期刊文献+

Research of Optical Fiber Coil Winding Model Based on Large-deformation Theory of Elasticity and Its Application 被引量:5

Research of Optical Fiber Coil Winding Model Based on Large-deformation Theory of Elasticity and Its Application
原文传递
导出
摘要 Optical fiber coil winding model is used to guide proper and high precision coil winding for fiber optic gyroscope (FOG) application. Based on the large-deformation theory of elasticity, stress analysis of optical fiber free end has been made and balance equation of infinitesimal fiber is deduced, then deformation equation is derived by substituting terminal conditions. On condition that only axial tensile force exists, approximate curve equation has been built in small angle deformation scope. The comparison of tangent point longitudinal coordinate result between theory and approximation gives constant of integration, and expression with tangent point as origin of coordinate is readjusted. Analyzing the winding parameters of an example, it is clear that the horizontal distance from the highest point of wheel to fiber tangent point has millimeter order of magnitude and significant difference with fiber tension variation, and maintains invariant when wheel radius changes. The height of tension and accurate position of tangent point are defined for proper fiber guide. For application to fiber optic gyroscope, spiral-disc winding method and nonideal deformation of straddle section are analyzed, and then spiral-disc quadrupole pattern winding method has been introduced and realized by winding system. The winding results approve that the winding model is applicable. Optical fiber coil winding model is used to guide proper and high precision coil winding for fiber optic gyroscope (FOG) application. Based on the large-deformation theory of elasticity, stress analysis of optical fiber free end has been made and balance equation of infinitesimal fiber is deduced, then deformation equation is derived by substituting terminal conditions. On condition that only axial tensile force exists, approximate curve equation has been built in small angle deformation scope. The comparison of tangent point longitudinal coordinate result between theory and approximation gives constant of integration, and expression with tangent point as origin of coordinate is readjusted. Analyzing the winding parameters of an example, it is clear that the horizontal distance from the highest point of wheel to fiber tangent point has millimeter order of magnitude and significant difference with fiber tension variation, and maintains invariant when wheel radius changes. The height of tension and accurate position of tangent point are defined for proper fiber guide. For application to fiber optic gyroscope, spiral-disc winding method and nonideal deformation of straddle section are analyzed, and then spiral-disc quadrupole pattern winding method has been introduced and realized by winding system. The winding results approve that the winding model is applicable.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第5期640-647,共8页 中国航空学报(英文版)
基金 Fundamental Research Funds for the Central Universities (YWF-10-01-B30)
关键词 fibers fiber optics LARGE-DEFORMATION fiber optic gyroscope spiral-disc winding quadrupole pattern fibers fiber optics large-deformation fiber optic gyroscope spiral-disc winding quadrupole pattern
  • 相关文献

参考文献2

二级参考文献21

  • 1朱奎宝,张春熹,宋凝芳.光纤陀螺随机漂移模型[J].北京航空航天大学学报,2006,32(11):1354-1357. 被引量:13
  • 2李翠华,王巍,张俊杰.光纤陀螺低温快速启动技术[J].中国惯性技术学报,2007,15(2):237-240. 被引量:8
  • 3Herve C Lefevre. The Fiber-optic gyroscope[M]. Norwood: Artech House, 1993.
  • 4Friebele E Joseph, Askins Charles G. Miller Gary A, et al. Optical fiber sensors for spacecraft: Applications and challenges[C]// Proceedings of SPIE - The International Society for Optical Engineering. Denver, United States, 2004:120-131.
  • 5Ruffin Paul B, Baeder Janet S. Micro-sensor coils for miniature fiber optic gyroscopes[C]//Proceedings of SPIE - The International Society for Optical Engineering. Denver, United States. 2004:219-227.
  • 6Danny Wong. Thermal stability of intrinsic stress birefringence in optical fibers[J]. Journal of Lightwave Technology, 1990, 8(11): 1757-1761.
  • 7Forward R L, Hoyt R P. Application of the terminator tether^TM electrodynamic drag technology to the deorbit of constellation spacecraft[R]. AIAA-98-3491,1998.
  • 8Hoyt R P, Forward R L. The terminator tether^TM: autonomous deorbit of LEO spacecraft for space debris mitigation[R]. AIAA-2000 0329, 2000.
  • 9Izquierdo J G, Rozemeijer H, Muneheberg S. The tether system experiment-preparing for ESA'S first tether mission[J]. ESA Bulletin, 2000, 102: 139-143.
  • 10Blandino J, Gatsonis N, Gappelli M, et al. Overview of electric propulsion reserch in U.S. academia[R]. AIAA-2003-4442,2003.

共引文献12

同被引文献29

引证文献5

二级引证文献4

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