損傷容限 的英文怎麼說

中文拼音 [sǔnshāngróngxiàn]
損傷容限 英文
damage tolerance
  • 損 : Ⅰ動詞1 （減少） decrease; lose 2 （損害） harm; damage 3 [方言] （用尖刻的話挖苦人） speak sarcas...
  • 傷 : Ⅰ名詞1 （人體或其他物體受到的損害） wound ; injury 2 （姓氏） a surname Ⅱ動詞1 （傷害） injure; h...
  • 限 : Ⅰ名詞（指定的范圍; 限度） limit; bounds Ⅱ動詞（指定范圍, 不許超過） set a limit; limit; restrict
  • 損傷 : 1. （傷害） harm; damage; injure; lesion; scuff; hurt; damnify; impair 2. （損失） loss; cause loss to
  1. Hoop - stove chimney in the bao - steel incorporated company steel pipe factory regarded as the specifiable object the paper makes systemic studies including investigation and inspection of the reinforced concrete chimney and reliable assess method. some studies performed and results achieved mainly include : synthetical investigation method of the reinforced concrete chimney usage condition is put forward and real usage condition of the hoop - stove chimney in the bao - steel incorporated company steel pipe factory is handled by means of entirely investigation and inspection ; the mostly reason for impairment and defect of chimney locating in steel pipe factory hoop stove is revealed through result analysis of investigation and inspection ; to meet practical requirements that corporations manage industrial building all alone the paper presents condition appraisal method on reliability of the reinforced concrete chimney and assesses the reliability of hoop - stove chimney in the bao - steel incorporated company steel pipe factory

    論文以寶山鋼鐵股份有限公司鋼管廠環形爐煙囪為具體對象，對鋼筋混凝土煙囪的調查檢測和可靠性評定方法進行了系統研究，主要研究內容和成果包括：提出鋼筋混凝土煙囪使用狀況的綜合調查方法，並對鋼管廠環形爐煙囪進行了全面調查和檢測，掌握了煙囪實際的使用狀況；通過對調查檢測結果的分析，揭示了鋼管廠環形爐煙囪損傷和缺陷的主要原因；針對我國企業內部對工業建築管理的實際需要，提出鋼筋混凝土煙囪結構可靠性的狀態評估方法，並鋼管廠環形爐煙囪的可靠性進行了評定。
  2. The new engineering concept known as damage tolerance has been developed to provide quantitative guidance for this purpose.

    一個新的工程概念即損傷容限正發展起來，為這個目的提供了定量的指導。
  3. Further more, the tic pinned at the tips of the crack and impeded the crack propagation

    此外，還有tic雜質顆粒對于裂紋的釘扎。材料具有一定的損傷容限。
  4. And the effect of integrity parameter correlative is analyzed. by studying the damage tolerance and durability of aeroplane wings and strengthened planes, the quantitative result of correlative analysis is given

    同時也分析了完全性參數相關的影響，並通過對飛機機翼加勁板的損傷容限和耐久性的研究，給出相關分析的定量計算結果。
  5. Then an integrated application program including some functional modules such as residual strength analysis, crack growth analysis, principle structure elements database management, material properties database management etc, with friendly interfaces and favorable windows styles, is developed by using these classes. finally all of the typical structures described in the " damage tolerance design handbook " have been analyzed

    在此基礎上研製了具有友好界面和良好windows風格的損傷容限分析與評定應用程序，並完成了《設計手冊》中給定的全部典型開裂結構的實例化，實現了對這些結構的裂紋擴展分析和剩餘強度分析。
  6. The work of this thesis has shown that the object - oriented damage tolerance program does require much less time and is indeed more suitable than procedure - oriented programming in damage tolerance analysis of engineering structures. furthermore, the damage tolerance analysis classes have excellent ability in hierarchy and extension, so they are great valuable in engineering and will be used more widely in the future

    本文工作表明，採用面向對象技術所建立的損傷容限分析類庫具有良好的繼承性和可擴充性，不僅可以使軟體性能和適用性得到顯著提高，而且還可以大大縮短軟體開發周期，在工程上具有良好的應用價值和應用前景。
  7. As it is difficult to obtain the accurate analytical solutions for the stress constraints of general 3d cracks, we have conducted systemically detailed researches on the out - of - plane stress constraint by finite elements ( fe ) and proposed a two - parameter description of non - through thickness 3d crack fields. several problems in damage tolerant design were also investigated based on continuum mechanics and probability theory

    三維應力約束對精確預測結構破壞不可缺少，因此，本文採用三維有限元等方法基於連續介質力學、概率論等理論，對典型三維裂紋尤其是非穿透裂紋系統深入地開展了三維應力約束理論計算、三維裂紋端部應力場描述以及結構三維損傷容限設計的研究。
  8. Considering the influence of material original flaw, the thesis gave the 4 # 125t crane of no. 3 steel - making plant of maansan steel co. for example to analyze the designing and remaining life of the crane ' s girder by using damnification limits design method. the method was based on the theory of rupture dynamics and the principle of disrepair - security

