft

小型无人倾转旋翼机全模式飞行操纵控制

Full Envelope Flight Control Method for Small Unmanned Tilt Rotor Aircraft

倾转旋翼机机翼向下载荷的计算方法及参数影响分析

Calculated Method and Parametric Effect Investigation of Wing Download of Tiltrotor Aircraft

倾转旋翼机直升机状态系统稳定性判断的一种方法

A Method of Stability Evaluation of Tiltrotor in Helicopter Mode

悬停和前飞状态倾转旋翼机的旋翼自由尾迹计算方法

The rotor free-wake analytical method for tiltrotor aircraft in hover and forward flight

新型倾转旋翼机气动弹性稳定性分析模型

Mathematical model and formulations of a new tilt-rotor aircraft for aeroelastic stability analysis

倾转旋翼机模拟平台自适应神经网络控制

Adaptive Neural Networks Control for Tilt Rotor Aircraft Platform

前飞状态倾转旋翼机气弹稳定性建模贝尔/波音609民用倾转旋翼飞机&民用飞机的新葩

Bell / Boeing 609 & First Civil Tiltrotor

倾转旋翼机模拟平台建模与仿真

Modeling of a tilt rotor aircraft platform

倾转旋翼机具有优良的垂直/短距起降和高速巡航性能。

Tiltrotor aircraft possess excellent vertical / short takeoff and landing and high speed cruising performances .

飞弹（飞机的导弹）前飞状态倾转旋翼机气弹稳定性建模

Flying bomb ( missiles resembling aircraft ) Modeling study on tilt-rotor 's aeroelastic stability in cruise flight

倾转旋翼机在旋翼倾转过程（过渡飞行）中，旋翼处于复杂的非定常气动环境中。

During the tilting process ( conversion flight ), rotors are in a complex unsteady aerodynamics condition .

建立倾转旋翼机数学模型是设计其合理的飞行控制律的基础。

A complete tilt rotor aircraft flight control model was developed to enable design of tilt rotor aircraft .

本文研究最优化设计技术在直升机和倾转旋翼机设计过程中的应用。

The design of helicopter and advanced high speed tilt-rotor aircraft is addressed using a series of optimization procedures .

O/W型稠油乳状液的静态稳定性评价前飞状态倾转旋翼机气弹稳定性建模

EVALUATION ON STATIC STABILITY OF OIL-IN-WATER VISCOUS CRUDE EMULSION Modeling study on tilt-rotor 's aeroelastic stability in cruise flight

建立了倾转旋翼机的螺旋桨动力学模型，分析研究了倾转旋翼机滚动通道模型。

Established the aerodynamic model of the airscrew , studied the rolling channel control model of the tilt rotor .

倾转旋翼机气动弹性稳定性研究进展滑行艇航向稳定性与旋回性理论分析

Review of Aeroelastic Stability Investigations for Tiltrotor Aircraft The analysis of course stability and the turning quality about the skimming boat

前飞状态倾转旋翼机气弹稳定性建模基于回弹的飞机蒙皮拉形模型面修模技术研究

Modeling study on tilt-rotor 's aeroelastic stability in cruise flight Surface Improvement Based on Springback Compensation for Aircraft Skin Stretching Tool

得出了对倾转旋翼机设计有实际指导意义的结论。

On the basis of above research , some new conclusions are presented which are of practical significance for the tiltrotor design .

倾转旋翼机是一种新型飞行器，它具有可以垂直起飞和降落的特性。而它的巡航性能又与固定翼飞机相同。

Tilt-rotor aircraft is a new kind of flight vehicle which has the characteristics of vertical take-off and land ( VTOL ) .

青岛海湾大桥箱梁整体钢侧模支架体系计算及抗倾覆稳定分析前飞状态倾转旋翼机气弹稳定性建模

Calculation and Stability Analysis on Integral Steel Side Formwork of Continuous Box-Girder in Qingdao Bay-Bridge Modeling study on tilt-rotor 's aeroelastic stability in cruise flight

实验结果表明，模型有效地反映了倾转旋翼机的短舱在倾转过程中，短舱倾转角与飞机姿态之间的动态关系。

Experiment results using a flight control platform show that the model accurately reflects the dynamic relationships between the nacelles tilting angle and the aircraft attitude .

基于上述旋翼自由尾迹方法，在第四章对倾转旋翼机的双旋翼气动干扰特性进行了计算和分析，给出了一些有意义的结果。

In Chapter 4 , the above free-wake method is improved to predict the interactional aerodynamic characteristics of twin tilt-rotors , and some new results are acquired .

倾转旋翼机旋翼/机翼/机身组合流场的模拟是直升机空气动力学领域具有挑战性和重要意义的研究内容。

The simulation on the coupled tilt-rotor / wing / fuselage flowfield of tilt-rotor aircraft is a challenging and important subject in the field of Helicopter Aerodynamics .

另外，该平台是一个高阶非线性系统，在一定程度上像倾转旋翼机，为更进一步研究倾转旋翼机提供了很好的实验平台。

The platform is quite simple , relatively unexpensive , and very safe , so it provides an excellent experimental platform for research on tilt rotor aircraft .

针对新型半铰接式、摆振柔软的倾转旋翼机，建立了旋翼/动力舱/机翼气动弹性稳定性分析模型，并导出了系统的动力学方程。

An analytical model of tilt-rotor / pylon / wing coupled aeroelastic stability is presented and the dynamic equations are derived for a new semi-articulated , soft-inplane tilt-rotor aircraft .