蒙皮結構 的英文怎麼說

中文拼音 [mēngpíjiēgòu]
蒙皮結構 英文
stressed-skin construction
  • 蒙 : 蒙名詞（蒙古族） the mongol nationality
  • 皮 : Ⅰ名詞1 （人或物體表面的一層組織） skin 2 （皮革） leather; hide 3 （毛皮） fur 4 （包在外面的一層...
  • 結 : 結動詞（長出果實或種子） bear （fruit）; form （seed）
  • 構 : Ⅰ動詞1 （構造; 組合） construct; form; compose 2 （結成） fabricate; make up 3 （建造; 架屋） bui...
  • 結構 : 1 （各組成部分的搭配形式） structure; composition; construction; formation; constitution; fabric;...
  1. Based on the former overseas and domestic study on the sheeting diaphragms effect of fender structure, the " rib - diaphragm " shear model is applied to multi - story steel structure according to its character in this paper, and the result is satisfactory

    本文結合國內外對鋼結構圍護結構蒙皮效應的研究，針對多層鋼結構側移的特點，將「肋-板」結構的抗剪單元應用在多層鋼結構的框架當中，取得了很好的效果。
  2. These advantage make it excellent materials for control surface, wing and skin of airplane

    是飛機結構中對剛度要求較高的操縱面、機翼和機身蒙皮結構用較理想的材料。
  3. According to the special shape and operate requirements of the torpedo, the structure and moulding process of the torpedo shell are established, in which the body and overlay block with grooves are moulded by fiber winding, and close moulding respectively with the adhesive by limited stop compression. in the light of the selection of raw material system, composite system with outstanding performance are defined, based on which the mechanical properties are tested., with the overall consideration of structural characters and design demands, the main factors which may have effects on the strength and stability ( including stiffness section dimension, stiffeners space, skin thickness and skin lay angle ) is optimized one by one for the structure design parameters on the base of the fem model of skin, stiffness and layover block by fem. as a result, the prototype with 1 : 1 proportion and its structure and lay optimization design are completed. the moulding technology for polyurethane foam moulding the stiffened shell is obtai ned in terms of the design, manufacture moulding, experimental mould and tooling

    依據在研產品特殊的外型結構和使用要求，確定了該型號水雷復合材料殼體的具體結構形式和復合成型工藝路線，即由纖維纏繞工藝成型主體異形件，閉模成型帶通槽外貼塊，用限位加壓工裝實現粘接的工藝路線；通過對原材料體系的篩選，確定了綜合性能較好的復合材料體系，以此為基礎進行了力學性能測試；運用有限元方法，建立了蒙皮、筋條和外貼塊的分析模型，綜合考慮結構特點和設計要求，對影響結構強度與穩定性的主要因素（包括筋截面尺寸、筋間距、蒙皮厚度、蒙皮鋪層角度）分別進行了結構設計參數的優選，最終完成了復合材料異形耐外壓殼體1 : 1樣件和縮比實驗件結構及鋪層優化設計；完成了聚氨酯泡沫胎成型內置加筋殼體的成型工藝技術研究；對縮比件進行外壓性能測試，並給出了應力、應變測試結果。
  4. Integral panel is a flat part integrated with framework elements, connection elements and skin in traditional aircraft structure, it is the main supporting structure in aircraft, having the advantages of high - intensity, low - weight, and so on

    整體壁板是將傳統飛機結構中的骨架元素、連接元素和蒙皮製成一體的板類零件，是飛機的主要受力結構件，具有強度高、重量輕、氣密性好等優點。
  5. In the formula, our experience in structural strength design and the experimental results are considered. and such factors are also considered as differences in materials of the skin and the reinforcer, effects of bending, torsion, stretching and offcenter of the reinforcer. furthermore, through post - buckling stress analysis of the skin, it is shown that even low stress level will result in buckling of the skin, but the skin still has loading capacity

