《航空發(fā)動(dòng)機(jī)》2016年總目次(中英文)
“先進(jìn)控制技術(shù)”專欄Advanced control technology column
超燃沖壓發(fā)動(dòng)機(jī)研究現(xiàn)狀及控制系統(tǒng)關(guān)鍵技術(shù)……………………………………………………………………………………袁春飛,仇小杰(4-1)
Research Status and Key Technologies of Control System for Scramjet…………………………………………………YUAN Chun-fei,QIU Xiao-jie(4-1)
艦用航改燃?xì)廨啓C(jī)通用控制系統(tǒng)研制及應(yīng)用………………………………………………………………………………………薛瑋,張力輝(4-8)
Development and Application of General Control System for Aeroderivative Gas Turbine Used in Ship………………………XUE Wei,ZHANG Li-hu(i4-8)
基于模型的系統(tǒng)工程概述………………………………………………………………………………………朱靜,楊暉,高亞輝,姚太克(4-12)
Summary of Model Based System Engineering……………………………………………………ZHU Jing,YANG Hui,GAO Ya-hui,YAO Tai-ke(4-12)
根軌跡法在燃油控制回路PI控制器參數(shù)設(shè)計(jì)中的應(yīng)用………………………………………………………………徐建,楊剛,胡文霏(4-17)
Research on Applying Root Locus to Parameter Design of Fuel Control Loop PI Controller………………………XU Jian,YANG Gang,HU Wen-fe(i4-17)
伺服回路故障檢測(cè)方法研究………………………………………………………………………………………………賈盼盼,劉冬,王振華(4-21)
The Research for Fault Diagnosis Method of Servo Loop……………………………………………………JIA Pan-pan,LIU Dong,WANG Zhen-hua(4-21)
小型渦噴發(fā)動(dòng)機(jī)故障分析及控制系統(tǒng)改進(jìn)………………………………………………………………………………………陶德桂,王成軍(4-25)
Failure Analysis and Control System Improvement of Small Turbojet Engine……………………………………………Tao De-gui,Wang Cheng-jun(4-25)
航空發(fā)動(dòng)機(jī)燃油系統(tǒng)執(zhí)行機(jī)構(gòu)故障診斷及驗(yàn)證………………………………………………………………潘陽(yáng),李秋紅,姜潔,劉立婷(4-30)
Fault Diagnosis and Validation for Aeroengine Fuel System Actuator………………………………PAN Yang,LI Qiu-hong,JIANG Jie,LIU Li-ting(4-30)
混合總線測(cè)控系統(tǒng)在R0110燃?xì)廨啓C(jī)低排放試驗(yàn)中的應(yīng)用……………………………………………………………陳海清,孫永飛,熊進(jìn)星(4-36)
Application about Mixed-Bus Measure-Control System in R0110 Low Emission Tests……………CHEN Hai-qing,SUN Yong-fei,XIONG Jin-xing(4-36)
渦扇發(fā)動(dòng)機(jī)極值限制保護(hù)閉環(huán)控制設(shè)計(jì)……………………………………………………………………………………………王曦,李志鵬(5-1)
Design of Limit Protection Controller with Closed Loop for Turbofan Engine……………………………………………………WANG Xi,LI Zhi-peng(5-1)
存在數(shù)據(jù)丟包的航空發(fā)動(dòng)機(jī)分布式控制器設(shè)計(jì)…………………………………………………………………………宋軍強(qiáng),黃金泉,潘慕絢(5-8)
Controller Design for Aeroengine with Communication Data Dropout in DCS……………………SONG Jun-qiang,HUANG Jin-quan,PAN Mu-xuan(5-8)
基于直升機(jī)/發(fā)動(dòng)機(jī)綜合模型的變旋翼轉(zhuǎn)速控制研究……………………………………………………………………………陳國(guó)強(qiáng),楊娟(5-14)
Research on Variable Rotor Speed Control Based on Integrated Helicopter/Engine Model……………………………CHEN Guo-qiang,YANG Juan(5-14)
