火焰筒的英文

发音:

"火焰筒"怎么读用"火焰筒"造句

英文翻译手机版

burner inner liner
burner liner
burner-can
combustion liner/combustor can/combustor basket/flame tube
combustor liner
flame tube

"火焰"英文翻译 flame; blaze
"筒"英文翻译 a section of thick bamboo
"火焰筒火管炉胆" 英文翻译 : flametube
"火焰筒颈" 英文翻译 : flame tube cover
"同心火焰筒" 英文翻译 : concentric liners
"燃烧室火焰筒" 英文翻译 : burner basket; combustion-system flame tube
"直流式火焰筒" 英文翻译 : straight-flow flame tube
"火焰筒气膜冷却" 英文翻译 : flame-gouging torch
"内环腔火焰筒壁" 英文翻译 : inner burner shroud
"外环腔火焰筒壁" 英文翻译 : outer burner shroud
"八个火焰筒的环形燃烧室" 英文翻译 : eight-unit-can-annular combustion chamber
"八个火焰筒的燃烧室" 英文翻译 : eight-can combustor
"隔焰屏；消焰筒" 英文翻译 : flame arrestor
"火焰" 英文翻译 : [化学] flame; blaze
"bakersfield火焰" 英文翻译 : california league
"靶火焰" 英文翻译 : target plume
"扁火焰" 英文翻译 : flat flame
"单火焰" 英文翻译 : single flame
"点火焰" 英文翻译 : pilot light
"发火焰" 英文翻译 : flame
"非火焰" 英文翻译 : nonflame
"横火焰" 英文翻译 : cross flame
"花火焰" 英文翻译 : flame var
"回闪(火焰)" 英文翻译 : flash back
"火焰(救生)" 英文翻译 : flare-ulight

例句与用法

The combustor of gas turbine engine operates under inhomogeneous high temperature , which causes very complicated mechanical behavior of combustor ' s material , and makes combustor failure
燃气涡轮发动机火焰筒在非均匀温度场的作用下，材料会呈现复杂的力学行为，导致使用过程中出现裂纹而造成故障。
In order to study the influence of dimensional configuration of the film cooling hole on the discharge coefficient , some kinds of film cooling holes with different dimensional configuration were designed
摘要为了研究火焰筒壁面气膜冷却孔几何结构对流量系数的影响规律，设计了几种具有不同几何尺寸和排列结构的气膜冷却孔实验件。
In this thesis , in order to search the condition and reason of failure for a combustor , thermal stress was analyzed in steady and transient temperature field . according to the investigation , three conclusions are obtained
在忽略瞬态升温过程得到的稳态温度场作用下，火焰筒的热应力不足以导致裂纹萌生，所以仅进行稳态分析不能得到合理的结论。
On the contrary , if temperature gradient is relatively low , combustor only undergo low compressive stress at high temperature . the combustor of engine has a longer life length . these results can provide some reference for maintain and design for gas turbine combustor
分析也表明，若在起动过程中筒壁的温度梯度较为平缓，火焰筒的气膜唇边在起动完成后始终受微小的压应力作用，火焰筒的寿命可以大大延长。
Jet impingement cooling is an advantage method in heat transfer enhancement owing to its extremely high local heat transfer coefficient and simple structure . as regard as the combustor flame tube cooling structure is concerned , the impingement - converse convection - film composite cooling is an effective method , in this composite cooling structure , the impingement cooling problem could be modeled as impingement inside semi - confined channel
对于冲击-逆向对流-气膜复合冷却的火焰筒结构而言,火焰筒壁面冷气侧的冲击冷却实质上是半封闭通道的冲击冷却,即冲击射流从冲击孔板喷出,冲击到换热靶面后形成壁面射流沿通道单方向流出。
Flame tube in aircraft engine undergoes high temperature and high speed airflow washing . a hypothesis was suggested , which takes the transient heat transferring as the main reason to the cracking and damage on flame tube . finite element method was adopted to simulate the thermal fatigue and the hypothesis was reproduced
发动机火焰筒的热疲劳损伤是导致火焰筒失效的主要原因，本文提出了一种火焰筒热疲劳损伤假设，认为火焰筒热疲劳损伤不是由于发动机的运行和停车时冷热温度循环造成的，而是发动机启动时瞬态温度传导过程中材料循环塑性变形的结果，利用该假设结合有限元计算模拟了火焰筒产生疲劳损伤的原因。
The combustor do n ' t fail if transient rise of temperature field is neglected , the stress field of combustor can n ' t cause gas film wall rupture . 2 . combustor ' s creep and relaxation is calculated in steady temperature field , the results show that creep and relaxation is not main reason destroying combustor chamber
对稳态温度场下的蠕变松弛计算表明，高温下的蠕变松弛促使火焰筒的热应力下降，在所考虑的条件下稳态温度场导致火焰筒的蠕变变形不是火焰筒破坏的主要原因。
If there are high temperature gradient between cool liner and hot liner , compressive plastic strain appear at that transient time , which lead to gas film wall bearing high tensile stress at high temperature . high tensile stress is one of main reasons which destroy combustor
分析表明，起动过程中由于热传导滞后引发的温度梯度可以导致火焰筒气膜唇边在起动瞬间发生较大的压缩塑性应变，进而使得该区域在工作时承受较高水平的拉伸应力，高的拉应力会导致火焰筒萌生裂纹。