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检索条件"机构=Aviation Key Laboratory of Science and Technology on Aero-Engine Altitude Simulation"
27 条 记 录,以下是11-20 订阅
排序:
Intention Estimation of Adversarial Spatial Target Based on Fuzzy Inference
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Intelligent Automation & Soft Computing 2023年 第3期35卷 3627-3639页
作者: Wenjia Xiang Xiaoyu Li Zirui He Chenjing Su Wangchi Cheng Chao Lu Shan Yang School of Information and Software Engineering University of Electronic Science and Technology of ChinaChengdu610054China Institute of Logistics Science and Technology Beijing100166China Science and Technology on Altitude Simulation Laboratory Sichuan Gas Turbine Establishment Aero Engine Corporation of ChinaMianyang621000China Department of Chemistry Physics and Atmospheric SciencesJackson State UniversityJacksonMS 39217USA
Estimating the intention of space objects plays an important role in air-craft design,aviation safety,military and otherfields,and is an important refer-ence basis for air situation analysis and command *** paper studi... 详细信息
来源: 评论
CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL  32
CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF...
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32nd Congress of the International Council of the aeronautical sciences, ICAS 2021
作者: Su, Jinyou Tang, Zhili Tian, Jinhu Pan, Biao Luo, Shaojun Key Laboratory of Unsteady Aerodynamics and Flow Control Ministry of Industry and Information Technology Nanjing University of Aeronautics and Astronautics Nanjing210016 China Science and Technology on Altitude Simulation Laboratory Sichuan Gas Turbine Establishment Aero Engine Corporation of China Sichuan Mianyang621000 China
In order to study the test requirements of vectoring nozzle aeroengine in high altitude simulation test bed, and the matching between the vectoring nozzle and the exhaust ejector of the test bed in the supersonic work... 详细信息
来源: 评论
Neural Machine Translation by Fusing key Information of Text
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Computers, Materials & Continua 2023年 第2期74卷 2803-2815页
作者: Shijie Hu Xiaoyu Li Jiayu Bai Hang Lei Weizhong Qian Sunqiang Hu Cong Zhang Akpatsa Samuel Kofi Qian Qiu Yong Zhou Shan Yang School of Information and Software Engineering University of Electronic Science and Technology of ChinaChengdu610054China Science and Technology on Altitude Simulation Laboratory Sichuan Gas Turbine Establishment Aero Engine Corporation of ChinaMianyang621000China School of Power and Energy Northwestern Polytechnical UniversityXi’an710072China School of Computer Science Southwest Petroleum UniversityChengdu610500China Department of Chemistry Physics and Atmospheric SciencesJackson State UniversityJacksonMS 39217USA
When the Transformer proposed by Google in 2017,it was first used for machine translation tasks and achieved the state of the art at that *** the current neural machine translation model can generate high quality tran... 详细信息
来源: 评论
A Model Average Algorithm for Housing Price Forecast with Evaluation Interpretation
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Journal of Quantum Computing 2022年 第3期4卷 147-163页
作者: Jintao Fu Yong Zhou Qian Qiu Guangwei Xu Neng Wan School of Computer Science Southwest Petroleum UniversityChengdu610500China Key Laboratory on Aero-Engine Altitude Simulation Technology Sichuan Gas Turbine EstablishmentAECCMianyang621000China Aero Engine Academy of China Aero Engine Corporation of ChinaBeijing101300China
In the field of computer research,the increase of data in result of societal progress has been remarkable,and the management of this data and the analysis of linked businesses have grown in *** are numerous practical ... 详细信息
来源: 评论
Arrangement of signal measuring points of planetary gear transmission based on dynamics simulation  15
Arrangement of signal measuring points of planetary gear tra...
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15th IEEE Global Reliability and Prognostics and Health Management Conference, PHM-Beijing 2024
作者: Yang, Weixin Liu, Feichun Xin, Tang Zhu, Rupeng AECC Hunan Aviation Powerplant Research Institute Zhuzhou China Aero-engine vibration technology in Aeronautical Science Key Laboratory Zhuzhou China Nanjing University of Aeronautics and Astronautics Nanjing China
Planetary gear box has complex structure and high failure rate. How to effectively reveal the fault characteristics of the key components in the planetary gear box and find and solve the fault in time is the focus and... 详细信息
来源: 评论
Investigation of tip-leakage-vortex breakdown and its role in rotating stall in a 1.5-stage low-speed axial-compressor  16
Investigation of tip-leakage-vortex breakdown and its role i...
