C - combustor 中文

combustor n.【機械工程】燃燒室。

n. 【機械工程】燃燒室。 “annular combustor“ 中文翻譯：沖壓式宛氣噴氣動機; 環形燃燒室; 環行燃燒室“automatic combustor“ 中文翻譯：自動燃燒器“can combustor“ 中文翻譯：筒形燃燒室“cannular combustor“ 中文翻譯：環管燃燒室“combustor casing“ 中文翻譯：燃燒室機匣“combustor liner“ 中文翻譯：火焰筒“combustor pressure“ 中文翻譯：燃燒室壓力“conic combustor“ 中文翻譯：錐形燃燒室“conical combustor“ 中文翻譯：錐形燃燒室“counterflow combustor“ 中文翻譯：逆流式燃燒室“multiple combustor“ 中文翻譯：多室式燃燒室“tubular combustor“ 中文翻譯：管形燃燒室“vapourizing combustor“ 中文翻譯：汽化式燃燒室“annular chamber combustor“ 中文翻譯：環形燃燒室“baffle-type combustor“ 中文翻譯：環形燃燒室“camshaft annular type combustor“ 中文翻譯：環管形燃燒室“can annular combustor“ 中文翻譯：環管型燃燒室“can annular type combustor“ 中文翻譯：環筒形燃燒器“can-annular combustor“ 中文翻譯：筒環形燃燒室“can-type combustor“ 中文翻譯：分管型燃燒室“circulating fluidized bed combustor“ 中文翻譯：循環流化床燃燒室“combustor exit gas“ 中文翻譯：燃燒室出口燃氣溫度“combustor fuel-flow rate“ 中文翻譯：燃燒室燃料流量“combustor gas pressure“ 中文翻譯：燃燒壓力“combustive activation“ 中文翻譯：燃燒活化“combustiontube furnace“ 中文翻譯：燃燒管爐

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In the introduction the review of the research on a dual - mode scramjet combustor both abroad and domestic is presented and the main work of this paper is also presented briefly 第一章為引言，簡要回顧了國內外雙模態沖壓發動機燃燒室研究的現狀，并在結尾介紹了本文的主要工作。
U37ng natural gas furnace ; combustor ; sit valve ; ceramic simulation logs ; ceramic simulation ashes ; brick plate ; large straight front high temperature resistance glass window ; flame regulator U37ng天然氣爐體;燃燒室； sit閥體；陶瓷仿真圓木；陶瓷仿真灰燼；火焰調節器。
Pulsating spray drying technique makes use of the unstable hot gas stream generated by a pulse combustor to atomi / e and dry a liquid material 脈動燃燒干燥技術是近年來出現的一種新型干燥技術，它利用脈動燃燒器產生的高溫，高頻脈動尾氣流直接霧化和干燥液態物料。
Residual carbons have also been collected from two industrial cfb boilers and a pilot cfb combustor , as well as from coal particles burning statically in open air 比表面積變化較小，與焦碳失活無關。中低溫燃燒下，不同煤中存在的礦物質的催化作用不一樣。
Epstein ' s microengine only has two parts : a moveable rotor and a stationary structure that together function as the compressor and combustor 愛匹斯丁的微型引擎只有兩個部分：一個可移動的水平旋轉翼和一個固定結構，兩者一起作為壓縮機和燃燒器進行運作。
Epstein ' s microengine only has two parts : a moveable rotor and a stationary structure that together function as the compressor and combustor 愛匹斯丁的微型引擎只有兩個部分：一個可移動的水平旋轉翼和一個整體可當壓縮機和燃燒器作用的固定構造組織。
In order to simulate parameters of different diesel exhaust heat , an simulative multi - heat testing flat is set up with an combustor and two fans 采用燃燒器和兩個離心風機構成的二級送風系統組成模擬多熱源實驗臺，以模擬不同的內燃機余熱條件。
The effect of the combustor temperature , pressure and coefficient of residual oxygen was experimentally investigated when the fuel was injected into the combustor 對燃料噴入時的燃燒室溫度、壓力及推進劑余氧系數等工作參數進行了試驗研究。
Epstein ' s microengine only has two parts : a moveable rotor and a stationary structure that together function as the compressor and combustor 愛匹斯丁的微型引擎只有兩個部分：一個可轉動的的轉子和一個固定的腔室，它們共同成為壓縮機和燃燒機。
And the experimentation has been done . it ' s primary results were given , such as temperature and pressure curve for the combustor and gasifier 并進行了多聯產方案試驗，給出了燃燒爐、氣化爐的升溫曲線、床層壓降曲線等初步試驗結果。
The performance of supersonic inlet determines the pressure and the air flux in combustor , then affect the work of ramjet 超聲速進氣道的性能優劣決定了補燃室流場內的壓強和空氣流量,進而影響到沖壓發動機的工作性能。
The process of mixing and chemical reaction in the second combustor is very complicated , many factors affect the combustion efficiency 然而補燃室內燃氣同空氣的摻混燃燒過程十分復雜，影響燃燒效率的設計參數很多。
In developing the mathematical models of the combustor , a general numerical simulation program to simulate gas turbine combustor is drawn up 在建立數學物理模型的基礎上，編制了燃氣輪機燃燒室的通用數值模擬程序。
In the past years , design of gas turbine combustor depends mainly on empirical formulae derived from experimental data 長期以來，燃氣輪機燃燒室的設計方法主要是依靠試驗及由大量實驗數據歸納出的經驗公式。
The structure design and the performance research of supersonic inlet / combustor are key techniques for solid rocket ramjet 超聲速進氣道及補燃室的設計與性能研究是固體火箭沖壓發動機的兩大關鍵技術。
It is a key technique for ducted rocket to make the second combustor operate at high efficiency and stability 實現補燃室高效率、穩定、可靠的工作，是固體火箭沖壓發動機的關鍵技術問題。
Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows 本文通過數值模擬得到了超燃沖壓發動機燃燒室化學反應流流場的流動結構。
Numerical simulation of gas - solid two - phase flows in a swirling - flow combustor through the use of a modified k - - kp two - fluid model 雙流體模型用于模擬旋流突擴燃燒室內氣固兩相流動
It is shown that results of study are useful for the optimum design of an annular combustor with the swirler cup 表明本文的研究結果可為發動機環形燃燒室設計提供有用的依據。

