熱結構 的英文怎麼說

中文拼音 [rèjiēgòu]
熱結構 英文
thermal structure
  • 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. Professir yuanxian gu visited the graz university of technology, austria and the stuttgart university, germany during 13 - 17 july 2003, and gave a seminar at the department of aerospace engineering of the stuttgart university on the design optimization of thermal structures and heat transfer problems

    顧元憲教授於2003年7月間訪問了奧地利格拉茨技術大學及德國斯圖加特大學，在德國斯圖加特大學航空工程系做了一次關于受熱結構的優化設計及熱傳導問題的學術報告。
  2. The different influences of temperature to two aeroelastic systems are analyzed

    分析了溫度對這兩種熱結構氣動彈性系統的不同影響。
  3. Thermomechanics analyses and optimization for the high power density blanket bfeb

    高功率密度包層的熱結構力學分析與優化
  4. For the sake of realizing compressive ignition of single fueled natural gas and aiming at the characteristics of high spontaneous combustion temperature of natural gas, the separated combustion chamber provided with low heat radiation structure was designed, meanwhile the heating device for the intake pipe air and the ceramic electro - thermal plug heating device inside the separation chamber were set up

    摘要為實現單一燃料天然氣的壓燃著火，針對天然氣自燃溫度高的特點，設計了具有低散熱結構的分隔式燃燒室，同時設置了進氣管空氣加熱裝置和分隔室內陶瓷電熱塞加熱裝置。
  5. With the development of reusable launch vehicles, the thermal protection system has been oriented by the idea of incorporate design which involves thermal protection - structure - thrust system. at the same time, the weight proportion of thermal protection system has been reduced, but the working temperature of thermal protection system has been increased

    隨著可重復使用航天器的發展，熱防護系統在向著防熱-結構-推進系統一體化設計的方向發展，與此同時，整個防熱系統在總起飛重量中所佔的重量比例也在降低，而使用溫度升高，即要求防熱結構日趨先進。
  6. The new method of adiabatic joining between conditioned pipe and pipe - hanging hook

    空調管道與吊架接點絕熱結構的新做法
  7. The results of static firing test shows that the thermal erosion properties, mechanical properties, tand thermal shock resistance of the c / sic composites can meet a demand for thermal - structure application in the area of aerospace such as liquid rocket thruster

    試驗發動機地面熱試車結果表明，該c / sic復合材料的力學性能、燒蝕性能和熱震性能優良，可滿足宇航工程中諸如液體火箭發動機推力室等對熱結構材料的使用性能要求。
  8. Heat structural coupling analysis under mehanical and temperature load is analyzed by using the powerful software ansys

    利用大型通用有限元分析軟體ansys研究了在機械載荷與溫度載荷作用下的熱結構耦合問題。
  9. 3d - c / sic is a new kind of promising thermal - structural material in aviation and aerospace field

    3d - c sic是一種新型的超高溫熱結構材料，在航空航天和高溫熱結構領域具有潛在的應用前景。
  10. It also introduces the principle of sld drive and automatic temperature control and advances the reasonable thermal frame from the angle of thermal science

    介紹了sld光源驅動及自動溫度控制的原理。並從熱學角度提出了光源合理的熱結構。
  11. The requirement of the primary hot structure provides both thermal protection and loading for the future spacevehicle can be achieved by integrated design of thermal protection and load bearing

    防熱?結構一體化設計，要求未來空天飛行器的關鍵熱結構能夠同時滿足防熱和承載的要求。
  12. That attracts much more attentions. three dimensional braided ceramic matrix composites ( cmc ) also have characters such as low density, high temperature resistance and wash out resistance

    三維編織陶瓷基復合材料還具有輕質、耐高溫、抗沖刷性能好的特點，是航天、航空發動機以及航天飛機熱結構用的理想材料。
  13. Three contents, which are the analysis of thermal structures, the analysis and design optimization of heat conduction, the design optimization of thermal structures, are summarized in this section

    接著回顧熱傳導結構耦合系統分析和優化設計的研究工作。分別敘述熱結構分析，熱傳導分析和優化設計及熱結構優化設計三個方面的現狀。
  14. Different zone block in the basin has different construction. cold and heat shells are at intervals. crust behaves as hot, light, flowing and thicker, however, mantle behaves as cold, weight, and harder, multi - phase and deep mantle

    盆地不同區塊熱結構不同，為冷、熱殼相間，地殼表現為熱、輕、軟、流、厚殼，地幔表現為冷、重、硬、多相、深幔的特點。
  15. Several non - linear phenomena are also analyzed. by using uncoupled thermal - structure analyzing method, with the consideration the additional stiffness caused by thermal stress, the finite element model for thermal - vibration analysis is obtained and two typical hypersonic wing structures are computed

    運用非耦合熱-結構分析方法，考慮熱應力引起的附加剛度，得到熱環境下的結構分析的有限元模型，並計算了兩種典型結構的高超音速翼面熱結構。
  16. Adopt double layer heat insulation framework and more reasonable inner circulate hot winds in two directions to ensure insulating heat and reduce the loss the heat, and in favor of the orientation shrink of the products

    採用隔熱效果更為出色的雙隔熱結構及更為合理的雙向循環熱風風道，確保隔熱、減少熱能損耗的同時更利於產品的定向收縮。
  17. Use of self heating and self radiating structure, a change to the conventional water cooling structure, so as to achieve simple structure, small volume, economy of operation cost, outstanding performance and dependable operation

    採用自熱散熱結構，改變了傳統的水冷卻結構，使結構簡單，體積小，節約運行費用，性能好，使用可靠。
  18. The 1w leds is a device that can be reflow soldered for automated production assembly. it features moksan ' s unique electrically neutral thermal path and contains no lead or mercury

    1w的發光二極體能應用於自動化生產中的迴流焊。這是木山公司產品的典型特徵，具有優越的散熱結構，不含鉛和汞。
  19. Based on g - w contact model, two rough surfaces in contact were simplified to a smooth one and a rough one which has regular rectangular asperities, and a three - dimensional transient thermal and stress coupled fem model was established using thermal - structure sequential coupling. the course of the sliding with friction was simulated using the nonlinear multiphysics field fem, meanwhile considering thermal - elastic problems of the two bodies, to calculate and analyze the temperature, contact pressure and stress of the sliding contact surfaces with frictional heating

    基於g - w接觸模型，將兩個粗糙表面簡化為一個有規則排列的長方體微凸體的粗糙表面與一光滑表面，利用熱結構順序耦合建立三維瞬態有限元計算模型，考慮兩個物體摩擦接觸的熱彈性問題，採用非線性有限元多物理場來實現，對粗糙表面接觸模型的瞬時摩擦溫度場、壓力場和應力場進行了計算分析。
  20. Provide a rugged, long - lived, solid - state lighting source for 350 ma lighting applications

    這是木山公司產品的典型特徵，具有優越的散熱結構，不含鉛和汞。
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