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1)  Coalescence and interference
合体与干涉
2)  RNA interference vector
干涉载体
3)  interfering body
干涉体
1.
The use of AutoCAD drawing software for triple eccentricity metal hard sealing butterfly valve seal extrusion was made to create interfering body,and its qualitative analysis and quantitative analysis were also made to provide basic design parameters for the amendment,verification and identification of triple eccentric butterfly valve.
运用AutoCAD绘图软件对三偏心金属硬密封蝶阀密封挤压带创建干涉体,并对其进行定性分析和定量分析,为修正、验证和确定蝶阀的三偏心参数提供设计依据。
4)  interference-fit
干涉配合
1.
Interference-fit Riveting of Composite Structures;
复合材料结构的干涉配合铆接
2.
Making use of Finite Element Method, experiment and academic analysis, the influence of stress concentration, residual stress and preload on fatigue life of interference-fit composite joint were studied.
通过有限元分析与理论推导,系统研究了应力集中、残余应力、预紧力对复合材料干涉配合接头疲劳寿命的影响。
3.
Researches on interference-fit riveting,riveting of composites structure and driving interference-fit fastener have been done according to the technological needs of large aircraft manufacturing.
针对大飞机制造的技术需求,分析了电磁铆接技术在大飞机研制中的作用,重点介绍了电磁铆接技术在干涉配合铆接、复合材料结构铆接、干涉配合紧固件安装等方面的应用。
5)  interference fit
干涉配合
1.
Some of the specimens were interference fit tapered shank bolt connections(IFBC), and the others were ordinary cylindrical shank bolt connections(OBC).
介绍了以7475 T761铝合金为基材的锥形螺栓干涉配合和普通螺栓非干涉配合连接的犬骨形试件,在随机疲劳载荷谱作用下的疲劳试验。
6)  Force-fit
干涉配合
1.
The experiment on force-fit hard-aluminum alloy LY12CZ sheet under the 6 mmthickness with 3.
1%情况下的航空用硬铝合金LY12CZ板销钉干涉配合预应力及其在35%σ0。
2.
Prestressing of Force-fit and its Characters of Tensile and Compression Load;
1%情况下的硬铝合金LY12CZ板销钉干涉配合预应力及其在 35 %σ0 。
补充资料:纯合体
由两个相同的显性基因或隐性基因的配子结合成的合子发育而成的个体。基因型能稳定地遗传,自交的后代基因型也是纯合体,不会出现性状分离。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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