蠕變疲勞 的英文怎麼說

中文拼音 [biànláo]
蠕變疲勞 英文
creefatigue
  • : 動詞(蠕動) wriggle; squirm
  • : 形容詞(疲乏; 勞累) tired; weary; exhausted
  • : Ⅰ動詞1 (勞動) work; labour 2 (煩勞) put sb to the trouble of; trouble sb with sth : 勞您費心...
  • 疲勞 : 1. (疲乏勞累) tired; fatigued; weary; become fagged 2. (機能或反應能力減弱) fatigue; strain 3. [物理學] fatigue
  1. Entron aisie is a share of the digestive system of human body, will be had dianhoea lf ansing pathological changes, lt is had that constipatiao adsorb, with vanous plant shrewd oll prescnption, stlff lnfiltation promtes enteron aisle into the regulation enteron aisle and cell of human body, through prefesslobal skill to wnggle, it is lasting to stengthen function health, eliminate function obstacle

    腸道是人體消化系統的一部分,如出現病會腹瀉,便秘,吸收不良,採用多種植物精油配方,強力滲透進人體細胞,調節腸道,通過專業的手法,促進腸道動,強化功能健康持久,消除障礙。
  2. The expressions of interaction fatigue - creep life and of thermal shock damage evaluated by modulus were obtained by the experimental analysis

    通過試驗分析,初步得到壽命表達式和模量表徵的熱震損傷表達式。
  3. We use the method of finite element analysis to find the most dangerous section of the rotator. through setting up a model of rotator, calculating the temperature and stress field of rotator, we get the section. then we supervise the section online, calculate the practical fatigue life loss and creep life loss

    我們使用有限元分析法,通過建模,計算轉子溫度場、應力場,得到最危險截面,然後對危險截面進行在線監測,計算實際運行中的壽命損耗和壽命損耗,為安全經濟運行提供有效監控手段。
  4. Accounting for creep and stress relaxation, a long - term life and low cycle fatigue life prediction method for gas turbine engine hot section is established

    摘要建立了考慮和應力鬆弛的航空發動機渦輪葉片等高溫構件的持久壽命和低循環壽命預測方法。
  5. Application of updated concurrent subspace optimization in the structural optimization with constraints of aerodynamics and rcs of aircraft

    可靠性敏度分析方法及其在非線性蠕變疲勞失效模型中的應用
  6. The influence factors of fracture life are composites boards lay structure, wood - lacuna, and bamboo structure

    影響斷裂壽命分散性的因素主要有層合板的鋪設結構、木材缺陷和竹材結構等的影響。
  7. 3d - c / sic fabricated with t300 carbon fibers weaved into 3 - dimensional and 4 - directional structure, was deposited pyrocarbon and sic matrix at 950 - 1000 with cvi method. fiber volume fraction of 3d - c / sic was 40 - 45 %, composite density was 2. 01g / cm3 and porosity was 17 %. in addition, the thickness of pyrocarbon interface was 200 nm for interaction fatigue - creep ; the interface layer of pyrocarbon for thermal shock had three thickness obtained by controlling deposition time which were 10h, 20h, 30h, respectively

    3d - c sic是用t300碳纖維編織成三維四向編織體, cvi法在950 - 1000緻密,纖維體積分數為40 - 45 ,密度為2 . 01g cm ~ 3和孔隙率為17 ,用於交互作用試驗熱解碳界面層厚度約0 . 2 m ;用於熱震試驗的有三種界面層厚度分別是熱解碳沉積時間10小時、 20小時、 30小時獲得。
  8. Facture damage behavior of wood - bamboo composites board under the mutual action of fatigue and creep was studied

    摘要研究了在交互作用下竹木復合層合板的斷裂損傷行為。
  9. And under the three conditions ( fatigue, creep and interaction fatigue - creep ), the damage caused by the interaction fatigue - creep was the most severe

    交互作用這三種條件下,以交互作用對材料的損傷最大。
  10. Under the mutual action of fatigue and creep, the destroy form of the composite board is mainly the syntheses of the fiber fracture, interface destroy and interbedded crack

    交互作用下層合板的破壞形式主要為纖維撕裂、界面剪切破壞和層間開裂3種形式的綜合表現。
  11. Thermal shock behavior and interaction fatigue - creep of 3d - c / sic had been investigated in the three environments ( argon, dry oxygen, wet oxygen ) in the preset work