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combustor

combustor n.【機械工程】燃燒室。

comby

Residual carbons have also been collected from two industrial cfb boilers and a pilot cfb combustor , as well as from coal particles burning statically in open air 比表面積變化較小，與焦碳失活無關。中低溫燃燒下，不同煤中存在的礦物質的催化作用不一樣。

Epstein ' s microengine only has two parts : a moveable rotor and a stationary structure that together function as the compressor and combustor 愛匹斯丁的微型引擎只有兩個部分：一個可移動的水平旋轉翼和一個整體可當壓縮機和燃燒器作用的固定構造組織。

In order to simulate parameters of different diesel exhaust heat , an simulative multi - heat testing flat is set up with an combustor and two fans 采用燃燒器和兩個離心風機構成的二級送風系統組成模擬多熱源實驗臺，以模擬不同的內燃機余熱條件。

The effect of the combustor temperature , pressure and coefficient of residual oxygen was experimentally investigated when the fuel was injected into the combustor 對燃料噴入時的燃燒室溫度、壓力及推進劑余氧系數等工作參數進行了試驗研究。

Epstein ' s microengine only has two parts : a moveable rotor and a stationary structure that together function as the compressor and combustor 愛匹斯丁的微型引擎只有兩個部分：一個可轉動的的轉子和一個固定的腔室，它們共同成為壓縮機和燃燒機。

And the experimentation has been done . it ' s primary results were given , such as temperature and pressure curve for the combustor and gasifier 并進行了多聯產方案試驗，給出了燃燒爐、氣化爐的升溫曲線、床層壓降曲線等初步試驗結果。

The performance of supersonic inlet determines the pressure and the air flux in combustor , then affect the work of ramjet 超聲速進氣道的性能優劣決定了補燃室流場內的壓強和空氣流量,進而影響到沖壓發動機的工作性能。

The process of mixing and chemical reaction in the second combustor is very complicated , many factors affect the combustion efficiency 然而補燃室內燃氣同空氣的摻混燃燒過程十分復雜，影響燃燒效率的設計參數很多。

In developing the mathematical models of the combustor , a general numerical simulation program to simulate gas turbine combustor is drawn up 在建立數學物理模型的基礎上，編制了燃氣輪機燃燒室的通用數值模擬程序。

In the past years , design of gas turbine combustor depends mainly on empirical formulae derived from experimental data 長期以來，燃氣輪機燃燒室的設計方法主要是依靠試驗及由大量實驗數據歸納出的經驗公式。

The structure design and the performance research of supersonic inlet / combustor are key techniques for solid rocket ramjet 超聲速進氣道及補燃室的設計與性能研究是固體火箭沖壓發動機的兩大關鍵技術。

It is a key technique for ducted rocket to make the second combustor operate at high efficiency and stability 實現補燃室高效率、穩定、可靠的工作，是固體火箭沖壓發動機的關鍵技術問題。

Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows 本文通過數值模擬得到了超燃沖壓發動機燃燒室化學反應流流場的流動結構。

Numerical simulation of gas - solid two - phase flows in a swirling - flow combustor through the use of a modified k - - kp two - fluid model 雙流體模型用于模擬旋流突擴燃燒室內氣固兩相流動

It is shown that results of study are useful for the optimum design of an annular combustor with the swirler cup 表明本文的研究結果可為發動機環形燃燒室設計提供有用的依據。