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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:
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
Health Assessment of Split Torque Transmission System Using Improved Generative Adversarial Networks
Health Assessment of Split Torque Transmission System Using ...
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TEPEN International Workshop on Fault Diagnostics and Prognostics, TEPEN-IWFDP 2024
作者: Wang, Zhi Hu, Niaoqing Xu, Fujian Yang, Yi Hu, Lei Laboratory of Science and Technology on Integrated Logistics Support NUDT Changsha410073 China Beijing Tangzhi Technology Development Co. LTD Beijing100043 China AECC Hunan Aviation Powerplant Research Institute Zhuzhou412002 China Aero-Engine Vibration Technology in Aeronautical Science Key Laboratory Zhuzhou412002 China Hunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment Hunan University of Science and Technology Xiangtan411201 China
Split-torque transmission system (STTS) is a new type of helicopter main rotor transmission. It has the characteristics of light quality, fewer transmission stages, high transmission efficiency, high reliability, low ... 详细信息
来源: 评论
RUL Prediction of Split Torque Transmission System Using Particle Filtering and Degenerate Model
RUL Prediction of Split Torque Transmission System Using Par...
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TEPEN International Workshop on Fault Diagnostics and Prognostics, TEPEN-IWFDP 2024
作者: Yang, Weixin Wang, Zhi Tang, Xin Hu, Lei Xu, Yuandong AECC Hunan Aviation Powerplant Research Institute Zhuzhou412002 China Aero-Engine Vibration Technology in Aeronautical Science Key Laboratory Zhuzhou412002 China Laboratory of Science and Technology on Integrated Logistics Support NUDT Changsha410073 China Beijing Tangzhi Technology Development Co. LTD. Beijing100043 China Hunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment Hunan University of Science and Technology Xiangtan411201 China
The split-torque transmission system (STTS) is considered to be the most likely alternative to a planetary gearbox for helicopter main rotor transmissions. SSTS has obvious advantages in reliability, weight, decelerat... 详细信息
来源: 评论
Film cooling effectiveness in the presence of internal hole random roughness: A comprehensive analysis
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International Communications in Heat and Mass Transfer 2025年 165卷
作者: Wang, Xinyu Ye, Lin Li, Wei Zheng, Tianyi Liang, Xiyuan Liu, Cunliang School of Power and Energy Northwestern Polytechnical University Shaanxi Xi'an710129 China State Key Laboratory for Strength and Vibration of Mechanical Structures Xi'an Jiaotong University Shaanxi Xi'an710049 China Science and Technology on Altitude Simulation Laboratory Sichuan Mianyang621000 China Hunan Aviation Powerplant Research Institute Aero Engine Corporation of China Hunan Zhuzhou412002 China
Film cooling, with its excellent cooling performance, is widely applied in the active thermal protection design of aerospace propulsion systems. However, during manufacturing and service, film holes are affected by dr... 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
Arrangement of Signal Measuring Points of Planetary Gear Tra...
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Prognostics and System Health Management Conference (PHM-Qingdao)
作者: Weixin Yang Feichun Liu Tang Xin Rupeng Zhu 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
Fractional Order Modeling of Dynamic Response for Shielded Total Temperature Probes Considering Unsteady aerothermal Processes
SSRN
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SSRN 2024年
作者: Li, Zhen Zhang, Weihao He, Tingyu Yang, Weiping School of Energy and Power Engineering Beihang University Beijing100191 China National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics Beijing100191 China Hunan Aviation Powerplant Research Institute Zhuzhou412002 China
In this paper, unsteady conjugate heat transfer simulation with radiation model was employed to analyze the gas flow, heat transfer characteristics inside and outside the typical shielded total temperature probe. It w... 详细信息
来源: 评论
μ-Synthesis-based robust L1 adaptive control for aeropropulsion system test facility
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aerospace science and technology 2023年 第1期140卷
作者: Liu, Jiashuai Wang, Xi Liu, Xi Zhu, Meiyin Pei, Xitong Dan, Zhihong Zhang, Song School of Energy and Power Engineering Beihang University Beijing100191 China Zhongfa Aviation Institute Beihang University Hangzhou311115 China Research Institute of Aero-Engine Beihang University Beijing100191 China Science and Technology on Altitude Simulation Laboratory AECC Sichuan Gas Turbine Establishment Mianyang621703 China
For aeropropulsion System Test Facility (ASTF) applied in aero-engine performance testing, it is critical to accurately control the pressure and temperature of the airflow to simulate the flight environment. This arti... 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
A Multi-Feature Fusion Method for Fault Diagnosis with Applications in Tail Paddle Lever Bearing
A Multi-Feature Fusion Method for Fault Diagnosis with Appli...
收藏 引用
Prognostics and System Health Management Conference (PHM-Qingdao)
作者: Zhou Long Hao Gan Weixin Yang Kai Li Xiuwen Li 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