aeroengine,英語單詞,主要用作名詞,作名詞時譯為“[航] 航空發動機;飛機引擎”。
基本介紹
- 外文名:aeroengine
- 詞性:名詞
- 釋義:[航] 航空發動機;飛機引擎
- 屬性:英語單詞

aeroengine,英語單詞,主要用作名詞,作名詞時譯為“[航] 航空發動機;飛機引擎”。
aeropulse,英語單詞,主要用作名詞,作名詞時譯為“脈動式噴射引擎”。短語搭配 aeropulse e 引擎 aeropulse engine 脈動式噴氣發動機 aeropulse e engine 脈動式噴氣發動機 ; 脈衝式噴氣發動機 單詞釋義 脈動式噴氣發動機 ...aeroplane飛機aeropulse脈動式噴氣發動機aeropulverizer噴磨機...引擎 ...aeropolitics國際航空...
中國航空發動機集團有限公司(簡稱:中國航發,英文:Aero Engine Corporation of China,英文縮寫:AECC)是中央直接管理的國有特大型企業,由國資委、北京國有資本經營管理中心、中國航空工業集團有限公司、中國商用飛機有限責任公司共同出資組建。2016年5月31日,中國航空發動機集團公司在北京市完成工商註冊,標誌著該公司...
4.2 Aeroengine system 4.2.1 Piston engines 4.2.2 Turbojet engines & turbofan engines 4.2.3 Turboprop engines & turboshaft engines 4.2.4 Ram-engines 4.3 Rocket engine system 4.3.1 Main performance parameters 4.3.2 Solid Rocket propulsion system 4.3.3 Liquid rocket propulsion system 4...
Aeroengine Active Stability Control[C].The 37Th Chinese Control Conference.2018.7 Wuhan, China 53. San-mai SU,Yong-qin CHEN.Exploration and Practice of MCU Course Teaching Methods in New Media Environment[C].The 3rd International Conference on Social, Education and Management Engineering (SEME2017...
Fenzhu Ji,Yangping Bao,Yu Zhou*.Investigation on Performance and Implementation of Tesla Turbine in Engine Waste Heat Recovery:Energy Conversion and Management,2019,179:326-338 Shuiting Ding,Guo Li,Yu Zhou*.Probabilistic failure risk assessment for aeroengine disks considering a transient process:...
[16] Matching synchrosqueezing wavelet transform and application to aeroengine vibration monitoring.Shibin Wang, Xuefeng Chen, Chaowei Tong, Zhibin Zhao.IEEE Transactions on Instrumentation and Measurement, 66(2), 360-372, 2017.[15] Nonlinear squeezing time-frequency transform and application in rotor ...
Hu XiaoAn; Zhang Qiang; Yang Xiao Guang; Shi Duo Qi*; Viscoplastic analysis method of an aeroengine turbine blade subjected to transient thermo-mechanical loading , International Journal of Mechanical Sciences, 2019, 152: 247-256.Li, Shaolin; Wang, Bingxue; Shi, Duoqi*; Yang, Xiaoguang*; ...
Foreign technology demonstration in aeroengine development is briefly introduced in this paper 定義 是指經過生產套用試驗與考核,證明技術的先進性、適用性和安全性,為技術推廣套用提供依據和信息的活動。技術驗證工作應當因地制宜,兼顧經濟效益、社會效益和生態效益,做到科學、規範、公正、公開,實行誰推廣、誰...
安道琳編著的論著有《Prediction of combustion noise for an aeroengine combustor》《A six sensor method for measuring acoustic properties in ducts》《Aeroacoustic source measurement methods for characterizing the sound generated by ducted flow devices with higher-order modes》《Combustion rumble prediction ...
航空燃油柱塞泵運動學與動力學特性分析研究,陳永琴著。副題名 外文題名 Research and analysis for aeroengine fuel piston pump kinematics and dynamic characteristic 論文作者 陳永琴著 導師 陳建軍指導 學科專業 學位級別 工學博士 學位授予單位 西安電子科技大學 學位授予時間 2011 關鍵字 航空發動機 燃油泵 機械...
