laminate plate 中文意思是什麼

laminate plate 解釋
積層板
  • laminate : vt 1 把(金屬等)輾壓成薄板。2 把…切[分]成薄片。 3 用薄片疊成。4 用薄板覆蓋。5 黏合(薄片)。vi ...
  • plate : n 1 厚金屬板 〈cf sheet〉 板(片);(記有姓名等的金屬)牌子,(尤指醫生的)招牌,藏書牌;【印刷...
  1. Using the complex potential method in the plane theory of elasticity of an anisotropic body, the series solution of finite anisotropic thin plate containing an elliptical inclusion is proposed with the help of faber series. a hybrid element with an elliptical inclusion for anisotropic materials is obtained by using the hybrid variable principle, and the element efficiency is verified by numerical examples. the state of the damage is modeled by an elliptical soft inclusion, and using the point stress criterion based on characteristic curve and yamada - sun etc. criteria, the prediction of the strength of a composite laminate with damage is set up

    首先基於經典層板理論,將復合材料層板的彈性問題化歸為均勻各向異性板來求解;採用各向異性體平面彈性理論中的復勢方法,以faber級數為工具,給出了有限大含橢圓核各向異性板彈性問題的級數解形式;利用雜交變分原理,成功導出含橢圓核各向異性板雜交應力有限元,並用算例驗證了該單元的可行性和有效性;採用含剛度折減橢圓形彈性核的沖擊損傷模型,引入基於特徵曲線和yamada - sun破壞準則的點應力判據,建立了含損傷復合材料層板剩餘強度的分析方法;通過數值計算詳細討論了各種幾何參數對損傷層板應力分佈、剩餘強度的影響,得到了一系列對工程應用具有實用價值的結論。
  2. Damage analysis of aluminum alloy plate and composite laminate

    鋁合金及復合材料板開孔損傷分析
  3. It can measure shell speed and crusting of film laminating by adopting fks - 1 tester of film laminating capacity ; the principle of this instrument is that it makes film laminate on heating plate and turns 90or 180 of heating plate for moving un - shell sand. and then it measures shell thickness and observes cocking condition of surface sand

    採用fks - 1型覆膜砂結殼性能測試儀可以觀測覆膜砂的結殼速度和起皮狀況,其原理是將覆膜砂撒在加熱板上,經過某一時間之後,將加熱板旋轉90或180移去未結殼的鬆散砂,然後測量結殼厚度,並觀察表層砂的翹起情況。
  4. The rigidity and strength performance such as tension bend, torsion of composite laminated plates are calculated by use of classical lamination theory, and then analyses the experiment methods for rigidity and strength of laminate in detail, the comparison of theoretical analysis and experimental result shows good consistent, which indicate that the theoretical analysis and experimental method presented there is applicable for design and manufacture of military medical shelter laminate. in addition, theoretical analysis is taken for heat preservation and insulation performance of the laminate material by use of stable plate heat conduction method

    採用經典迭層理論,計算了軍用醫療方艙復合夾層大板材料的拉伸、彎曲及扭轉等剛強度性能,由此深入研究了夾層大板材料彎曲剛強度性能試驗方法,對理論分析進行了試驗驗證,結果表明該課題提出的理論分析和試驗方法適于軍用醫療方艙鋁塑復合夾層大板力學分析,對軍用醫療方艙鋁-聚氨酯-鋁復合夾層大板的力學結構設計和製造具有重要的應用價值。
  5. And, the coefficient of heat conduction, temperature rise and fall in shelter chamber experiment are made, the result shows the stable plate heat conduction method is applicable, the integration of experience formula for calculation of heat and cool load and experiment analysis is suitable for design and validation of temperature in shelter chamber, the integration can nicely reflect the condition of microclimate temperature in shelter chamber, and have importance reference value for research of microclimate condition in shelter chamber. at last, in article the comparison is made between the felt techniques and foam techniques of the laminate plates, and improved manufacture techniques of composite laminate is brought forward. the experiment indicates the improved techniques can ensure the structure strength and heat preservation and insulation performance

    基於軍用醫療方艙特殊的微環境使用要求,運用穩定平壁傳熱分析方法建立了軍用醫療方艙鋁塑復合夾層大板傳熱系數理論計算模型,對軍用醫療方艙鋁-聚氨酯-鋁復合夾層大板材料隔熱保溫性能進行了理論分析;運用經驗分析方法進行了冷熱負荷計算分析;並對兩計算採用傳熱系數和艙室升溫、降溫試驗進行了對比試驗研究,結果表明穩定平壁傳熱分析方法計算傳熱系數方法可行,為方艙鋁塑夾層大板的隔熱保溫結構和性能設計提供重要依據,並準確表徵艙室內部微環境溫度條件,對軍用醫療方艙艙室微環境設計提供參考。
  6. The selection of material, typical the structural designs, the mechanical property and the forming pressure of unmanned aircraft sandwich composite material have been studied in this paper. it has analysed and discussed the flexural properties of honeycomb sandwich plate delamination under bending loads in detail. and then the mechanical properties of the laminate panel are studied which are compared with honeycomb sandwich panel

    在圍繞某無人機蒙皮選用材料的基礎上,重點對蜂窩夾層結構的結構設計、力學性能、成型壓力對力學性能的影響,以及缺陷對蜂窩夾層結構復合材料的彎曲性能影響進行了較深入的實驗研究和理論分析,同時比較了蜂窩夾層結構中面板與同樣材料鋪層的疊層板力學性能的差異。
  7. After mechanical and process properties testing, the results indicated that : ( 1 ) the film resin can make the properties good in climbing drum peer strength of sandwich constructions composite, the little effects of the film resin on other mechanical properties have been given ; ( 2 ) the sandwich composite has the better mechanical properties at central symmetry layer than asymmetric layer ; ( 3 ) through the study of the different pressure of the sandwich composite, the result is obtained that the edgewise properties increases, the flexural properties decreases with the pressure increase from 0. 2mpa to 0. 5mpa ; ( 4 ) at the sameness extend layer, the mechanical properties of the laminate is bigger than that of the honeycomb sandwich panel ; ( 5 ) through the studies on honeycomb sandwich plate delamination under three - point bending tests. it is found that the flexural strength decreases with the area of delamination increases

    研究表明: ( 1 )膠膜能明顯的提高蜂窩夾層結構的剝離性能,對其它性能的影響不大; ( 2 )對稱鋪層較非對稱鋪層的力學性能高; ( 3 )固化壓力由0 . 3mpa提高至0 . 5mpa時,蜂窩夾層結構的側壓強度提高,而彎曲強度和剪切剛度分別降低; ( 4 )蜂窩夾層結構中的面板較同樣材料鋪層的復合材料疊層板的力學性能低; ( 5 )蜂窩夾層結構的界面上有缺陷時,彎曲強度下降,且隨著缺陷面積增大,彎曲強度下降幅度增大。
  8. A new higher - order shear deformation theory based on global - local superposition and refined triangular plate element of composite laminate

    局部高階剪切變形理論及層合板精化三角形單元
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