• Q: Where is the tail rotor?

    :在哪里尾桨

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  • It also featured an enclosed tail rotor.

    同样涵道为特色

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  • It also removes the need for a tail rotor.

    无需尾部旋翼

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  • Rotor blades: All-metal main or tail rotor blades are prohibited.

    转子叶片金属的旋翼旋翼材质,被禁止的。

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

    直升飞机个五旋翼一个四旋翼。

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  • The tail rotor keeps yaw in check while a servo-driven elevator takes care of pitch.

    尾桨保持偏航检查同时伺服驱动电梯照顾间距

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  • Once connected to the main body, the drive shaft components to the tail rotor are next.

    一旦连接到主体传动轴组件尾桨是在明年

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  • Additionally walking into the tail rotor or main rotor is a safety concern for bystanders.

    此外走进尾桨旋翼一个安全关切旁观者

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  • Natural frequency of tail rotor of some kind of helicopter with uncertain composites was studied.

    研究具有不确定复合材料参数直升机尾桨固有频率

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  • This paper presents the tail rotor failure patterns, handle methods and flight test methods of helicopter.

    介绍直升机尾桨故障类型及其处理方法试飞方法。

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  • It is a good practice to check the bolts and nuts on the main rotor head and tail rotor after every flight.

    每次检查旋翼旋翼头螺丝螺母一个很好的习惯

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

    浸料工艺性能差异刚度不足造成产品寿命下降主要原因。

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  • 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特性

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  • 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可以很容易地查阅

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

    剪刀式尾桨气动特性进行了实验分析研究

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  • It investigates influence of the factors such as engine power, airspeed and flight altitude on the tail rotor failure flight test.

    探讨发动机功率空速飞行高度因素尾桨故障试飞影响

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  • 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方法

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  • Number 8. BELL UH-1 IROQUOIS (HUEY) is a military helicopter powered by a single turboshaft engine, with a two-bladed main rotor and tail rotor.

    第八名:贝尔uh - 1IROQUOIS(惠)一种军用直升机搭载涡轮轴发动机具有双桨叶主旋翼和尾桨。

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  • Dave Thomas: A helicopter has four main controls: foot pedals, collective pitch lever , cyclic, and throttle. The foot pedals control the tail rotor.

    戴夫·托马斯直升机四个主要控制器踏板操纵杆周期变距操纵杆以及气门

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  • Helicopters require a tail rotor to counteract the rotor torque; this and the articulated head complicate flying, construction and maintenance enormously.

    需要直升机尾桨抵消转子力矩阐述复杂飞行建造维修极大

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  • A free wake analytical model is then developed for predicting the aerodynamic characteristics of a scissors tail rotor and validated by numerical examples.

    然后建立一个剪刀式尾桨气动特性计算分析模型进行了验证。

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  • The Z-9B variant features a modified 11-blade Fenestron faired-in tail rotor with wider-chord, all-composite blades instead of 13 all-metal blades as in as 365n1.

    Z - 9b型特点一个改进11浆叶涵道尾桨,减阻内置螺旋浆采用宽弦、全-复合浆而不是AS 365n1型中的13片全-金属浆叶。

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  • Chaos characteristics of the aerodynamic noise are discussed and the aeroacoustic noise signals on helicopter scissors tail rotor is analyzed by the chaos theory.

    研究剪刀尾桨气动噪声混沌特性,并应用混沌理论进行直升机尾桨气动噪声信号分析

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  • The motor burns out quickly (or I should say that the plastic component in the motor melts) as the power demand of the tail rotor is much larger than that I expected.

    汽车烧伤很快(或者应该塑胶组件汽车熔体)由于电力需求尾桨要远远大于所料

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  • Like the Z-9B, the Z-9C also features a modified 11-blade Fenestron faired-in tail rotor with wider-chord, all-composite blades instead of 13 all-metal blades as in as 365n1.

    如同Z - 9b, Z - 9c具有的特征一个改进11叶涵道减阻内置螺旋浆,采用宽弦全复合浆而不是AD 365n1型一样13-金属浆叶。

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  • For the current helicopter of single main rotor with tail rotor, the effect of inflow models with different characteristics on helicopter trim and digital simulation was discussed.

    常规旋翼尾桨直升机为对象,讨论均匀与均匀入流模型直升机飞行数值仿真影响

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  • For the current helicopter of single main rotor with tail rotor, the effect of inflow models with different characteristics on helicopter trim and digital simulation was discussed.

    常规旋翼尾桨直升机为对象,讨论均匀与均匀入流模型直升机飞行数值仿真影响

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