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16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016
作者: He, Xiang Ma, Hongwei Wei, Wei National Key Laboratory of Science and Technology Aero-Engines Collaborative Innovation Center of Advanced Aero-Engine School of Energy and Power Engineering Beihang University Beijing100191 China China Aviation Powerplant Research Institute Zhuzhou412002 China
A whole-annulus unsteady numerical simulation is carried out to investigate the mechanism of the rotating stall in a 1.5-stage low-speed axial-compressor. By comparing the experimental and numerical results, the numer... 详细信息
来源: 评论
aerodynamic design of three-stage vaneless counter-rotating turbine
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航空动力学报 2014年 第7期29卷 1667-1679页
作者: ZHOU Kun LIU Huo-xing ZOU Zheng-ping WANG Lei National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beijing University of Aeronautics and Astronautics Beijing 100191 China Turbine Division Shenyang Engine Design and Research Institute Aviation Industry Corporation of China Shenyang 110015 China
An aerodynamic design criterion was discussed for the 1+3/2 counter-rotating turbine by analyzing the velocity *** are 8 key aerodynamic parameters in the criterion,based on the consideration of aerodynamic efficiency... 详细信息
来源: 评论
Quantitative study of high-frequency fatigue hole-edge stresses in nickel-based single-crystal superalloy  2
Quantitative study of high-frequency fatigue hole-edge stres...
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2nd International Conference on Frontier Materials, ICFM 2023
作者: Li, Leyu Li, Zheng Liu, Jiabin Zhang, Jingang Deng, Zhiwei Li, Quanwei Liu, Xinling AECC Beijing Institute of Aeronautical Materials China AVIC Failure Analysis Center China Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation China Key Laboratory of Aeronautical Materials Testing and Evaluation Aero Engine Corporation of China China Aviation Key Laboratory of Science and Technology on Materials Testing and Evaluation China
In this paper, the influence of air film holes on the stress distribution of nickel-based single-crystal superalloy blades is investigated, a simulated test piece is designed for the analysis and test of the stress di... 详细信息
来源: 评论
A Multi-Feature Fusion Method for Fault Diagnosis with Applications in Tail Paddle Lever Bearing  15
A Multi-Feature Fusion Method for Fault Diagnosis with Appli...
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15th IEEE Global Reliability and Prognostics and Health Management Conference, PHM-Beijing 2024
作者: Long, Zhou Gan, Hao Yang, Weixin Li, Kai Li, Xiuwen AECC Hunan Aviation Power Plant Research Institute Aero-engine Vibration Technology in Aeronautical Science Key Laboratory Zhuzhou China TangZhi Science & Technology Hunan Development Co.Ltd. Changsha China BeiJing TangZhi Technology Development Co. Ltd. Beijing China
Aiming at the problems such as difficult monitoring and inaccurate state evaluation of helicopter tail rotor rod bearing. In this paper, temperature and vibration sensors are used to collect the temperature and vibrat... 详细信息
来源: 评论
aerodynamic modeling and transient performance improvement of a free jet altitude test facility  6th
Aerodynamic modeling and transient performance improvement o...
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6th International Conference on Artificial Intelligence and Security,ICAIS 2020
作者: Wu, Feng Gao, Limin Wu, Xinyun Feng, Xudong Leng, Lintao Li, Yaoyu School of Power and Energy Northwestern Polytechnical University Xi’an710072 China The National Key Laboratory of Aerodynamic Design and Research Xi’an710129 China School of Information and Software Engineering University of Electronic Science and Technology of China Chengdu610054 China Key Laboratory of Science and Technology on Aero-Eigine Altitude Simulation AECC Sichuan Gas Turbine Establishment Chengdu610000 China
An inlet-engine altitude test facility for flight condition simulation is modeled for the system dynamic performance improvement. The system model equations are solved with an improved Euler integral method. To simula... 详细信息
来源: 评论