    在總結過去結構強度設計和試驗分析的基礎上，應用扁殼理論，在廣義力與廣義應變關系中考慮了蒙皮與加筋不同材料以及加筋的彎曲、扭轉、伸縮和偏心等的影響，推導出適合於工程應用的加筋殼結構軸壓屈曲臨界載荷的計算方法;並通過對薄壁結構蒙皮后屈曲應力分析，說明蒙皮在很低的應力水平時就出現失穩現象，但失穩后的蒙皮仍具有一定的承載能力。
  6. Concerning the tests, analyses, design and calculation of performances for light gauge steel framing, this paper focuses on following items : ( 1 ) the calculation of light gauge steel framed compound bearing walls ( lgsfcbw ) in compression and bending. based on north american specification and commentary for the design of cold - formed steel structural members, which was published by the american iron and steel institute, the detailed design requirements of wall stud assemblies are given considering the structural contribution of the attached sheathings and shear diaphragm is discussed briefly. then the calculational theoretic and method for sheathing braced wall stud assemblies complying with national code is brought up in compression and bending

    本文圍繞輕鋼龍骨體系結構性能的試驗、分析、設計和計算，主要進行了以下四方面的研究工作： （ 1 ）輕鋼龍骨復合承載墻體的受壓、受彎計算：以美國鋼鐵協會發行的北美冷成型鋼構件設計規范及其規范說明為依據，重點考慮罩面材料對墻龍骨設計的影響，給出了目前對承重墻龍骨設計的具體要求，並對剪力蒙皮進行了簡要討論；然後提出了符合我國規范術語的剪力蒙皮作用的輕鋼龍骨復合承載墻體（即罩面支撐墻龍骨）受壓、受彎的計算理論和方法；最後對提出的計算進行簡化，使之完全與我國規范相符。
  7. Opposite to the traditional construction, the stressed skin diaphragm system is an efficacious structure system

    相對于傳統結構而言，受力蒙皮結構是一種高效的結構體系。
  8. Firstly, itis explained that the application research of smart layer. to laod detecting and simulative damage for the model of wing - box, fbg fiber smart layer and pzt smart layer are designed, and manufactured. so, those are surface - mounted respectively on the stiffened skin of aluminum alloy and carbon fiber reinforced. data acquisition system based on different signal processing technique are designed

    針對機翼盒段試件結構載荷識別和模擬損傷監測的功能要求，結合智能夾層的設計製作工藝，設計製作了基於fbg傳感器的光纖和壓電兩種智能夾層，並分別安裝在機翼盒段試件上的鋁合金和碳纖維制蒙皮上。
  9. It is mainly made up of lognitudinal framework, latitudinal framework, airfoil shell, tie - in etc. for the frp airfoil shell, we generally use moulding method of handcraft laying

    飛機機翼曲面是一個結構復雜的非回轉曲面，其整體結構主要由縱向骨架、橫向骨架、蒙皮和接頭等構件組成。
  10. 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。
  11. The finite element method ( fem ) is also employed in stability analysis of reinforced shells. in the fem model the principle of equivalent width is employed to simplify calculation of the modulus of the skin and the loading capacity of the post - buckling skin is also considered

    在運用有限元法對加筋殼穩定性進行分析時，對薄壁加筋殼結構按等效寬度原理，並考慮蒙皮屈曲后的承載能力，對蒙皮的彈性模量進行簡化處理。
  12. The rayleigh - ritz method is used to lead to analytical expressions for the stiffness and mass matrices and load vector as well as their sensitivities, which uses the simple polynomials to define assumed displacement functions, geometry and construction of wing structures. excluding some selected terms from the displacement functions or using stiff springs at the specified locations imposes boundary conditions. the accuracy of calculated results is improved by including transverse shear effects and using multiple sets of ritz functions in the analysis

    它使用簡單多項式作為ritz基函數、定義翼面的幾何和結構參數，利用rayleigh - ritz方法導出翼面結構的剛度矩陣、質量矩陣和載荷向量及其靈敏度的解析表達式，通過排除位移函數中某些選定的項或在指定點使用約束彈簧施加各種邊界條件，考慮橫向剪切變形和使用多組ritz基函數改進分析的質量，使用等效蒙皮和等效夾芯技術提高計算效率。
  13. Stressed skin construction

    蒙皮受力式結構
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