1000-8055
2014 Issue 7
Structure dynamics design method of aero-engine high pressure rotor
LIAO Ming-fu;TAN Da-li;GENG Jian-ming;SONG Ming-bo;L Pin;School of Power and Energy;Northwestern Polytechnical University;Institute of Naval Vessel;Naval Academy of Armament;
LIAO Ming-fu;TAN Da-li;GENG Jian-ming;SONG Ming-bo;L Pin;School of Power and Energy;Northwestern Polytechnical University;Institute of Naval Vessel;Naval Academy of Armament;
..............page:1505-1519
Numerical simulation of effect of high temperature oxidation on stress field distribution of EB-PVD thermal barrier coating
HAO Yong;QI Hong-yu;MA Li-qiang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;Co-Innovation Center for Advanced Aero-Engine;
HAO Yong;QI Hong-yu;MA Li-qiang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;Co-Innovation Center for Advanced Aero-Engine;
..............page:1520-1526
Imbalance response of rotor system with nonlinear bearing stiffness
MA Yan-hong;HE Tian-yuan;ZHANG Da-yi;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
MA Yan-hong;HE Tian-yuan;ZHANG Da-yi;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1527-1534
Method of fault feature extraction based on EMD sample entropy and LLTSA
XIANG Dan;GE Shuang;School of Automation;Guangdong Polytechnic Normal University;School of Mechanical and Automotive Engineering;South China University of Technology;
XIANG Dan;GE Shuang;School of Automation;Guangdong Polytechnic Normal University;School of Mechanical and Automotive Engineering;South China University of Technology;
..............page:1535-1542
Vibration of bending-torsion coupling gear-rotor-rolling bearing transmission system
LI Chao-feng;ZHOU Shi-hua;LIU Wen-ming;REN Zhao-hui;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;The Turbine Design Institute;Shenyang Blower Works Group Corporation;
LI Chao-feng;ZHOU Shi-hua;LIU Wen-ming;REN Zhao-hui;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;The Turbine Design Institute;Shenyang Blower Works Group Corporation;
..............page:1543-1555
Approach for civil aero-engine repair objective determination based on life limited parts
FU Xu-yun;CHEN Yin;ZHONG Shi-sheng;Department of Mechanical Engineering;Harbin Institute of Technology at Weihai;School of Mechatronics Engineering;Harbin Institute of Technology;
FU Xu-yun;CHEN Yin;ZHONG Shi-sheng;Department of Mechanical Engineering;Harbin Institute of Technology at Weihai;School of Mechatronics Engineering;Harbin Institute of Technology;
..............page:1556-1561
Comparison of bilinear process method and group test method for performance degradation
WANG Zhi-hua;FU Hui-min;HUANG Rong;ZHANG Yong-bo;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
WANG Zhi-hua;FU Hui-min;HUANG Rong;ZHANG Yong-bo;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1562-1566
High-temperature ultra-high cycle fatigue test of TC17 titanium alloy
LI Jiu-kai;LIU Yong-jie;WANG Qing-yuan;HOU Fang;Key Laboratory of Ministry of Education for Energy Engineering Safety and Disaster Mechanics;College of Architecture and Environment;Sichuan University;School of Aeronautics and Astronautics;Sichuan University;
LI Jiu-kai;LIU Yong-jie;WANG Qing-yuan;HOU Fang;Key Laboratory of Ministry of Education for Energy Engineering Safety and Disaster Mechanics;College of Architecture and Environment;Sichuan University;School of Aeronautics and Astronautics;Sichuan University;
..............page:1567-1573
Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method
LU Si-da;GAO Xi-guang;SONG Ying-dong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Department of Power and Propulsion;School of Engineering;Cranfield University;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;
LU Si-da;GAO Xi-guang;SONG Ying-dong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Department of Power and Propulsion;School of Engineering;Cranfield University;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;
..............page:1574-1582
Taguchi method based tolerance design for rotor system dynamics
YANG Jun;ZANG Chao-ping;LIU Yong-quan;WANG Xiao-wei;FENG Guo-quan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
YANG Jun;ZANG Chao-ping;LIU Yong-quan;WANG Xiao-wei;FENG Guo-quan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1583-1590
Experiment on friction and wear performance of textured port plate pair
LI Yang;DENG Hai-shun;WANG Xiao-lei;Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;College of Mechanical Engineering;Anhui University of Science and Technology;
LI Yang;DENG Hai-shun;WANG Xiao-lei;Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;College of Mechanical Engineering;Anhui University of Science and Technology;
..............page:1591-1597
Performance investigation of intercooler operating in wet condition using distributed parameter model
ZHOU Ya-feng;LIU Gui-lin;HAN Ya-hui;YANG Chun-xin;ZHU Zhi-li;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Mechanical Engineering Department;Army Aviation Institute;the Chinese People’s Liberation Army;
ZHOU Ya-feng;LIU Gui-lin;HAN Ya-hui;YANG Chun-xin;ZHU Zhi-li;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Mechanical Engineering Department;Army Aviation Institute;the Chinese People’s Liberation Army;
..............page:1598-1605
Mixing characteristics of hyperburner with a lobed mixer
CHENG Xiao-jun;FAN Yu-xin;CAI Di;WANG Jia-hua;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
CHENG Xiao-jun;FAN Yu-xin;CAI Di;WANG Jia-hua;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1606-1614
Effect of rib orientation on film cooling performance
LUO Jian-xia;ZHU Hui-ren;LIU Cun-liang;JIA Guang-sen;School of Power and Energy;Northwestern Polytechnical University;
LUO Jian-xia;ZHU Hui-ren;LIU Cun-liang;JIA Guang-sen;School of Power and Energy;Northwestern Polytechnical University;
..............page:1615-1622
Modeling and simulation of general fuel tank thermal model
