1) stall wind turbine unit
主动失速型机组
2) active stall wind turbine
主动失速型风力机
3) stall-controlled wind turbines
失速型风电机组
1.
Soft cut-in control algorithm of stall-controlled wind turbines;
失速型风电机组软并网控制新算法
4) active stall
主动失速
1.
The dynamic characteristics of the active stall wind turbine system was presented in this paper.
通过分析主动失速型机组的来流风速、气动、机械传动与发电机等部件的机理,建立了机组各主要部件的子系统模型(如气动模型、传动模型、发电机暂态模型、补偿电容模型、电网模型和控制系统模型等),近而得到了全系统的动态非线性模型。
2.
Pitch control includes passive stall and active stall .
功率的控制可用桨距调节来实现，桨距调节又有被动失速与主动失速之分。
5) post-stall maneuver
过失速机动
1.
Quantitative evaluation on characteristic index of post-stall maneuvers fighter;
战斗机过失速机动特征指标的量化评估
2.
This paper analyzed the characteristic of two typical methods of combination of control surfaces,the least energy control combination method and the chain combination method,according to the harmonization problem of aero/thrust vector control surfaces in post-stall maneuver.
针对在过失速机动中气动/推力矢量控制面协调问题,分析了最小控制能量和链式递增两种典型控制面融合方式的特点。
3.
Tactical advantages can be gained by use of post-stall maneuvering or super maneuvering in air-to-air combat situation.
在空中格斗中，使用过失速机动可获得显著的战术优势，而飞机在大迎角和高角速率的情况下，其动力学具有强耦合性和非线性，本文讨论了应用非线性动态道进行超机动飞机飞行控制系统的设计。
6) post stall maneuver
过失速机动
1.
The effects of unsteady free stream on the post stall maneuvering aircraft;
非定常自由来流对飞机过失速机动特性的影响研究
2.
For researching the flight test techniques of thrust vector controlled aircraft,dynamic models of thrust vector controlled aircraft were established,four post stall maneuver control laws were designed with the dynamic inverse method,tested and investigated according to a standard evaluation maneuver set(STEMS).
为研究推力矢量飞机的试飞技术,建立了推力矢量飞机的动力学模型,用动态逆方法设计了4种过失速机动控制律,并在地面飞行模拟器上参考标准评估机动动作集(STEMS)进行了飞行模拟试验研究。
3.
To improve the post stall maneuverability of aircraft, by reference to the flight control system design philosophy of X 31A, compensating the non linear factors such as aerodynamics, motional coupling and inertial coupling, a controller was constructed by the implicit model following technique for satisfactory flying qualities.
为提高飞机的过失速机动能力 ,参考 X-3 1 A飞机的飞行控制系统模型 ,对非线性因素如气动力、陀螺惯性耦合以及重力影响进行补偿后 ,按飞行品质要求采用隐模型跟踪法设计了某机的反馈控制器。
补充资料：20B、30B、40B型吸尘粉碎机组
 主要用途 本机适用于制药、化工、食品等行业、是粉碎与吸尘为一体的新一代粉碎设备。 工作原理 本机组利用活动齿盘和固定齿盘间的相对运动，使物料经齿冲击、摩擦及物料彼此间冲击而获得粉碎。粉碎好的物料经旋转离心力的作用，自动进入捕集袋，粉尘由吸尘箱经布袋过滤而回收。该机按“GMP”标准设计，全部用不锈钢材料制造，生产过程中无粉尘飞扬。目前已达国际先进水平。 技术参数：
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说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条