渦扇發動機分路式多變數PI解耦控制,航空動力學報,2008.5 [6] 航空發動機燃油柱塞泵計算機輔助設計方法,計算機仿真,2012.3 [7] Global convergence iterative learning controller design for aeroengine nozzle actuating system,ICECC,2011.9 [8] 一種採用徑向串聯方式的組合旋渦泵設計方法,推進技術,2013.2 ...
Zepeng Li, Yanan Wang*, Baijie Qiao, Bi Wen, Xuefeng Chen. Experimental Investigation of Aeroelastic Instabilities in an Aeroengine Fan: Using Acoustic Measurements[J]. Aerospace Science and Technology, 2022. 130, 107927.Yuda Zhu, Yanan Wang*, Baijie Qiao, Shunguo Fu, Mei Liu, Xianqiang ...
[9] C.N. Wong, H. Huang, J. Xiong and T. Hu, Weibull Distributed Stress-Dependent Strength Analysis of Aeroengine Alloy using Lagrange Factor Polynomial, Proceedings of the ASME 2010 IDETC/CIE, DETC2010-28090, August 2010.[10] C.N. Wong, J. Xiong, H. Huang and T. Hu, Damage ...
[19] Jiang, RS, Zhang DH, Wang WH. An integration system for investment casting mould design of aeroengine turbine blade. CHINA FOUNDRY, 2008,2(5)獲獎情況 主持完成的“空心渦輪葉片精鑄模具CAD/CAM系統”,榮獲1999年部級科技進步一等獎。作為骨幹成員參與完成的“航空發動機整體葉盤高效精密數位化冷...
[11] Jiang RS*, Zhang DH, Wang WH, et al. An integration system for investment casting mould design of aeroengine turbine blade [J]. CHINA FOUNDRY, 2008, 5(2): 114-118. (SCI: 000256945200008)[12] 蔣睿嵩*, 張定華, 汪文虎, 董一巍. 航空發動機渦輪葉片精鑄模具集成設計系統[J]. 鑄造, ...
China's Multidisciplinary Design Optimization Accepting the Challenge of Aeroengine Development Development of Helicopter Power Transmission System Technology 基於試驗設計及支持向量機的向心葉輪結構最佳化設計方法研究 輪盤概念設計中拓撲和形狀同時最佳化方法研究 Multidisciplinary Design Optimization Technology Accepting ...
IsoehermalForgingoftheTc6-TitaniamAlloyTailrodfarAeroengine 航空發動機TC6鈦合金管接頭的等溫鍛造 IsothermalForgingoftheTc6TitaniumAlloyTubeUnionforAeroengines 一種寬頻帶綜合交流磁參數測試儀 ASyntheticalwideFrequencyBandTesterforA.C.MagneticParameters X射線螢光光譜分析中理論α係數法與經驗係數法的比較研究 A...
1.The UK Technology Strategy Board, Tool-less Manufacture of Aeroengine Turbine Components (Rolls-Royce Fast Make Program), 12/2013-05/2016, 主要參與。2.The UK Technology Strategy Board, Sustainable and Resource Efficient Cutting of Titanium Alloys, 01/2013-04/2016, 主要參與。3.湖南大學“青年...
Low cycle multiaxial fatigue failure is the main failure mode of aeroengine compressor disk.低循環多軸疲勞失效是航空發動機低壓壓氣機輪盤的主要失效形式。Experimental study on multiaxial failure criterion of concrete before and after wet-screened is just at the initial stages.混凝土濕篩前後的多軸破壞...
[1] Yang Hai-Sheng, Chen Guo-Ding, Deng Si-Er,et al. Rigid-flexible couple dynamic simulation of aeroengine main-shaft cylindrical roller bearing[C]. ChengDu: IEEE Computer Society. 2010: 431-435(EI收錄號:20104613374067)[2] Yang Hai-Sheng, Chen Guo-Ding, Deng Si-Er,et al. Dynamic ...
24. New method for the measurement of aeroengine blade edge.Guodong Liu; Zhaobang Pu; Zuo Zhang; Yunbin Sun. SPIE,Vol.4929 ,2002.10,國際會議。專利 1.用於空間物體三維檢測與定位的光電式自準直顯微測量儀,國家發明專利,ZL 2007 1 0071972.X 1。2.束靶耦合感測器,國家發明專利,ZL 2008 1 ...
