航空發動機 的英文怎麼說

中文拼音 [hángkōngdòng]
航空發動機 英文
aerial engine
  • : Ⅰ名詞(船) boat; shipⅡ動詞(航行) navigate (by water or air); sail
  • : 空Ⅰ形容詞(不包含什麼; 裏面沒有東西或沒有內容; 不切實際的) empty; hollow; void Ⅱ名詞1 (天空) s...
  • : 名詞(頭發) hair
  • : machineengine
  • 航空 : aviation; voyage
  1. Failure analysis of stainless pipes in aero - engine

    航空發動機不銹鋼導管失效分析
  2. Optimization of in - flight shutdown rate of aero - engine

    航空發動機中停車率的優化
  3. Research and analysis on material and machining for aerocraft engine gear

    航空發動機齒輪材料及加工精度分析研究
  4. Study of intelligent aeronautic engine temperature - control amplifier testing system

    航空發動機溫控放大器智能測試平臺的研製
  5. High carbon chromium bearing steel for aircraft engine

    航空發動機用高碳鉻軸承鋼
  6. Study on primary combustion zone of aeroengine combustor

    航空發動機燃燒室主燃區特性的研究
  7. General specification for aircraft engine gearbox

    航空發動機減速器通用規范
  8. Jet engines with which most modern high-speed aircrafts are equipped develop thrust on the same principle as the propellers of conventional aero-engines.

    大多數現代高速飛裝備的噴氣產生推力的原理,與普通航空發動機的螺旋槳相同。
  9. Mtu aero engines

    Mtu航空發動機
  10. Specification for aircraft engine nacelle fire extinguisher doors

    航空發動機艙滅火器裝料口規范
  11. Robust controller design and experiment of turbofan

    航空發動機多變量魯棒數字控制器的設計
  12. Study of maps methods for turbofan engine performance seeking control

    方法在航空發動機性能尋優控制中的應用
  13. A component level aerothermodymamic model of a turbofan aeroengine is created in this thesis using oo technology

    本文基於面向對象技術建立了某型雙軸渦扇航空發動機的部件級氣熱力模型。
  14. The application of the adcs can greatly reduce the weight of the control system ; reduce the control system design cost and maintenance costs ; make the design adaptable to new aeroengine types, adaptability to changes in components

    航空發動機採用分散式控制系統能大大降低總體重量;減少研製成本和維護費用;利於控制系統擴展、升級。
  15. A airfoil blade is one of the most important workpiece in aircraft ' s engines. in aircraft ' s engines, it takes the key pole of energy transfer

    葉片是航空發動機中的一種重要零件,它在航空發動機中起著能量轉換的關鍵作用。
  16. It is reported that the mechanical failure accounts for most of the aviation accidents, and among them, the wear faults occupy a considerably large proportion rate. based on the traditional ferro - graph and spectral analysis technology, and with the introduction of computer vision and information fusion technology, this article focus on the study of aviation engine abrasion diagnoses in the fields of debris analysis and information fusion

    據統計,導致飛行事故的主要因素是械故障,其中,磨損類故障又占很大比例,本文就以傳統的鐵譜分析技術和光譜分析技術為基礎,引入計算視覺與信息融合技術,開展基於磨粒分析和信息融合的航空發動機磨損故障診斷技術研究。
  17. At present carbon fiber - reinforced composite is developed to use in some aero - engine components in our country. using the numerical method and fatigue damage theory, the buckling and fatigue on the composite materials and composites case are studied for aero - engine design

    本文從實際工程背景出,利用板殼理論和現代數值分析技術的研究成果,結合疲勞累積損傷理論,對航空發動機用的復合材料及其匣結構的屈曲與疲勞壽命問題開展了較為系統深入的研究。
  18. Design of life usage monitoring system of aeroengine critical part

    航空發動機關鍵件使用壽命監視系統設計
  19. Aero - engine multivariable learning fuzzy decouple control

    航空發動機多變量自學習模糊解耦控制
  20. Results from this thesis concluded that numerical simulation can be applied to study " effect of varying the incident angle of dilution air on the performance of the gas turbine combustor "

    本文針對某種航空發動機火焰管模型結構,採用數值模擬方法對「摻混氣噴射角度對燃燒室性能的影響」這一問題進行了探討。
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