渦輪機室 的英文怎麼說

中文拼音 [guōlúnshì]
渦輪機室 英文
turbine house
  • : 渦名詞1. (漩渦) eddy; whirlpool; vortex 2. (酒窩) dimple
  • : Ⅰ名1 (輪子) wheel 2 (像輪子的東西) wheel like object; ring; disc 3 (輪船) steamer; steamboa...
  • : machineengine
  • 渦輪機 : aeroturbine
  • 渦輪 : [機械工程] turbine; worm wheel渦輪泵 [航空] turbopump; roturbo; 渦輪發動機 turbine engine; 渦輪風...
  1. Washed air purifier working principle : siphon and using centrifugal principle will be mixed in water pure plant essential oils inhaled through its siphon principle the motor base coaxial centrifugal turbines in the bottom of straw through exchanges cover a very high - speed rotary motor, reuse centrifugal principle, will be mixed in water pure plant essential oil spray bottle in the form within a water film bile, the dust in the air and inhaled bacteria in water purification at the same time after the indoor air insufflation, quickly and efficiently by removing indoor toxin biological, dust, cigarette smoke, the smell, virus

    水洗空氣清新工作原理:是利用虹吸以及離心原理;將混合於水的純植物精油通過虹吸原理吸入其電底座的同軸離心下部的吸管中,通過交流罩極電高速旋轉,再利用離心原理,將混合於水的純植物精油噴在瓶膽內形成一層水膜,將空氣中的灰塵以及細菌吸入水中,同時將經過凈化的空氣吹入內,快速有效地去除內的有毒素生物、灰塵、煙味、臭味、病毒等。
  2. 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器部件,例如運載火箭發動的推力轉子、人造衛星的鈦導管、姿控發動噴注器和波導器件、載人飛船的反射器、導管和蜂窩壁板、航天飛的主發動噴管和預燃以及空間站的管路系統等的廣泛應用情況。
  3. Based on detailed analyze on turbine engine and ramjet, a new conceptive internal - rotor burnt rotating ramjet ( irbrr ) with an rotating cylinder in the center of rotor in which the revolved stream can be ram - compressed and burnt has been proposed and some primary research have been done as below : the scheme of structure, principles, thermodynamic cycle and performances of the new conceptive engine has been studied in the paper

    本文通過對燃氣發動和航空沖壓發動的原理結構進行詳細分析並進行融合創新,提出了一種利用內置旋轉汽缸進行旋轉氣流沖壓壓縮和旋流燃燒的新概念內置燃燒旋轉沖壓發動,並進行了一些前期的基礎性探索研究,具體研究內容有:對旋轉沖壓發動進行了總體方案設計、工作原理分析、氣動熱力循環和性能分析等概念性研究。
  4. The precondition of establishing mathematics model of torpedo turbine system in design condition is to fulfill the external conditions ( such as torpedo sailing speed and depth etc. ) and inner conditions ( such as turbine power and efficiency etc. ). after establishing mathematics model of torpedo turbine system in design condition, we compiled simulation program to compute all kinds of inner parameters of turbine engine include engine type, principal layout of turbine, inner structure of turbine and state parameters of gases

    首先分析設計工況時動力系統,在滿足魚雷動力系統的各項外部條件(如魚雷航深、航速等)和內部條件(如功率、效率,燃燒壓力、溫度,轉子械強度等)的前提下,建立起設計工況發動的數學模型,編程計算並確定內部械結構和燃氣熱力學狀態各參數。
  5. And the finite element method ( fem ) was used to simulate the stress and deformation of the outer casing and the bearing chock. on the basis of the experiments and fem analysis, the strength and fatigue lifetime, the interaction of creep and fatigue lifetime, the creep lifetime of outer casing and bearing chock have been analyzed, at the end of trail, sem analyses of failure section has been conducted

    同時對航空發動燃氣匣和軸承座進行了有限元模擬計算,得到外匣和軸承座的焊接處的強度和變形情況的模擬結果。根據試驗數據和有限元的計算結果,對發動燃燒匣和軸承座兩種結構(包含焊縫)進行靜強度分析、疲勞壽命分析、蠕變壽命分析、蠕變疲勞交互作用壽命分析以及斷口的金相分析。
  6. Port engines ingested some foreign matter during take - off roll, fan blades severely damaged, we abandoned taxing back to terminal

    起飛滑跑中左發進氣口吸入異物, ()風扇葉片損壞,中斷起飛,滑到候
  7. To meet the needs for wider surge margin of the turbofan engine, a new model was developed to predict the characteristics of the fan / high pressure compressor and turbine in this thesis. several ways, including, variable inlet guide vanes of the fan, variable guide vanes of the high pressure compressor, the variable inlet area ratio of the mixer and the nozzle areas, were presented to enlarge the surge margin of the turbofan engine. meanwhile, a method of combined variable geometries for optimizing controls of inlet guide vanes of the fan, guide vanes and the first two stators of high pressure compressor, area ratio of mixer and noz zle areas was established

    為了滿足下一代作戰飛對推進系統的性能和穩定性要求,本文建立了壓縮系統特性和特性的新模型,並分別採用改變扇發動風扇進口導流葉片、壓氣導流葉片和前兩級靜葉片、混合進口處內、外涵面積比和尾噴管面積,研究了其對發動性能和穩定性的影響,進而得出了扇發動變幾何擴穩的方法,為發動變幾何擴穩研究打下理論基礎。
  8. Some experimental wind turbines have incorporated an added structural design feature, known as augmenters

    一些試驗性的發電增加了一些結構設施,即加速
  9. This machine consists of bin, vibration chamber, coupling and motor. the vibration chamber is made up of eccentric wheel. rubber soft piece, main shaft and bearing. the adjustable eccentric hammering is transmitted to the centerline of main shaft by motor drive, and produce centrifugal force at unsteady state so as to change the strength of material and form vortex in the sieve. weghted regulator and amplitude can be adjusted as per different material and sieve mesh

    由料斗、振蕩、聯軸器、電組成,振蕩電腦內由偏心、橡膠軟體、主軸、軸承組成,可調節的偏心重錘經馬達驅動傳到主軸中心線,在不平衡狀態下,產生離心力,使物料強度改變在篩內形成漩,重錘調節器和振幅大小可根據不同物料和篩網進行調節。
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