Title :
Solid Rocket Grain Configuration Variational Design Method Based on Geometric Constraint Sketch
Author :
Cai, Qiang ; Bao, Futing ; Liu, Yang ; Hu, Haifeng ; Wei, Han
Author_Institution :
Sch. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
Abstract :
In order to design solid rocket grain configuration intuitively and accurately, this paper introduces a 3D feature design method based on the variational design technology which is popular in the field of Mechanical Product Computer Aided Design. First of all, with the help of geometry constraint solver, the fuzzy concept of grain configurations can be converted to a geometric constraint sketch. Then, through the definition of grain feature entities and design rules, as well as the identification algorithm of Color-Marked Burning Surface in the process of Boolean Operation, designers can implement the grain feature definition, detailed design, calculation of grain mass property and burn back simulation all in one sketch. Finally, a grain configuration design package is developed and a finocyl grain sample is presented to show the effectiveness of this grain design method.
Keywords :
CAD; aerospace engineering; computational geometry; design engineering; mechanical engineering computing; mechanical products; propellants; rockets; solid modelling; variational techniques; 3D feature design method; color marked burning surface; computer aided design; finocyl grain sample; geometric constraint sketch; mechanical product; solid rocket grain configuration; variational design; Algorithm design and analysis; Design automation; Rockets; Solid modeling; Solids; Surface treatment; Three dimensional displays; Geometric Constraint; Grain Configuration; Solid Rocket Motor; Variational Desig;
Conference_Titel :
Software Engineering (WCSE), 2010 Second World Congress on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-9287-9
DOI :
10.1109/WCSE.2010.26