combustion mechanism的意思
combustion mechanism中文翻譯:
燃燒機理
mechanism───n.機制;原理,途徑;進程;機械裝置;技巧
combustion───n.燃燒,氧化;騷動
combustion air───[熱]助燃空氣;[熱]燃燒空氣
combustion chamber───燃燒室; 爐膛;[動力]燃燒室
antiasthmatic mechanism───平喘機制
spontaneous combustion───n.自燃
coping mechanism───應對機制,應付機制
escapement mechanism───[儀]擒縱機構
combustion tube───[分化]燃燒管;縱火筒
of water-blend heavy oil and combustion mechanism were discussed.───重油摻水乳化的實質及乳化油燃燒過程進行了探討。
combustion mechanism of spheric propellants obtained is discussed reasonably.───對所制備球形藥的燃燒機理提出了合理的解釋。
useful to carry out the re-search on the combustion mechanism in coal outcrop.───研究煤層露頭火區氧氣輸運、逾滲規律、露頭火災機理具有積極意義。
Based on the combustion mechanism of PP, effects of different nano-fillers on the intumescent flame retarded PP composites were discussed.───本文基于聚丙烯的燃燒機理,討論了不同納米材料對膨脹阻燃聚丙烯復合材料阻燃性能的影響。
Based on the combustion mechanism of polymer material, measures of reducing the toxicity and damage to environment are also given.───根據高分子材料燃燒機理,提出了減少煙氣毒性和環境危害的措施。
Though the pre-chamber stratified-charge combustion system has been in use for years, its combustion mechanism is not yet fully understood.───盡管分開式分層充氣燃燒系統已有了實際應用,但對它的燃燒機理尚未完全了解。
Boron Trioxide and Carbon Content Determination in Combustion Residue of Boron-Containing Solid Propellants and Their Combustion Mechanism───含硼固體推進劑燃燒殘渣中三氧化二硼和碳含量測定及燃燒機理研究
Perspectives on spontaneous combustion mechanism and prediction theory of coal───煤自燃機理及預測理論研究進展
The Computation and Analysis on the Reduced Combustion Mechanism for a LPG Engine───LPG發動機機理簡化及其適用性的計算與分析
Physicochemical properties and combustion mechanism of boron are introduced. Long ignition delay time and low combustion efficiency are due to the properties of boron itself.
The combustion mechanism and the variation of residual carbon value of the HS A diesel oil are analyzed and some test conditions given.
Based on the thermochemistry and chemical kinetics, the combustion mechanism and flowing direction of combustion heat for the three main species of solid fuels was studied.
The combustion mechanism of RDX modified double base spheric small size propellants is presented.
A mathematical model was set up to calculate the minimum ignition energy based on thorough analysis of combustion mechanism of the engine combustible mixture.
The combustion catalyst adopted by ordinary double base propellant can adjust the burning rate. It's necessary to study further on the combustion mechanism.
The combustion mechanism of spheric propellants obtained is discussed reasonably.
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