渦動反應器 的英文怎麼說

中文拼音 [guōdòngfǎnyīng]
渦動反應器 英文
vortex reactor
  • : 渦名詞1. (漩渦) eddy; whirlpool; vortex 2. (酒窩) dimple
  • : Ⅰ名詞1 (方向相背) reverse side 2 (造反) rebellion 3 (指反革命、反動派) counterrevolutionari...
  • : 應動詞1 (回答) answer; respond to; echo 2 (滿足要求) comply with; grant 3 (順應; 適應) suit...
  • : 名詞1. (器具) implement; utensil; ware 2. (器官) organ 3. (度量; 才能) capacity; talent 4. (姓氏) a surname
  1. Nuclear power station with pressurised water reactor is basically divided into the " nuclear island " where steam is produced in the steam generator by nuclear power generated from a reactor, a " conventional island " where steam supplied from the nuclear island is used to drive the turbine - generator to produce electricity, and the balance of plant ( bop ) which consists of the station auxiliaries and ancillary plants, etc

    採用壓水式堆的核電站基本分為核島、常規島和核電站其他部分。由堆產生的核能會通過在核島內的蒸汽發生產生蒸汽,而核島所供的蒸汽會推常規島內的輪發電機發電。核電站其他部分則包括站內的輔助設備及附屬設施等。
  2. Nuclear power station with pressurised water reactor is basically divided into the " nuclear island " where steam is produced in the steam generator by nuclear power generated from a reactor, a " conventional island " where steam supplied from the nuclear island is used to drive the turbine - generator to produce electricity, and the balance of plant which consists of the station auxiliaries and ancillary plants, etc

    採用壓水式堆的核電站基本分為核島常規島和核電站其他部分。由堆產生的核能會通過在核島內的蒸汽發生產生蒸汽,而核島所供的蒸汽會推常規島內的輪發電機發電。核電站其他部分則包括站內的輔助設備及附屬設施等。
  3. Abstract : this paper briefly presents th e application of advanced brazing techniques for a larye number of assemblies of space vehicles, such as thrust chamber and turbine rotor of launch rock et engine, titanium tube of satellite, attitude control engine injector and wave guide component of satell ite, reflector, tube and honeycomb panel of manned spacecraft, main engine nozzl e and preburner of space shuttle as well as the pipeline systems of space statio n

    文摘:簡略地介紹了先進釬焊技術在航天部件,例如運載火箭發機的推力室和輪轉子、人造衛星的鈦導管、姿控發機噴注和波導件、載人飛船的、導管和蜂窩壁板、航天飛機的主發機噴管和預燃室以及空間站的管路系統等的廣泛用情況。
  4. 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

    本文基於簡單的旋分裂模型,建立了固體火箭沖壓發機補燃室內的湍流燃燒模型,並在該模型下對某實驗發機進行了三維數值模擬,研究了補燃室設計參數包括進氣道出口設計參數和燃氣發生噴管設計參數對燃燒效率的影響。
  5. In this article, constituting some the equations which reflect the flow law and building and applying many mathematical models of physical and chemical reactions in the the plasma ignition : applying k - two equations turbulence model to calculate the turbulence parameter supplying simplied reaction systerm model and applying eddy break - up model and p - i thermal radiation model. with these reasonable simplied modles, numerically simulating the flow field in the plasma ignition. during the numerical simulation, applying the body - fitted coordinates for the complex geometry of the computional field ; using the mixing format to disperse the equations ; applying simplec algorithm method to solve the equations ; using above models and methods, it can get flow field distribution ; including temperature, pressure, turbulent kinetic energy and its dissipation rate, turbulent viscosity, velocity, density. these results are significant to design and improve the plasma ignition

    本文旨在通過構造映等離子點火內部流規律的基本方程組,建立描述等離子點火內部的復雜物理化學過程機制數學模型:模擬等離子發生內部燃燒的-雙方程湍流流模型;模擬氣體燃料在燃燒時中化學的簡單化學系統模型;模擬等離子點火內部湍流預混燃燒的漩破碎模型;模擬等離子點火高溫燃氣及其壁面的p - i輻射換熱的模型等等,對模型進行一定的合理的簡化,然後數值模擬等離子點火內部流場的流
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