進氣進氣口 的英文怎麼說

中文拼音 [jìnjìnkǒu]
進氣進氣口 英文
air inlet
  • : 進構詞成分。
  • : Ⅰ名詞1 (氣體) gas 2 (空氣) air 3 (氣息) breath 4 (自然界冷熱陰晴等現象) weather 5 (氣味...
  • : Ⅰ名詞1 (人或動物進飲食的器官; 嘴) mouth 2 (容器通外面的地方) mouth; rim 3 (出入通過的地方) ...
  • 進氣 : air admission; admission; inlet; onflow; charging; access of air; admittance; air in; air intake;...
  1. While working, the air with dust enters into the sedimentation chamber via wind entrance, dust with large size granule will fall because of sudden expand of the aeriform cubage, then the air will pass the water area of arc boards of the two sides to stir the water. then air with dust will be mixed with water forming water curtain at the exit, fine powder will be collected, purified air will be discharged by blower fans via breakwater and wind exit

    工作時含塵空入沉降室由於體的體積驟然膨脹,大顆粒粉塵沉集下來,然後空經過兩側弧形板間的水域並將水攪動含塵空與水充分混合在出處形成水幕,較細的粉塵捕集下來,凈化后的空經擋水板和出風由風機排走。
  2. The fresh-air inlet was usually the crankcase breather cap.

    新鮮空一般是曲軸箱通蓋。
  3. Modern medical uses include : bronchitis, diarrhea, dysentery, hyperthyroidism, stretch marks, thrush, ulcers, vaginal thrush, viral hepatitis, asthma, athlete ' s foot, candida, catarrh ( mucus ), coughs, eczema, digestion, dyspepsia ( impaired digestion ), flatulence ( gas ), fungal infections, gingivitis, gum infections, hemorrhoids, support immune system, mouth ulcers, decongest prostate gland, ringworms, sore throats, skin conditions ( chapped and cracked ), skin inflammation, wounds, and wrinkles, toothpastes, mouthwashes, cosmetics, and food flavorings

    現代的醫藥用途包括:支管炎,腹瀉,痢疾,甲狀腺機能亢,緊張,鵝瘡,潰瘍,陰道的鵝瘡,哮喘,腳癬,粘膜炎,咳嗽,濕疹,消化不良,腸胃脹,真菌感染,齒齦炎,齒齦感染,痔瘡,支持免疫系統,潰瘍,解除前列腺充血,癬茵病,咽喉痛,皮膚問題(乾燥和裂開) ,皮膚發炎,傷和皺紋,還可用作牙膏,漱水,化妝品和食物調味料。
  4. The thesis focuses on the development of the dynamic simulation model of evaporators, the accomplishment of the stable and dynamic simulation of the parameters of cryogen - side, air - side and how to carry out dynamic simulation on the refrigerating effect of evaporators under different evaporating temperature and the realization of the analyses and calculations of the main parameters, such as, the wind speed of air - side and specific humidity etc, which affect the function of evaporators

    本文重點是對蒸發器建立動態模擬模型,並對製冷劑側和空側參數行穩態和動態模擬,同時對蒸發器在不同蒸發溫度下的製冷量行了動態模擬,而且對影響蒸發器性能的主要參數(空側入風速、入含濕量等)行了分析和計算。
  5. A high - pitched woodwind instrument consisting of a slender tube closed at one end with keys and finger holes on the side and an opening near the closed end across which the breath is blown

    由一根一端封閉的纖細管子組成的高音木管樂器,側邊有按鍵和指孔,靠近封閉端有一個使入的開
  6. Direct gas - fired door heaters ; addenda

    直接燃加熱器.補充件
  7. The effect of exit back pressure and length / height ratio of isolator on forebody / inlet flow field is analyzed and discussed in the paper

    本文還研究了隔離段出反壓及隔離段長高比對道流場的影響。
  8. With account for the effect of temperature and shock - boundary layer interaction, the forebody / inlet with plane lip and wedge lip are designed by using the design methods of constant shock wave intensity and constant shock wave angle. in the design, the incidence angle of the first ramp, height of isolator, length of forebody and total turning angle of the designed forebody / inlet models are given

    另外,根據優選結果,給定前體長度、前體預壓縮楔角、總壓縮轉角及隔離段高度,分別用等激波強度和等激波角度的方法設計了唇平直和唇帶楔角的前體道。
  9. The calculation results indicate that the starting performance of forebody / inlet with wedge - shaped lip is better than that with plane lip at low flight mach number. at high flight mach number, the performance of the forebody / inlets designed by the two methods is approximate. at low flight mach number, the starting performance of forebody / inlet designed by the method of constant shock wave intensity is better

    結果表明:唇帶楔角的道在低飛行馬赫數下的起動性能優于唇平直的道;採用等激波強度和等激波角度方法設計的道在高飛行馬赫數下的性能相近,在低飛行馬赫數下,採用等激波強度方法設計的道起動性能較優。
  10. Tom takes a deep breath, relaxes on the exhale, and says, " humph, sounds ii ike you had a hard day.

