蜂窩夾層結構 的英文怎麼說

中文拼音 [fēngwōjiācéngjiēgòu]
蜂窩夾層結構 英文
honeycomb sandwich construcion
  • 蜂 : 名詞1. （昆蟲名） wasp2. （特指蜜蜂） bee Ⅱ副詞（比喻成群地） in swarms
  • 窩 : Ⅰ名詞1 （鳥獸、昆蟲住處） nest 2 （比喻壞人聚居處） den; lair; nest 3 [方言] （比喻人體或物體所佔...
  • 夾 : 夾構詞成分。
  • 層 : i 量詞1 （用於重疊、積累的東西 如樓層、階層、地層） storey; tier; stratum 2 （用於可以分項分步的...
  • 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...
  • 蜂窩 : 1. （蜂巢） honeycomb2. （像蜂巢物） a honeycomb-like thing
  • 結構 : 1 （各組成部分的搭配形式） structure; composition; construction; formation; constitution; fabric;...
  1. Peeling analysis of unperforated honeycomb structure

    無孔蜂窩夾層結構脫粘剝離應力分析
  2. This paper presents the experimental results of typical elements of field works such as reinforced concrete beams, fiber glass reinforced plastic honeycomb sandwich plates, flexible covers ; examines the interrelationship of the loads and deformation under the condition of large deformation ; obtains the laws governing the interaction of the medium and the structure ; solves the design and calculation problems related to shallow buried structures in soil

    本文在對大量試驗資料進行整理和作了大量分析計算的基礎上，選取了野戰工事中有代表性的構件即鋼筋混凝土梁，玻璃鋼蜂窩夾層梁式板和帆布被復作為研究對象進行試驗研究。深刻地考察了大變形條件下荷載和變形之間的內在關系，進而掌握了介質與結構相互作用的規律，較好地解決了土中淺埋結構的設計計算問題。
  3. The purpose of this thesis is to use this powerful method to identify the dynamic characteristic of the honeycomb sandwich structure

    本文的主要目的就是利用dbm方法的強大辨識能力對蜂窩板夾層結構的動力學特性進行辨識。
  4. On the other hand, it seems not quite easy to use the conventional methods to identify the dynamic characteristic of the honeycomb sandwich structure, which is a main structure of the modern satellite, due to its complex construction

    而另一方面，作為構成現代衛星的主要結構之一的蜂窩板夾層結構，由於其復雜的構成方式使得應用傳統的辨識方法難以對其動力學特性給出清楚和完整的描述。
  5. Finally, the improved method is utilized to identify data acquired by vibration test of a honeycomb sandwich structure with different magnitudes, locations or vibration directions, and the identification results are used to analyze the characteristic of the structure in order to guide the further study of satellite structure ’ s design

    最後利用改進后的dbm方法對幾組在不同量級、不同振動方向、不同測點的蜂窩板夾層結構的振動數據進行辨識，並利用辨識的結果對于結構的動力學特性進行分析，從而為實現對衛星結構的設計提供依據。
  6. To identify the dynamic characteristic of honeycomb sandwich structure via method mentioned in this thesis can be valuable in practice for further design,

    利用本文的方法，實現了對鋁蜂窩夾層結構動力學特性的辨識，這對鋁蜂窩夾層結構的設計，實驗和分析具有一定的實用價值。
  7. Finally, the nonlinear identification method to stochastic data in frequency domain is used to analyze and identify the nonlinear characteristic of some multifunctional electrical case with honeycomb sandwich structure

    最後，將隨機數據的頻域非線性分析與辨識方法應用於某鋁蜂窩夾層結構多功能電子機箱的非線性特性研究中。
  8. The paper briefly describes the characteristic and damnification of carbon / epoxy facings - aluminum honeycomb sandwich construction which was used for one satellite that was manufactured by us, and also detailed introduce the repairing technics for damnification

    摘要本文介紹了我單位研製的某型號衛星碳環氧面板鋁蜂窩夾層結構件結構特點及損傷情況，且對損傷修補內容作了較詳細敘述。
  9. The honeycomb sandwich structure has been widely utilized in engineering field nowadays. however, due to the complex construction of this structure, it seems not quite easy to describe its dynamic characteristic clearly and completely via conventional methods. the purpose of this thesis is to analyze and identify the dynamic characteristic of honeycomb sandwich structure based on nonlinear methods to stochastic data in frequency domain

    現今鋁蜂窩夾層結構廣泛應用於工程領域，但由於鋁蜂窩夾層結構復雜，使得應用傳統的辨識方法難以對其動力學特性給出清楚和完整的描述，本文的目的就是應用隨機數據的頻域非線性分析與辨識方法對鋁蜂窩夾層結構的動力學特性進行辨識。
  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. Standard specification for structural film adhesives for honeycomb sandwich panels

    蜂窩夾層板用結構薄膜粘結劑的標準規范
  12. Through the studies of its forming process and performance of nomex sandwich constructions composite, it not only provides the perfotmance data and test basis for the normal usage of sandwich constructions but also provides the experiences that was to be accumulated in aircraft

    總之，通過對nomex蜂窩夾層結構成型工藝及材料性能的研究，為蜂窩夾層結構在航空領域中的正常應用提供了性能數據和實驗依據，同時也為蜂窩夾層結構在飛機上的應用積累了經驗。
  13. Brazed all honeycomb sandwich

    銅焊全金屬蜂窩夾層結構
  14. Application of homogenization fem to the equivalent elastic constants of honeycomb structures

    蜂窩夾層結構等效彈性常數的多步三維均勻化數值計算分析
  15. To use the macro - mechanics theory and the composite - mechanics theory analysed the honeycomb structure, and get the equivalent parameter of the honeycomb structure

    進而從宏觀力學、復合材料力學的角度，對蜂窩夾層結構進行了理論分析，得出了蜂窩結構等效參數的推導方法。
  16. 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。
  17. Chapter 3 introduces the static test of shallow - buried structures with flexible coverings and with fiber glass reinforced plastic honeycomb sandwich plates, presenting in detail the method and process of the test and the data charts obtained from the test

    第三章介紹了淺埋柔性被復結構和玻璃鋼蜂窩夾層板的靜力試驗。詳細給出了試驗方法和試驗過程以及試驗取得的數據圖表。
  18. Thermal conductivity of honeycomb sandwich panels with carbon fibre mesh plates at low temperature

    網狀碳纖維面板蜂窩夾層結構低溫熱導率測試研究
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