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变量化约束草图驱动的药柱三维特征设计研究 被引量:4

Research on feature design of SRM grains driven by variational constraint sketch
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摘要 为了直观而准确地支持固体火箭发动机药柱设计,提出了一种约束草图驱动的药柱三维特征造型方法。该设计方法首先通过变量化约束求解引擎对设计人员模糊的设计概念进行精确的几何坐标定位,形成一幅设计变量驱动的约束草图。然后,经过药柱特征定义,在设计规则和基于设计历史的燃面追溯统计算法的支持下,设计人员能够在约束草图上进行任意形式复杂药柱的特征定义、造型设计、燃面推移仿真与燃面统计。最后,开发了相应的药柱设计系统,并以一个管槽形药柱的设计过程,验证了本设计方法的计算效率、直观性、准确性和有效性。 In order to make solid rocket motor grain design more intuitive and accurate, a kind of 3D feature design method of SRM grains driven by the variational constraint sketch was put forward. In the method, the variational constraint solver is used first to interpret the grain designers'ambignous design concept into a kind of constraint sketch driven by design variables. Then, with the help of the specified grain feature definition, design rules and burning surface trace statistics algorithm based on design history, de- signers can freely finish feature definition, shape modeling, burning-surface regression simulation and statistics of complicated grain on the sketch. Finally, a grain design software platform was developed, and a slotted-tube grain design example was used to verify the efficiency, intuitive, accuracy and effectiveness of this grain design method.
出处 《固体火箭技术》 EI CAS CSCD 北大核心 2010年第1期13-16,33,共5页 Journal of Solid Rocket Technology
关键词 药柱设计 变量化约束草图 特征造型 grain design variational constraint sketch feature modeling
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  • 1鲍福廷,李逢春,徐东来.固体发动机装药CAD[J].固体火箭技术,1994,17(3):1-7. 被引量:8
  • 2方蜀州,胡克娴.三维燃面计算方法的比较与实体造型方法的特点[J].推进技术,1994,15(1):32-38. 被引量:5
  • 3Osher S, Sethian J. Fronts Propagating with Curvature Dependent Speed: Algorithms Based on Hamilton-Jacobi Form-ulation. J Comp Phys, 1988, 79:12~49.
  • 4Sethian J. Theory Algorithms, and Applications of Level Set Methods for Propagating Interfaces. Technical Report, Center for Pure and Applied Mathematics (PAM-651), University of California, Berkeley, 1995.
  • 5Hegab A, Jackson T L, Buckmaster J, Stewart D S. Nonsteady Burning of Periodic Sandwich Propellants with Compl-ete Coupling between the Solid and Gas Phases. Combustion and Flame, 2001, 125: 1055~1070.
  • 6Peng D, Merriman B, Osher S, Zhao H, Kang M. A PDE-Based Fast Local Level Set Method. J Comput Phys, 1999, 155: 410~438.
  • 7Jiang G S, Peng D. WENO Schemes for Hamilton-Jacobi Equations. UCLA CAM Report, 1997, 97~29.
  • 8Shu C W. Total-Variation-Diminishing Time Discretization. SIAM J Sci Stat Comput, 1988, 9:1073.
  • 9董新刚,陈林泉,侯晓.基于PRO/E平台下的固发装药CAD软件[C]//2002年中国宇航学会固体推进专业委员会年会论文集(上)、昆明:[出版者不详],2002,109-114.
  • 10王信,杨久林.三维装药通用计算方法——体积元素法[J]推进技术,1988(04).

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  • 1周华盛.药柱通用坐标计算法计算结果跳动的原因分析及解决途径[J].固体火箭技术,1994,17(3):8-16. 被引量:10
  • 2秦飞,何国强,刘佩进,李江.基于等值面(Level Set)函数方法的复杂装药燃面算法研究[J].西北工业大学学报,2005,23(4):456-460. 被引量:6
  • 3李晓斌,王中伟,张为华.推进剂稳态燃速最优化辨识[J].固体火箭技术,2006,29(1):28-30. 被引量:6
  • 4Ravi Kumar G V V, Shastry K G, Prakash B G. Computing constant offsets of a NURBS B-Rep [ J ]. Computer-Aided Design, 2003,35 ( 10) :935-944.
  • 5Willcox M A, Brewster M Q,Tang K C, et al. Solid propellant grain design and burnback simulation using a minimum distance function [ C]//AIAA 20054350,41st AIAA/ASME/ SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona,2005.
  • 6Blandford D K, Blelloch G E, Kadow C. Engineering a compact parallel delaunay algorithm in 3D[ C]// Proceedings of the 22nd ACM, Sedona, Arizona,2006.
  • 7董新刚,陈林泉,侯晓.基于Pm/E平台下的固发装药CAD软件[C]//昆明:2002年中国宇航学会固体推进专业委员会年会论文集(上),2002:109-114.
  • 8LEDAS Ltd. LEDAS geometric solver 2D overview[ R]. ht- tp ://ledas. com/products/lgs2d.
  • 9P0skolco G, Ulas A. 3-D grain bumback analysis of solid propellant rocket motors: Part 2--modeling and simulations [J]. Aerospace Science and Technology, 2008( 12): 585- 591.
  • 10Lilley J S. Burning rate characterization from one motor firing: an an- alytical approach. AIAA/SAE/ASME 19th Joint Propulsion Confer- ence, Seattle, Washington, 1983.

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