    湯姆深深吸,緩緩呼出,說: 「你今天好像很累。 」
  11. At the same time air is sucked into the inlet to replace the exhausted air.

    同時,外面空吸入代替被排出的空
  12. In this dissertation, the pulse jet style, the influence on the shock wave, the flow in the tube and the cooling effect was deeply studied theoretically and experimentally. the influence of the pulse jet style on the forming of shock wave and the shock wave intensity was explored. the initial disconnection style in oscillating tube vented and the initial disconnection breakdown was proposed by different pulse jet style

    本文對脈動射流的型式及其對激波、管內流動及冷效應的影響行了較系統的理論和實驗研究,主要包括:探討了脈動射流的型式對形成管內激波形成及激波強度的影響,給出了不同脈動射流的型式下振蕩管開端初始間斷的類型,對初始間斷行了分解,導出了包含、排參數及工質物性參數的管內入射激波馬赫數mj的表達式,給出了管內激波形成的三種原因及其所對應的脈動射流型式和具體的工作狀態。
  13. The results prove that : ( 1 ) when the mach number of the flow at the exit increases, the total pressure recovery decreases, and the circular steady total pressure distortion coefficient, turbulence intensity and synthesis distortion increase

    研究結果表明: ( 1 )地面工作狀態下,隨著出馬赫數的增加,蛇形道出截面的總壓恢復系數不斷下降,而穩態周向畸變指數、紊流度和綜合畸變指數均上升,穩態徑向畸變指數變化不大。
  14. With fluid dynamic derived from marine mammals and subtle character lines stretching down the body ; the powerful imposing view of our canopy in flight is simply stunning

    為了營造出古代羅馬戰神盔甲的雄壯勢,極度誇張霸的設計,搭配腮狀側孔,飛行時流直達動力核心,增強熱能疏散。
  15. In this paper, simple reacting flow model in solid - propellant ducted rocket combustor based on eddy break - up model is established. the model is used to simulate the three - dimensional combustion flowfields in an experimental motor. some factors how to affect the combustion efficiency are discussed in the paper, including air intake and gas generator nozzle

    本文基於簡單反應的旋渦分裂模型,建立了固體火箭沖壓發動機補燃室內的湍流燃燒模型,並在該模型下對某實驗發動機行了三維數值模擬,研究了補燃室設計參數包括道出設計參數和燃發生器噴管設計參數對燃燒效率的影響。
  16. Other regulatory programs included emergency and contingency plans, controls over importing and exporting natural gas, supervision of utilities and industry converting from oil and gas to coal, establishment of priorities for natural gas curtailment, and coordination of regional power systems

    其他的法律規范活動包括緊急和突發事件應對計劃、天然管制、對從石油和天然中制取焦碳的工業和應用的監管、壓縮天然優先性的制定,以及區域電力系統之間的協調。
  17. Qualified heat recovery rate acquired from the merge equation ' s resolve in terms of the fortran program and the hvac - id graph in the course of the theory calculation. determining the experimental equations applying the ortho imitated experimental design on the basis of the simple spray chamber. the experimental date originated running double - spray chamber ' s entrance and exit air

    理論計算中通過編制的fortran程序求解組合方程組,並結合hvac - id圖求得符合要求的熱回收率,其間試驗公式是在單噴水室的基礎上採用一次正交回歸試驗設計得到,試驗結果是通過對運行的雙噴系統中的室內外空狀態參數行測定而得到。
  18. The results show the exit back pressure and length / height ratio of isolator have great impact on exit flow field and starting performance of inlet. high back pressure of inlet will result in unstart

    研究表明:隔離段長高比對道出參數影響較大;隔離段出反壓不能太高,否則會引起道不起動。
  19. With computations and analysis, the comprehension on the mixing and combustion process is increased, and some significative results are listed below : a ) there are three recirculation regions and one vortex region in the combustor, and these recirculation regions affect the combustion process deeply, b ) increasing side - arm angle and moving side - air inlet position toward the fuel inlet can improve mixing and combustion characteristics, and increase the combustion efficiency, c ) when the angle between two air - inlets equals to 180

    通過計算與分析,增了對補燃室內摻混燃燒過程的理解,為固體火箭沖壓發動機補燃室設計提供了一些有意義的結果: 1補燃室內的流動十分復雜,存在三個迴流區和一個旋渦區,迴流區對摻混燃燒過程有重要影響; 2增大空入射角度、向前移動道出位置有利於增強頭部迴流區強度,增強摻混效果,燃燒效率上升; 3
  20. The raw material to be dried can not be polluted and the quality of raw materials to be dried can not be damaged

    都有空過濾器,不會污染被乾燥的物料,影響其品質。
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