| 1. | Simulation of yzl16 landing gear shimmy damper
16操纵减摆器仿真研究 |
| 2. | A damper finite element model is coupled to rotor system equations of motion
推导了常规粘弹减摆器旋翼耦合系统运动方程。 |
| 3. | Failure analysis of broken shaft and its improvement of vibration reducer in a teaching aircraft
某型教练机减摆器断轴失效分析及改进研究 |
| 4. | Analysis of kinematics and parameters for a nonlinear hydraulic damper of helicopter rotor
直升机旋翼非线性液压减摆器几何耦合及参数影响分析 |
| 5. | Model experiment and damping identification for aeroelastic stability of helicopter rotor with elastomeric lag damper
带粘弹减摆器旋翼系统气弹稳定性试验与阻尼识别 |
| 6. | The method of eigenvalue analysis is used to investigate the ground resonance stability of the helicopter rotor / body coupled system with two connections of dampers
采用特征分析法计算了两种减摆器连接形式的直升机地面共振稳定性。 |
| 7. | In order to analyze this model , a modified multi - blade coordinate transformation was proposed . at last , the aeromechanical stability problem was analyzed with the two
最后用上述两种分析方法对带叶间减摆器的旋翼/机体耦合系统的气动机械稳定性问题进行了分析研究。 |
| 8. | Therefore , in this thesis , the magneto - rheological damper ( mrfd ) was studied which is of simple structure , high reliability and self adaption
为此,本文研究了结构简单、可靠性高并具有自适应能力的磁流变减摆器(阻尼器) ,用于控制直升机旋翼/机体耦合动不稳定性运动。 |
| 9. | An analytical model is developed for the dynamic stability analysis of helicopter rotor / fuselage coupled systems with general connections or inter - blade connections for the nonlinear elastomeric lag dampers
摘要建立了粘弹减摆器不同连接形式时的旋翼机体耦合动稳定性分析模型。 |
| 10. | Dipl . ing . eugen vom cleff gmbh offers offers on shaft seals , o rings and hydraulic packings . additionally also on radial shaft sealing rings and shaft seals
该企业为您提供阻尼器、减震器、消声器、减摆器、扭转振动减振器、汽船、调节风门、阻尼装置、密封环和缓冲装置以及棒料密闭和自紧油封的报价。 |