LAN Jiang;ZHU Lei;ZHAO Jing-quan;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
LAN Jiang;ZHU Lei;ZHAO Jing-quan;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1623-1630
Feature-parameter-criterion for predicting lean blowout limit of aero-engine combustor
ZHANG Zhi-bo;ZHENG Hong-tao;LING Rui;College of Power and Energy Engineering;Harbin Engineering University;
ZHANG Zhi-bo;ZHENG Hong-tao;LING Rui;College of Power and Energy Engineering;Harbin Engineering University;
..............page:1631-1638
Influence of improved structure of bluff-body on combustion flow characteristics in advanced vortex combustor
SUN Hai-jun;ZENG Zhuo-xiong;XU Yi-hua;HU Chun-bo;School of Astronautics;Northwestern Polytechnial University;School of Aircraft Engineering;Nanchang Hangkong University;
SUN Hai-jun;ZENG Zhuo-xiong;XU Yi-hua;HU Chun-bo;School of Astronautics;Northwestern Polytechnial University;School of Aircraft Engineering;Nanchang Hangkong University;
..............page:1639-1646
Effect of baffle plate of rotating limited lamilloy on flow heat transfer of lamilboy
BAI Guo-qiang;CHANG Hai-ping;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
BAI Guo-qiang;CHANG Hai-ping;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1647-1653
Effect of porous media structure parameters on surface flame blow-out performance
ZHANG Long;XU Quan-hong;ZHANG Chi;LIN Pei-hua;LIN Yu-zhen;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHANG Long;XU Quan-hong;ZHANG Chi;LIN Pei-hua;LIN Yu-zhen;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1654-1659
Experiment on inlet pressure distortion of high-pressure compressor
WU Hui;ZHANG Guo-wang;YANG Ming-sui;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
WU Hui;ZHANG Guo-wang;YANG Ming-sui;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1660-1666
Aerodynamic design of three-stage vaneless counter-rotating turbine
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;Turbine Division;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
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;Turbine Division;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1667-1679
Dynamics mechanism of tip leakage flow trajectory movement in rotor
LIU Dong-jian;LI Jun;LI Jian-wei;LUO Zhi-huang;LI Fan-yu;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;Military Representative Office in Jingdezhen Region;Army Aviation Department;General Staff Headquters;
LIU Dong-jian;LI Jun;LI Jian-wei;LUO Zhi-huang;LI Fan-yu;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;Military Representative Office in Jingdezhen Region;Army Aviation Department;General Staff Headquters;
..............page:1680-1687
Numerical investigation on effect of heat transfer on tip clearance flow in micro centrifugal impellers
SUN Qian-wei;LI Qiu-shi;LI Zhi-ping;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Co-Innovation Center for Advanced Aero-Engine;
SUN Qian-wei;LI Qiu-shi;LI Zhi-ping;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Co-Innovation Center for Advanced Aero-Engine;
..............page:1688-1694
Numerical investigation of effect of tip clearance on stress of high pressure turbine rotor
LI Yu-jie;LIU Yong-bao;College of Power Engineering;Naval University of Engineering;
LI Yu-jie;LIU Yong-bao;College of Power Engineering;Naval University of Engineering;
..............page:1695-1700
Feature analysis on US military aircraft engine advanced technology programs
LIANG Chun-hua;SUN Ming-xia;LIU Hong-xia;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
LIANG Chun-hua;SUN Ming-xia;LIU Hong-xia;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1701-1709
One-dimensional unsteady calculational method of secondary air system
LI Peng;WU Hong;TAO Zhi;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
LI Peng;WU Hong;TAO Zhi;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1710-1720
Flight dynamics characteristics of miniature unmanned ducted vehicle
ZHAO Hong;LI Jian-bo;CUI Zhao;State Key Laboratory of Helicopter Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
ZHAO Hong;LI Jian-bo;CUI Zhao;State Key Laboratory of Helicopter Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1721-1728
Optimal guaranteed cost fault-tolerant control with bi-index constraints for aero-engine distributed control system
WANG Lei;XIE Shou-sheng;PENG Jing-bo;YANG Yong;REN Li-tong;Aeronautics and Astronautics Engineering College;Air Force Engineering University;Unit 93704 of the Chinese People’s Liberation Army;
WANG Lei;XIE Shou-sheng;PENG Jing-bo;YANG Yong;REN Li-tong;Aeronautics and Astronautics Engineering College;Air Force Engineering University;Unit 93704 of the Chinese People’s Liberation Army;
..............page:1729-1737
Real-time obstacle avoidance trajectory planning for missile borne air vehicle based on constrained artificial potential field method
WANG Wei;WANG Hua;School of Astronautics;Beijing University of Aeronautics and Astronautics;
WANG Wei;WANG Hua;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:1738-1743
Design and simulation of a control scheme for turbo-shaft engine in helicopter autorotation training process
YAN Chang-kai;ZHOU Xiao;ZHANG Hai-bo;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
YAN Chang-kai;ZHOU Xiao;ZHANG Hai-bo;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1744-1751
Pre-control and experiment method of meshing performance for face gear drives
LEI Bao-zhen;LI Da-qing;WANG Xun-wei;DENG Xiao-zhong;School of Mechatronics;Beijing Union University;School of Mechanical Engineering;Henan Institute of Engineering;School of Mechatronics Engineering;Henan University of Science and Technology;
LEI Bao-zhen;LI Da-qing;WANG Xun-wei;DENG Xiao-zhong;School of Mechatronics;Beijing Union University;School of Mechanical Engineering;Henan Institute of Engineering;School of Mechatronics Engineering;Henan University of Science and Technology;
..............page:1752-1760