旋翼直升机的英文

发音:

"旋翼直升机"怎么读用"旋翼直升机"造句

英文翻译手机版

autogiro
autogyro
helicopter

"旋"英文翻译 whirl
"翼"英文翻译 the wing of a bird
"单旋翼直升机" 英文翻译 : single-rotor helicopter
"双旋翼直升机" 英文翻译 : dual-rotor helicopter; twin-rotor helicopter
"四旋翼直升机" 英文翻译 : four-rotor helicopter
"刚接式旋翼直升机" 英文翻译 : helicopter; rigid-rotor; rigid-rotor helicopter
"喷气旋翼直升机" 英文翻译 : tip-driven helicopter
"四叶旋翼直升机" 英文翻译 : four-blade rotor helicopter
"无关节旋翼直升机" 英文翻译 : helicopter; hingeless rotor; hingeless rotor helicopter
"折叠式旋翼直升机" 英文翻译 : collapsible helicopter
"纵列双旋翼直升机" 英文翻译 : helicopter; tandem-rotor
"交叉式双旋翼直升机" 英文翻译 : helicopter; intermeshing-rotor; intermeshing-rotor helicopter
"同步交叉式双旋翼直升机" 英文翻译 : synchropter
"压缩传动喷气旋翼直升机" 英文翻译 : pressure jet helicopter
"纵列式双旋翼直升机" 英文翻译 : tandem helicopter; tandem rotors helicopter; tandem-rotor machine
"有翼直升机" 英文翻译 : helicopter; winged
"冲压发动机喷气旋翼直升机" 英文翻译 : athodyd helicopter
"火箭发动机喷气旋翼直升机" 英文翻译 : rocket-powered helicopter
"冷压缩传动喷气旋翼直升机" 英文翻译 : cold-jet helicopter
"热压缩传动喷气旋翼直升机" 英文翻译 : hot-cycle helicopter
"带短翼直升机" 英文翻译 : helicopter; stub-wing
"直升机旋翼" 英文翻译 : helicopter rotor
"次临界旋翼（直升机）" 英文翻译 : subcritical rotor
"直升机反扭矩旋翼" 英文翻译 : antitorque rotor
"直升机旋翼挥舞" 英文翻译 : helicopter flapping

例句与用法

In 1945 c . j . ghu turned his attention to rotorcraft and designed a co - axial helicopter , known as the humming bird model a
1945年，朱家仁先生制造了一架共轴双旋翼直升机，即蜂鸟一号。
But the variation of its aerodynamic forces will induce flapping motion and produce the cyclic pitch on the main rotor blades by the bell mixing mechanism . in order to study the effect of bell - hiller stabilizer bar on helicopter stability and control , this paper first analyze the function and the principles , give the flapping equation and a flight dynamic model with bell - hiller stabilizer bar . and then works over the stability and control of uav r - 50 in hover and cruise condition , and analyzed the influence from parameters of the bar to it
为了深入研究希勒伺服旋翼对直升机稳定性和操纵性的影响,本文首先分析了希勒伺服旋翼的功能和工作原理,推导了伺服旋翼的挥舞运动方程,建立了带有希勒伺服旋翼直升机的飞行动力学模型,然后以yamahar - 50无人直升机为例,分析该直升机在悬停和前飞时的平衡、稳定性和操纵性,在此基础上进一步研究希勒伺服旋翼设计参数变化对直升机稳定性和操纵性的影响。