海军航空工程学院学报
海軍航空工程學院學報
해군항공공정학원학보
JOURNAL OF NAVAL AERONAUTICAL ENGINEERING INSTITUTE
2011年
5期
571-575
,共5页
捏合机%桨叶%搅拌
捏閤機%槳葉%攪拌
날합궤%장협%교반
kneading mixer%blade%mixing
通过对在不同转速下的搅拌过程中桨叶所受的扭矩、压力分布、应力和变形规律进行研究,表明在搅拌过程中,转速越高、越靠近捏合机底部,桨叶所受的压力越大,且压力的极值点出现在桨叶尖部;远心桨的扭矩要大于近心桨;所承受应力也较大,捏合状态时近心桨的相对变形量比远心桨大,且变形不对称,向一侧偏转,最大相对变形处在近心桨底部桨翼的捏合处尖端,远心桨的最大相对变形在桨叶底部桨翼的刮壁处尖端。
通過對在不同轉速下的攪拌過程中槳葉所受的扭矩、壓力分佈、應力和變形規律進行研究,錶明在攪拌過程中,轉速越高、越靠近捏閤機底部,槳葉所受的壓力越大,且壓力的極值點齣現在槳葉尖部;遠心槳的扭矩要大于近心槳;所承受應力也較大,捏閤狀態時近心槳的相對變形量比遠心槳大,且變形不對稱,嚮一側偏轉,最大相對變形處在近心槳底部槳翼的捏閤處尖耑,遠心槳的最大相對變形在槳葉底部槳翼的颳壁處尖耑。
통과대재불동전속하적교반과정중장협소수적뉴구、압력분포、응력화변형규률진행연구,표명재교반과정중,전속월고、월고근날합궤저부,장협소수적압력월대,차압력적겁치점출현재장협첨부;원심장적뉴구요대우근심장;소승수응력야교대,날합상태시근심장적상대변형량비원심장대,차변형불대칭,향일측편전,최대상대변형처재근심장저부장익적날합처첨단,원심장적최대상대변형재장협저부장익적괄벽처첨단。
In this paper, the distribution law of torque, pressure, stress and deformation of the blades in the mixing process at different speeds were analyzed. The result indicates that the higher the speed of blade the closer to the bottom of kneading mixer, the greater the pressure on the black. The maximal pressure lay in the spire of the blade. The torque and stress of the far blade was greater than the near blade, and the relative deformation of the near blade was bigger than the far blade when they were in kneading situation. In the kneading process, the relative deformation of the near blade was asymmetry, deflecting to one side. The largest relative deformation was at the tip of kneading zone of the near blade bottom wing.