故障間隔 的英文怎麼說

中文拼音 [zhàngjiān]
故障間隔 英文
time between failures
  • : Ⅰ名詞1 (事故) event; incident; happening; accident 2 (原因) cause; reason 3 (朋友; 友情) fr...
  • : Ⅰ動詞(阻隔; 遮擋) block; hinder; obstruct Ⅱ名詞(遮擋物) barrier; block; obstacle
  • : 間Ⅰ名詞1 (中間) between; among 2 (一定的空間或時間里) with a definite time or space 3 (一間...
  • : partitionseparate
  • 故障 : hitch; breakdown; stoppage; fault; faulting; accident; blunder; bug; conk; failure; impairment; i...
  • 間隔 : interval; space; spacing; blanking; blank; region; distance; gap; intermission
  1. Combination fuse - switch ( cfs ) unit compartments shall be designed and type - tested for arcing fault containment where the energy level available to the input terminals of the compartment exceeds 1, 000, 000 a2 seconds

    試譯:式組合熔絲開關櫃( cfs )的室設計應滿足,在室的輸入端子的有效能級超過100萬安培秒之處,能進行閃包容以及閃包容的型式試驗。
  2. Based on establishing a failure distribution model repository, the failure distribution is obtained by parameter estimating and goodness - of - fit testing. 2. decision - making technologies of maintenance ways and maintenance interval are studied

    在建立裝備分佈模型庫的基礎上,研究了參數估計和擬合優度檢驗的方法,據此確定了裝備分佈; 2 、研究了裝備維修方式和維修期決策技術。
  3. Mean time between failures mtbf

    平均故障間隔
  4. Mtbf mean time between failure

    平均故障間隔
  5. Mean time between failure mtbf

    平均故障間隔
  6. Time between failures

    故障間隔
  7. At the same time, the formulas on reliability, mean time to failure and availability, mean time between failure etc were deduced respectively based on the distribution density function and markov state - transition diagram

    同時依據分佈密度函數和馬爾可夫模型的數學理論分別推導了兩種系統的可靠度、平均前時和可用度、平均故障間隔等指標的計算公式,為軟體內核程序的開發奠定了理論基礎。
  8. Basing on the mission requirement of a new type radar, this paper analyses the weakness of traditional mtbf centered design concept, and presents a new design concept of reliability, maintainability, and supportability ( rms ) centered maintenance free operating period

    摘要根據新型雷達任務的需要,對傳統的以平均故障間隔為中心的設計思想的不足進行了分析,提出了基於無維修工作期的可靠性、維修性、保性設計思想。
  9. The count of failure includes that of failure classification and failure pattern ; reliability indicator includes mean time to first failure ( mttff ) and mean time between failure ( mtbf ) ; life indicator includes feature life, center life, and specified life

    其中,統計包括類別的統計和模式的統計;可靠性指標包括平均首次里程mttff和平均故障間隔里程mtbf ;壽命指標包括特徵壽命、中位壽命、額定壽命等。
  10. Arid an algorithm of parity residuals and the theory of residual vector probability - data fusion are used for detecting the abrupt change failure of srfcs, especially the failure of actuators ' failures and single control surface ' s failures

    該系統是按照軟體工程規范,採用等價空法和殘差向量的概率信息融合法研製和開發的,不僅能對飛行控制系統的突變作動器卡死和控制舵面損傷進行實時檢測和離,而且具有良好的用戶界面。
  11. A fault threshold expressed in terms of the number of faults in a prescribed period of time

    以「在規定的時內出現的」次數來表示的一種閥值。
  12. A pressure transducer was set up in this system to realize pressure control in main lines and adjustment of pump operating time ; the distributors were designed to accomplish grease storage in fixed quantity and transport them into all lubricating points ; the single chip microcomputer was utilized to control interval lubrication and realize auto - lubricating or fault alarm

    系統通過設置壓力傳感器實現主油路的壓力控制和油泵工作時的自動調節,通過配油器實現定量儲油和將油脂輸送至各潤滑點,通過電子監控器設定加脂,實現自動加脂與報警。
  13. This layout can stop the internal arc fault expansion ; can avoid harmful moisture, small animal and dusty interferences. it also has good perfomiance and high reliability. because the heat cannot transmit to the outside of the bus room, a good operation environment for the low space can be obtained

    主母線室置於箱體頂部一個單獨的金屬封閉的內,並與10kv開關室、儀表室等相互獨立,為同類產品首創;這種結構可以防止內部電弧的擴大化,避免「火燒聯營」事;防護性能好,防潮、防小動物侵害、防積塵,運行可靠;由於母線室的熱作用,為下層空創造了一個較好的運行環境。
  14. The failure modes are not inspected, and when the system is working, it is inspected once every random time until it attains the failure modes or until it is detected to be in an abnormal work mode

    系統開始工作后,每一段隨機時對它檢測一次,直到系統或檢測出系統處于異常狀態為止。
  15. A decision model of maintenance ways based on rcm logic analysis is established. then maintenance ways of equipments are made according to the result of failure mode effect analysis. finally maintenance interval is calculated and confirmed after the related algorithm is chosen according to the army ’ s practical application

    建立了基於rcm邏輯決斷分析的裝備維修方式決策模型,並根據裝備模式和影響分析的結果確定裝備的維修方式,再根據具體裝備選擇相關演算法,計算裝備合理的維修期; 3 、研究了裝備維修級別決策技術。
  16. Oscillating displacement pump which may achieve a considerably longer trouble - free operation than a conventional diaphragm piston pump

    往復式容積泵,有比傳統膜活塞泵長的多的無運行時
  17. Mean time between system failures must be no greater than once per week

    系統的平均不能大於每星期一次。
  18. B fault detection : detection and indication of inter - phase and earthed phase fault, detection of broken wire, transmission of fault data, fault isolation and service restoration

    檢測功能:檢測發生的時歷時過程,電流電壓的幅值和方向,錄波和報文記錄,遙測報文上送,與配電主站配合完成離和事恢復。
  19. The distribution network automated system ( das ) is a management information system, including computer software and hardware technology, the computer network technology, the automatic control technology, the data communication technology and electrical power system technology, and it is utilized to acquire the data from power distribution network, monitor operation, position breakdown fast, isolate the failure, restore the power supply and administrate need, what ’ s more, it reduces the time of power cut effectively, improve the reliability and quality of power supply

    配電自動化系統( das )是集計算機軟硬體技術、計算機網路技術、自動控制技術、數據通信技術及電力系統相關技術於一體的信息管理系統,為配電網路的數據採集、運行監視、快速定位、離、供電恢復以及需求側管理等提供了有力的技術手段,能夠有效地縮短事停電時、提高供電可靠性、改善供電質量。
  20. Abstract : the control reconfigurable aircraft with multi - surfaces needs robust basic flight control system to support enough time for failure detection and isolation. when partial surface loses, it can keep the damaged aircraft stable. in this paper, multivariable output feedback digital control laws are designed for the control reconfigurable aircraft ( cra ). the method uses fast - sampling digital pi controllers to design digital flight control tracking system. this paper gives the way to design the controller and analyze its robustness characteristics. the simulation results indicate that the controller is very robust and the output responses are fully satisfactory

    文摘:控制可重構飛機要求其基本飛行控制系統對舵面部分缺損具有強的魯棒特性,在發生后保證飛機的穩定性,提供足夠的時進行的檢測和離,為控制系統重構提供條件.本文採用高速采樣pi控制器設計輸出反饋跟隨系統,給出了控制器的設計方法,並分析了它對于控制舵面部分缺損的魯棒特性.模擬結果表明,這種控制器具有好的魯棒特性
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