緩沖系統 的英文怎麼說

中文拼音 [huǎnchōngxìtǒng]
緩沖系統 英文
buffer system
  • 緩 : Ⅰ形容詞1 （遲; 慢） slow; unhurried 2 （緩和; 不緊張） not tense; relaxed Ⅱ動詞1 （延緩; 推遲） d...
  • 系 : 系動詞（打結; 扣） tie; fasten; do up; button up
  • 統 : Ⅰ名詞1 （事物間連續的關系） interconnected system 2 （衣服等的筒狀部分） any tube shaped part of ...
  • 系統 : 1. （按一定關系組成的同類事物） system 2. （有條理的;有系統的） systematic
  1. A buffer system resists a change in ph.

    緩沖系統對pH的變化是有耐受能力的。
  2. The world's natural ecosystems act as a buffer.

    地球上的自然生態系統起著一種緩沖的作用。
  3. A new measurement system for electrical conductivity in an yj - 3000t press fitted with a wedge - type cubic anvil was set up on the basis of the old one. a solartron 1260 impedance / gain phase analyzer was used in the new system ; mo electrodes and a mo shield were also used to keep oxygen fugacity close to the mo - moo2, which is similar to that of iron - wustite ( iw )

    在yj ?緊裝式六面頂壓機上，對原有的礦物、巖石電性測量系統進行了進一步的改進：建立了一套以solartron1260阻抗增益?相位分析儀為測試儀器，使用mo電極和mo盾來控制樣品氧逸度的測量系統，該系統的氧逸度環境為mo ? moo _ 2 ，接近iw緩沖對。
  4. On the basis of it, this thesis sets up three sets of different types of pneumatic cushioning systems and successfully realizes their high - speed pneumatic cushioning control

    在此基礎上，本文成功完成三套計算機控制智能高速氣動緩沖系統的研製工作，並實現了系統的高速氣動緩沖控制。
  5. Now with the development of computer control technique applied in it, computer control technique has had a profound influence on pneumatic system structure / control performance / control theory etc. this thesis deeply researches on the task - computer control smart high - speed pneumatic cushioning system. which mainly includes the design of mechanical structure / electronical circuit / pneumatic loop and the researches of system modeling / simulation / control strategy

    計算機控制技術和電-氣比例伺服控制技術的結合，更是對控制系統的性能、系統的結構以及控制理論等多方面都產生了極為深刻的影響。本文對計算機控制智能高速氣動緩沖系統進行了機械、電氣、氣路系統的設計以及系統建模方法、系統辨識研究和控制策略研究。
  6. The paper described the building process of model that can identify the shock - absorber parameter of landing gear and at the same times optimize performance of system. in this paper, there are also some debate, it include identifying parameter which can not be measured, such as the air polytropic exponent and the orifice discharge coefficient of shock - absorber

    本文利用復合形優化演算法建立了起落架緩沖系統參數識別與系統優化模型，對緩沖器空氣壓縮多變指數和油孔流量系數等不可測參數的識別和著陸、滑跑載荷多目標優化問題進行了討論。
  7. This paper begin with the concept system and system simulation, treat the landing gear as a system, use the concept of system simulation to establish the mathematical models of the landing gear, and to begin the simulation research

    起落架軟體平臺的開發和應用在我國有著廣闊的發展前景。本文的目地是以系統模擬的概念入手，將起落架緩沖系統進行動力學的數學建模和模擬建模。
  8. In this paper, the mathematics model and simulation model of the passive landing gear shock absorber was built, and was verified by drop test. aimed at acquiring suitable efficiency diagrams, two simple semi - active control algorithms were designed. the mathematics model and simulation model of the semi - active landing gear shock absorber was built

    在本文中，建立了被動控制起落架緩沖系統數學模型和模擬模型，並通過落震試驗對該模型進行參數校驗；以合適的功量圖為控制目標設計出兩種半主動簡單控制律，建立了半主動控制起落架緩沖器數學模型和模擬模型；通過數字模擬對這兩種控制方法進行了比較，認為半主動控制較被動控制有很大的優越性。
  9. The predigested calculating model about lunar soft - landing damping system is established in the course of landing shock. the dynamic computer simulation model is established according to the structure parameters

    建立了磁流變阻尼器緩沖系統沖擊時的簡化模型，利用本文建立的動力學方程和所用阻尼器結構參數構建了動態模擬模型，並進行了計算機模擬。
  10. Foreign lunar soft - landing damping systems in the last years are analyzed and studied. according to the virtue of mrf, lunar soft - landing damping system based on mrf dampers is developed

    在對近年來國外常用的登月軟著陸緩沖系統進行分析研究后，針對磁流變液的優良特性，提出了磁流變阻尼器軟著陸緩沖系統。
  11. Chapter four first researches the structure design of computer control samrt cushioning system and the signal processing. then mainly studies the design of pid / pdf control algorithm and their parameters tuning. finally analyzes the basic characteristics of electropneumtic proportional / servo trace controlled system, especial study the influence of the valve dead zone, system friction and saturation phenomenon

    第四章首先研究了計算機控制智能緩沖系統的結構設計、信號處理；然後重點研究了pid 、 pdf控制演算法的設計及其參數整定；最後研究分析了控制系統的基本特性，著重分析了閥口死區、系統摩擦力和氣路飽和特性等對系統控制性能的影響。
  12. A notification occurs when the event - buffering system sends out messages for accumulated events

    當事件緩沖系統發出累積事件的消息時，就會出現通知。
  13. A notification occurs when buffering is disabled, the event - buffering system sends out messages for accumulated events, or an event occurs and the event - buffering system is disabled

    當緩沖被禁用、事件緩沖系統發出累積事件的消息時，或者在發生了事件而事件緩沖系統又被禁用時，將出現通知。
  14. The chapter 3 focused on the hydraulic damping system

    第三章著重分析研究了沖裁緩沖系統。
  15. In general, the control methods of the aircraft ' s landing gear shock absorbers are classified three categories : a passive type, an active type, and semi - active type

    一般地說，飛機起落架緩沖系統的控制方式有三種：被動控制、主動控制和半主動控制。
  16. Among them, as a compromise between active control and passive control, the controllability of semi - active control is access to full active control, and in the same time, the method is simpler, lighter and safer than full active control. it ' s suitable for the applications in landing gear shock absorbers

    其中半主動控制介於被動控制和主動控制兩者之間，具有類似主動控制的可控性，同時具有結構簡單、重量輕、安全性高的特點，適合於在起落架緩沖系統中的應用。
  17. A buffer system resists a change in ph

    緩沖系統對ph的變化是有耐受能力的。
  18. We still adopt traditional method about the design and analysis of landing gear buffer system at present in china

    起落架緩沖系統的設計和分析，在我國主要還是採用傳統的方法。
  19. Some of the relationship between the performance and some factors of the hydraulic damping system was found out according to the calculation and analysis

    然後針對50000kn汽車大樑液壓機的緩沖系統，分別從靜態和動態兩個方面進行了分析計算。
  20. At last, an available landing gear simulation software is developed, and different simulation results are made through modify the parameters

    為以後自主開發一套各種形式的起落架緩沖系統動力學模擬軟體平臺，奠定了基礎。
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