网络矢量喷管;实时数学模型 网络释义 1. 矢量喷管 thrust calculation_翻译 ... 滑坡推力: landslide thrust矢量喷管:Thrust-vectoring nozzle瞬态推力: instantaneous thrust ... www.lw23.com|基于2个网页 2. 实时数学模型 ... 径推联合轴承: radial-thrust hybrid bearing实时数学模型:Thrust-vectoring nozzle推力...
1)thrust vectoring nozzle矢量喷管 1.Three typical stages,two sway stage and one backhaul stage,were defined according to the kinetic characteristic ofthrust vectoring nozzle.针对矢量喷管机构的运动特点,将其运动过程分为2个摆动阶段和1个定位阶段,应用概率论和随机过程理论建立了对应这3个阶段的运动功能可靠...
Thrust-vectoring nozzle for jet propulsion systemJean G BouillerJacques A J PousRaymond J M Joubert
Independent actuation means are provided to rotate the extension arms and the shells, thereby enabling adjustment of the thrust-vector angle or the exhaust area of the nozzle.doi:US6938408 B2Lair, Jean-pierreUSUS6938408 * Mar 5, 2003 Sep 6, 2005 Propulsion Vectoring, L.P. Thrust vectoring ...
网络矢量喷管 网络释义 1. 矢量喷管 矢量弯管,vector... ... ) buckling vector 弯曲矢量 )vectoring thrust nozzle矢量喷管) thrust vectoring nozzle 矢量喷管 ... www.dictall.com|基于 1 个网页
Thrust vectoring J-10For the first time, a clear photo has been released showing Chengdu's J-10B fighter fitted with a stealthy thrust vectoring nozzle. In late 2017 - briefly, after the first J-20A was flown powered by two indigenous WS-10B Taihang engines fitted with a stealthy nozzle ...
A gimbal joint pivotably couples the nozzle rim to supporting structure. The gimbal joint allows the nozzle rim to be pivoted about a first axis and a second axis, thereby allowing changes to the vector at which the exhaust flow is discharged from the nozzle rim....
The double back-flips and controlled flat spins could be regarded as display gimmicks, but are designed to display the control power provided by the three-dimensional thrust vectoring nozzles on the Russian fighter's twin Klimov RD-33 OVT engines. In combat, that control power would translat...
Thrust-vectoring exhaust nozzle is the key component to realize the deflexion of thrust. 矢量喷管是实现推力矢量的关键部件,对矢量喷管的分类和设计方案进行了初步研究,在某型发动机上加装了轴对称矢量喷管,建立了起飞特性的数学模型,得出在不同状态下飞机起飞滑跑距离与推力矢量偏角之间的关系,对减小飞机起飞滑...
Using CFD and DOE an optimization study for a 2-D dual-throat fluidic thrust-vectoring nozzle is performed. 利用CFD技术并借用DOE技术,对二元双喉道射流推力矢量喷管进行了参数化研究和方案寻优研究,获得了一个性能较优的喷管设计方案。2) fluidic thrust vector 射流推力矢量 1. In the paper,nozzle ba...