期刊文献+

直升机旋翼试验塔振动模态和响应计算

Frequency Mode and Response Calculation of Helicopter Rotor Whirl Tower
下载PDF
导出
摘要 以中国第一座直升机旋翼试验塔为研究对象,建立了塔体的动力学有限元模型,对塔体的模态频率和振型进行了计算,并对塔体在旋翼动载荷作用下的响应进行了计算,最后探讨了旋翼塔对旋翼试验可能造成的影响。 This paper researches the first helicopter rotor whirl tower in china. Dynamic finite element model is built, and the model vibration and frequency of the tower shell is calculated. The response of the tower shell under the action of the rotor dynamie load is calculated. The influence of rotor whirl tower on rotor test is discussed.
出处 《机械工程师》 2017年第3期18-19,共2页 Mechanical Engineer
关键词 旋翼试验塔 模态 响应 有限元 rotor whirl tower vibration model response finite element
  • 相关文献

参考文献2

二级参考文献12

  • 1李开成,尹春望,等.一种旋翼提前操纵角试验测量方法[C].第26届全国直升机年会,2010.
  • 2尹春望,等.直升机动部件综合系统动力特性试验关键技术[C].第21届全国直升机年会,2005.
  • 3Felker F F, Betzina M D, Signor D B. Performance and loads data from a hover test of a full-scale XV 15 rotor[R].NASA TM-86833,1985.
  • 4Van Aken J M. Analysis of calibration data for the multi-component rotor balance installed in the NFAC large rotor test apparatus[C]. AIAA 2007-146, 2007.
  • 5Kitapiloglu C. Analysis of small- scale rotor hover performance data[R].NASA TM- 102271,1990.
  • 6Carpenter P J. Effect of wind velocity on performance of helicopter rotors as investigated with the langley helicopter apparatus[R]. NACA TN No. 1699, 1948.
  • 7Shinoda P M. Wayne Johnson, Performance results from a test of S-76 rotor in the NASA ames 80-by120- foot wind tunnel [C]. AIAA 93 3414 CP, 1993.
  • 8Shivers J P, Carpenter P J Effects of compressibility on rotor hovering performance and synthesized blade-section characteristic derived from measured rotor performance of blades having NACA 0015 airfoil tip sections[R]. NACA TN 4356, 1958.
  • 9Tasker F A, Chopra I. Nonlinear damping estimation from rotor stability data using time and frequency domain techniques[C]. AIAA 89 -1243 CP, 1989.
  • 10Smith C B, Wereley N M. Linear and nonlinear damping identification i systems[C]. AIAA n helicopter rotor 98-2003,1998.

共引文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部