航天制造技术
航天製造技術
항천제조기술
Aerospace Manufacturing Technology
2015年
5期
1-6
,共6页
钟世宏%孙巍%张崇耿%乔园园%赵亮%许强
鐘世宏%孫巍%張崇耿%喬園園%趙亮%許彊
종세굉%손외%장숭경%교완완%조량%허강
可折叠弹翼%机构优化%动力特性
可摺疊彈翼%機構優化%動力特性
가절첩탄익%궤구우화%동력특성
folding bomb wing%device optimization%dynamical characteristic
根据巡航导弹可折叠弹翼支架部件的工作特点和性能要求,提出弹翼转轴、展开机构、导向机构及燃气作动筒等部件的设计要点,对燃气作动筒安装型式和展开机构提出了新的设计思路,并对弹翼支架各主要构件的动力特性作了理论分析,给出支架部件全新的优化设计方案.
根據巡航導彈可摺疊彈翼支架部件的工作特點和性能要求,提齣彈翼轉軸、展開機構、導嚮機構及燃氣作動筒等部件的設計要點,對燃氣作動筒安裝型式和展開機構提齣瞭新的設計思路,併對彈翼支架各主要構件的動力特性作瞭理論分析,給齣支架部件全新的優化設計方案.
근거순항도탄가절첩탄익지가부건적공작특점화성능요구,제출탄익전축、전개궤구、도향궤구급연기작동통등부건적설계요점,대연기작동통안장형식화전개궤구제출료신적설계사로,병대탄익지가각주요구건적동력특성작료이론분석,급출지가부건전신적우화설계방안.
According to the work condition and structure characteristic demand for the folding bomb wing bracket of cruise missle, design gists are presented, including the bomb wing rotation axis, expandedness device, guide device and gas-drive tube. New design idea is proposed for the setting type of gas-drive tube and its expandedness framework, and the dynamical characteristics of the main components of wing bracket are analyzed theoretically, which provide a new optimization design scheme.
