强度与环境
彊度與環境
강도여배경
STRUCTURE & ENVIRONMENT ENGINEERING
2014年
1期
50-56
,共7页
谯盛军%高行山%王富生
譙盛軍%高行山%王富生
초성군%고행산%왕부생
复合材料%刚度%桁条%结构布局和尺寸
複閤材料%剛度%桁條%結構佈跼和呎吋
복합재료%강도%항조%결구포국화척촌
composite%stiffness%stringer%structural layout and dimension
利用薄壁结构力学剖面计算的理论，通过计算获得全复合材料机翼的扭转和弯曲刚度及刚心位置，并进一步研究了桁条的结构布局对机翼整体结构刚度的影响。结果表明：机翼的剖面刚度随桁条的尺寸和分布的变化而改变，桁条最佳间距为130~150mm。该内容的研究为复合材料飞机机翼结构设计和气动弹性分析提供了重要依据。
利用薄壁結構力學剖麵計算的理論，通過計算穫得全複閤材料機翼的扭轉和彎麯剛度及剛心位置，併進一步研究瞭桁條的結構佈跼對機翼整體結構剛度的影響。結果錶明：機翼的剖麵剛度隨桁條的呎吋和分佈的變化而改變，桁條最佳間距為130~150mm。該內容的研究為複閤材料飛機機翼結構設計和氣動彈性分析提供瞭重要依據。
이용박벽결구역학부면계산적이론，통과계산획득전복합재료궤익적뉴전화만곡강도급강심위치，병진일보연구료항조적결구포국대궤익정체결구강도적영향。결과표명：궤익적부면강도수항조적척촌화분포적변화이개변，항조최가간거위130~150mm。해내용적연구위복합재료비궤궤익결구설계화기동탄성분석제공료중요의거。
The present study aimed at obtaining retorting stiffness, bending stiffness and stiffness center position of full composite wing using thin wall structure mechanics theory. The influence of stringer layout on wing integer structure stiffness was furthermore investigated. It is found that wing section stiffness was influenced by stringer layout and dimension. The best spacing of stringer was within the range from 130 to 150 mm. The study of this paper provided important support for structural design and aeroelastic analysis on composite wing.