    本文研究了3d - c sic在空氣介質下的熱震損傷規律和在三種介質(氬氣、干氧和濕氧)下的的損傷規律。
  12. Results showed that the curves of fatigue / creep have three stages at the 75 % stress and the curves of fatigue / creep have two stages at the 55 % stress

    結果表明,在交載荷最大值為75 %的應力水平下,其斷裂曲線為3段式曲線;在55 %的應力水平下, 15小時內其曲線為兩段式曲線。
  13. So far, many studies on general properties of 3d - c / sic have been carried out, but the study on its interaction fatigue - creep and thermal shock behavior, especially at high temperature, has not been reported

    文獻中對其常規力學性能研究較多,而對其熱震和交互作用行為鮮見報道。
  14. Therefore, a systemic and in - depth study is of significant importance for improving, engineering design and application of 3d - c / sic on the interaction fatigue - creep and thermal shock properties

    研究3d - c sic熱震和交互作用行為和積累更全面的性能數據,對改進該材料、工程設計和應用具有重要的意義。
  15. Several types of damage had been identified, including the matrix microcrack, fiber fracture, debonding and sliding between fiber - bundles, and fiber oxygen involved in the interaction fatigue - creep of 30 - c / sic composites

    3d - c sic1300交互作用的損傷形式包括基體開裂、纖維和纖維束的斷裂和拔出,還有纖維的氧化而引起的損傷。
  16. During the operation of equipments in the modern industry, the interaction of fatigue - creep under complex condition is often the cause of the failure of equipments. for the other side, with the rapid development of science and technology, the study like this is booming, and the subject is becoming an integrated subject including macro - mechanics, metal microstructure and so on

    現代石化行業中的設備在操作過程中,破壞以及材料的交互作用影響著設備的使用壽命;隨著科學技術的飛速發展,-交互作用研究也已經成為宏觀力學理論與金屬微觀結構學等綜合為一體的新興學科。
  17. And the finite element method ( fem ) was used to simulate the stress and deformation of the outer casing and the bearing chock. on the basis of the experiments and fem analysis, the strength and fatigue lifetime, the interaction of creep and fatigue lifetime, the creep lifetime of outer casing and bearing chock have been analyzed, at the end of trail, sem analyses of failure section has been conducted

    同時對航空發動機燃氣渦輪外機匣和軸承座進行了有限元模擬計算,得到外機匣和軸承座的焊接處的強度和形情況的模擬結果。根據試驗數據和有限元的計算結果,對發動機燃燒室外機匣和軸承座兩種結構(包含焊縫)進行靜強度分析、壽命分析、壽命分析、蠕變疲勞交互作用壽命分析以及斷口的金相分析。
  18. This paper discusses life - wastage of creep - fatigue for headers of superheater and reheater and algorithm of this two kinds wastage. based on these theories, b - p neural network with self - organized function has been introduced detailedly to calculate the fatigue wastage. at the same time, the paper introduces the calculation method of stress

    本文主要介紹了過熱器和再熱器聯箱的壽命損耗的問題以及這兩種壽命損耗的計算方法,並在此基礎上採用前饋型網路( b - p )來計算高溫低周的壽命損耗(交互作用) 。
  19. According to the failure factors, the mechanism, the processes, the critical conditions, the aftereffects etc, the main steam pipe ' s failure patterns are divided into five types : frangibility, toughness, high temperature, creep, fatigue, the processes and characters of each type is analyzed and summarized

    根據主蒸汽管道失效因素、失效機理、失效發展過程、失效臨界條件、失效後果等幾個方面,確定了主蒸汽管道失效的五種形式,即脆性失效、韌性失效、高溫失效、失效和失效,並對每種失效形式的過程和特徵進行了分析。
  20. The expressions of the creep damage is acquired by performing the plexiglas creep test and the fatigue test at the different frequencies. the method for separating the creep damage from the fatigue damage is set up through the analysis. the life under the joint action of the creep and the fatigue was estimated with this method, which is compatible with the test results, so this method is of satisfactory ability in life prediction

    開展了有機玻璃試驗和不同頻率下的試驗,擬合得出了損傷計算公式,通過研究,建立了損傷和純損傷的分離方法,並用此方法對/共同作用下的壽命進行了預測,與試驗結果吻合較好,說明該方法有很好的壽命預測能力。
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