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检索条件"机构=Aviation Key Laboratory ofScience and Technology on Life-support Technology"
55 条 记 录,以下是41-50 订阅
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Numerical simulation and experimental research of shear-driven water film on flat plate
Numerical simulation and experimental research of shear-driv...
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CSAA/IET International Conference on Aircraft Utility Systems (AUS 2024)
作者: Qinyang Li Ning Guan Bo Ning Guangya Zhu Dalin Zhang Weijian Chen Key Laboratory of Aircraft Environment Control and Life Support MIIT Nanjing University of Aeronautics and Astronautics Nanjing People's Republic of China College of Aeronautics Shandong Jiaotong University No.5001 Haitang Road Changqing University Science and Technology Park Jinan People's Republic of China Utility System Design and Research Department Jiangxi Hongdu Aviation Industry Group Company Ltd. Nanchang People's Republic of China
The supercooled water droplets in the air will form a water film on the aircraft during flight, which will then form icing, which will have an impact on the aerodynamic performance of the aircraft and even endanger th...
来源: 评论
Research on measurement method of six degree of freedom for head based on safetr of aircraft pilot seat
Research on measurement method of six degree of freedom for ...
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CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020)
作者: G. Luo Z. Jin W. Xie R. Wang Aviation Key Laboratory of Science and Technology on Life-support Technology Xiangyang Hubei China AVIC Aerospace Life-support Industries Ltd. China
In order to ensure the safety of the pilot's life, the six degree of freedom data of the ATD head need to be obtained through dynamic impact test to evaluate the possibility of head injury in the cockpit. A binocu... 详细信息
来源: 评论
Equivalent study on delethalization test for sled head injury criteria test of civil aircraft passenger seat
Equivalent study on delethalization test for sled head injur...
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CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020)
作者: Z. Jin W. Shen G. Luo M. Li Z. Jia W. Zhou L. Jia L. Zhang Aviation Key Laboratory of Science and Technology on Life-support Technology Xiang yang China Test Department AVIC Aerospace Life-Support Industries LTD No.29 Xinhua road Xiang yang China
The equivalent study between delethalization test and sled HIC test is in order to improve the efficiency of Head Injury Criteria (HIC) test on civil aircraft passenger seats, as well as to reduce the test consumption... 详细信息
来源: 评论
Simulation study on dynamic opening characteristics of airplane drag chute under the condition of stable crosswind
Simulation study on dynamic opening characteristics of airpl...
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CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020)
作者: L. Jin P. Yang X. Hu H. Li L. Zhang D. Cui Aviation Key Laboratory of Science and Technology on Life-support Technology Xianyang China AVIC The First Aircraft Institute Institute of mechanical and electrical system Xi’an China
In this paper, the ALE fluid-solid coupling algorithm is used to realize the simulation of the dynamic opening process of a certain type of airplane drag parachute. Based on the drag parachute working principle and fo... 详细信息
来源: 评论
Reliability Analysis of Certain Rocket Engine Based on Fault Tree  4
Reliability Analysis of Certain Rocket Engine Based on Fault...
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4th International Conference on Manufacturing, Material and Metallurgical Engineering, ICMMME 2019
作者: Wang, Wensheng Jin, Liying Sun, Xi Liu, Jing Aviation Key Laboratory Science and Technology on Life-Support Technology Xiangyang Hubei441003 China School of Mechanical Engineering Xi'an Jiaotong University Shaanxi Xi'an714200 China Aerospace Life-Support Industries Ltd. Xiangyang Hubei441003 China
In this paper, a fault tree model of certain rocket engine is established according to its structure and working principle. Through qualitative analysis and quantitative calculation, the factors affecting the reliabil... 详细信息
来源: 评论
Reliability Analysis of Certain Rocket Engine Based on Fault Tree
Reliability Analysis of Certain Rocket Engine Based on Fault...
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作者: Wensheng Wang Liying Jin Xi Sun Jing Liu Aviation Key Laboratory Science and Technology on Life-Support Technology Aerospace Life-Support Industries Ltd. School of Mechanical Engineering Xi'an Jiaotong University
In this paper, a fault tree model of certain rocket engine is established according to its structure and working principle. Through qualitative analysis and quantitative calculation, the factors affecting the reliabil...
来源: 评论
Numerical investigation of influence of structure and operating parameters on performance of vortex oil filter
Numerical investigation of influence of structure and operat...
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CSAA/IET International Conference on Aircraft Utility Systems, AUS 2018
作者: Wang, Ning Chen, Weijian Ning, Guoli Hui, Ma Key Laboratory of Aircraft Environment Control and Life Support MIIT Nanjing University of Aeronautics and Astronautics Nanjing China Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing China
In this paper, the three-dimensional numerical simulation of solid-liquid two-phase flow in a vortex oil filter is performed by means of numerical simulation. The Reynolds stress turbulence model is used in the simula... 详细信息
来源: 评论
Preparation of biodegradable PLA/PCL composite filaments: effect of PLA content on strength
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IOP Conference Series: Materials Science and Engineering 2020年 第1期770卷
作者: H M Qiu K W Hou J P Zhou W J Liu J B Wen Q F Gu School of Material Science and Engineering Nanchang Hangkong University Nanchang 330063 China Aviation Key Laboratory of Science and Technology on Life-Support Technology Xiangyang 441000 China
As one of the predominant 3D additive manufacturing technology, fused deposition modeling (FDM) suffers from the rich printable filaments. The goal of this paper is to produce a fully biodegradable polymeric composite...
来源: 评论
Simultaneously static and dynamic layout designs of stiffening structures
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IOP Conference Series: Materials Science and Engineering 2020年 第1期892卷
作者: Zhijie Feng Kai Wu Xuan Liang Jianbin Du AVIC Aerospace Life-Support Industries LTD Aviation Key Laboratory of Science and Technology on Life-Support Technology Xiangyang 441000 P.R. China School of Aerospace Engineering Tsinghua University Beijing 100084 P.R. China
In the present paper, the topological design problem of lightweight stiffening structures are studied. Multiple design criteria like static compliance, dynamic compliance, eigenfrequency/eigenfrequency gaps and weight...
来源: 评论
Research on Reliability Assessment Method of Emergency Escape Parachute
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Journal of Physics: Conference Series 2020年 第1期1544卷
作者: Fangyun Ma Huajin Lei Wensheng Wang Jing Liu Liying Jin Aviation Key Laboratory Science and Technology on Life-Support Technology Hubei Xiangyang 441003 China Aerospace Life-Support Industries Ltd. Hubei Xiangyang 441003 China School of Mechanical Engineering Hubei University of Arts and Science Xiangyang 441053 China
Aiming at the problem that emergency escape parachute cannot meet the requirements of the index using the binomial evaluation method, combined with the characteristics of emergency escape parachute products, comprehen...
来源: 评论