    本文以馬鋼第三煉鋼廠4 # 125t鑄造起重機主梁下蓋板大面積可見裂紋情況為例，考慮材料初始裂紋的影響，在斷裂力學理論和破損?安全設計原則的基礎上，採用損傷容限設計法來重新計算鑄造起重機的設計壽命；並對正在服役的鑄造起重機計算其剩餘壽命，為鑄造起重機的安全運行提供了較可靠的理論依據。
  9. Three dimensional braided composite is one kind of textile composite. structures with complex shape can be manufactured easily by three dimensional braiding technologies. three dimensional braided composite has higher impact resistance and higher damage tolerance than other textile composite have

    三維編織復合材料是紡織復合材料的一種，三維編織技術可以製造任意復雜形狀的構件並且三維編織復合材料具有更高的抗沖擊性能和損傷容限，使三維編織復合材料的研究受到高度的關注。
  10. For the fine solution of this problem, the author has made an attempt to introduce the object - oriented technique to damage tolerance analysis. a set of basic and auxiliary classes, based upon some important concepts of object - oriented technique, which can be directly used for the development of programs of damage tolerance analysis has been designed and implemented by c + + language

    為此，本文將面向對象的程序設計方法引入到損傷容限分析中，運用面向對象觀點對損傷容限分析方法和數據需求作了全面分析，設計了一套損傷容限分析的基本類庫和輔助類庫，建立了損傷容限分析的對象模型，並採用c + +語言進行了實現。
  11. The fem model was accurate and effective by using submodel and error estimation technique that ensured the reliability of calculation and analysis. the thesis got the measure of critical flaw and designing life of the girder. in addition, the thesis calculated the remaining life of the girder while the flaw reaching 150mm

    結合有限元分析結果和損傷容限設計方法，本文計算了馬鋼第三煉鋼廠4 # 125t鑄造起重機主梁下蓋板的臨界裂紋尺寸，及初始裂紋為0 . 5mm時主梁的設計壽命，並估算了在裂紋尺寸達到150mm時主梁的剩餘壽命。
  12. As the damage tolerance technique has being widely and deeply adopted in the design and life prediction of aircraft structures, the development of high performance and more suitable software used in damage tolerance design and assessment is more urgent. while at the same time the existing domestic software is not well suitable for requirements in engineering

    隨著損傷容限技術在飛機結構設計和壽命評估中的廣泛採用，研製高性能且實用的損傷容限分析與評定軟體系統越來越迫切，而國內現有的損傷容限分析軟體經實踐證明其性能和適用性不能很好滿足工程需要，特別是結構剩餘強度和裂紋擴展分析程序。
  13. The second part concerns about the fracture analysis of cracked metalic structures. the last part investigates the behavior of impact dents on aircraft windshield glass and their possibility to be analyzed using fracture mechanics. in chapter 1, a review is made to the resent developments of cumulative damage models and fatigue life prediction methodology of composite laminates

    本論文研究飛機結構疲勞和損傷容限分析中的若干問題，按研究的對象（材料、結構）可以大致劃分為三個組成部分：復合材料層壓結構疲勞分析，第一章第三章；金屬結構斷裂分析，第四、五章；座艙蓋玻璃撞擊損傷的斷裂分析，第六章。
  14. Focusing on the micro construction of concrete materials, some research has been done. based on the former accomplishment and two theories : fraction mechanics and damage mechanics, the thermal damage model is established. the temperature damage developing equation is presented, as well as the calculation of arch construction

    本文在總結前人研究成果的基礎上，從混凝土材料組成的微細觀角度出發，應用混凝土斷裂力學和損傷力學理論對混凝土材料在溫度荷載作用下的損傷問題進行了理論與試驗研究，提出了混凝土溫度損傷模型，並導出了混凝土溫度損傷演變方程，最後用損傷有限元對拱型結構進行了數值計算，論文的具體內容如下： 1
  15. Therefore, interlayer toughened composites are the excellent candidate materials for primary structure of aircrafts. in this paper, composites modified with particle - interlayer were fabricated. based on the aims of improving compression strength after impact ( cai ) and evaluate damage resistance and damage tolerance, mode ii fracture toughness test and quasi - static indentation test ( qsi ) were conducted

    本文採用層間顆粒增韌技術制備試驗件，基於提高沖擊后壓縮強度（ cai ）和考察損傷阻抗、損傷容限的目的，試驗測試了型層間斷裂韌性g _ （ c ） 、準靜壓痕（ qsi ）試驗的分層起始能量和接觸力?凹坑深度關系。
  16. Therefore, the structural damage diagnosis which makes use of structural dynamic response to identify the physical parameter, sequentially to assess the performance of the structure and to realize the finite element model updating has become the advancing front of civil engineering researches

    對于重大土木工程結構，容易實現和量測的是結構的動力響應。利用結構的動力響應識別結構的物理參數，並進而評價結構性能、判別結構的損傷以及實現結構的有限元模型修正已成為新世紀土木工程領域的一個前沿研究熱點。
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