步進(jìn)電機(jī)驅(qū)動(dòng)的燃油計(jì)量裝置建模與仿真……………………………………………………………………曹啟威,王彬,趙皓岑,葉志鋒(5-21)
Modeling and Simulation of Fuel Metering Unit Driven by Stepping Motor…………………CAO Qi-wei,WANG Bin,ZHAO Hao-cen,YE Zhi-feng(5-21)
全權(quán)限數(shù)字電子控制器雷電試驗(yàn)方法研究………………………………………………………………………………孔祥明,邵志江,顧穎慧(5-26)
Lightning Test Methods for FADEC………………………………………………………………KONG Xiang-ming,SHAO Zhi-jiang,GU Ying-hu(i5-26)
SPWM控制算法的Matlab仿真和失真度分析…………………………………………………………………余樂(lè)詠,張小妍,范明,季國(guó)林(5-32)
Research on Matlab Simulation and THD Analysis for SPWM Control Algorithm………………YU Le-yong,ZHANG Xiao-yan,FAN Ming,JI Guo-lin(5-32)
用于分級(jí)燃燒的高性能燃油分配器的改進(jìn)設(shè)計(jì)與仿真…………………………………………………………………李鑫,張榮,葉志鋒(5-38)
Improved Design and Simulation of High Performance Fuel Distributor for Staged Combustion………………………LI Xin,Zhang Rong,Ye Zhi-feng(5-38)
SCADE在航空發(fā)動(dòng)機(jī)FADEC軟件開(kāi)發(fā)中的應(yīng)用………………………………………………………………………………方偉,周彰毅(5-43)
Research on SCADE for Aeroengine FADECS oft ware……………………………………………………………………FANG Wei,ZHOU Zhang-y(i5-43)
半物理試驗(yàn)起動(dòng)階段低溫燃油流量計(jì)量技術(shù)路徑探究……………………………………………………………………………………史春雨(6-1)
Measurement Technology of Fuel Flowunder Low Temperature Starting in Semi-physical Test…………………………………………SHI Chun-yu(6-1)
國(guó)外渦槳發(fā)動(dòng)機(jī)控制技術(shù)的發(fā)展……………………………………………………………………………………………………陳懷榮,王曦(6-9)
Development of Turboprop Engine Control Technology in the West………………………………………………………CHEN Huai-rong,WANGX(i6-9)
基于FPGA的步進(jìn)電機(jī)細(xì)分控制研究…………………………………………………………………古玉雪,張小妍,李華忠,何流,蔣文亮(6-18)
Research on Microstep Control of the Stepping Motor Based on FPGA……GU Yu-xue,ZHANG Xiao-yan,LI Hua-zhong,HE Liu,JIANG Wen-liang(6-18)
基于確定學(xué)習(xí)理論的軸流壓氣機(jī)系統(tǒng)分岔預(yù)測(cè)………………………………………………………文彬鶴,王聰,易學(xué)飛,聞偉,朱愛(ài)峰(6-23)
Precursor for Bifurcation of Axial Compression System based on Deterministic Learning……………………………………………………………………………………WEN Bin-he,WANG Cong,YI Xue-fei,WEN Wei,ZHU Ai-feng(6-23)
微型渦輪噴氣發(fā)動(dòng)機(jī)風(fēng)車起動(dòng)特性研究……………………………………………………………………………………………………萬(wàn)照云(6-30)
Study on Micro Turboengine Windmill Starting Characteristics………………………………………………………………………WAN Zhao-yun(6-30)
設(shè)計(jì)Design
基于蜂群算法的變循環(huán)發(fā)動(dòng)機(jī)最小耗油率優(yōu)化………………………………………………………駱廣琦,李游,吳濤,胡砷纛,曾劍臣(1-1)
The Minimum Fuel Consumption Optimization of Variable Cycle Engine Based on Artificial Bee Colony Algorithm………………………………………………………………………………………LUO Guang-qi,LI You,WU Tao,HU Shen-dao,Zeng Jian-chen(1-1)
90°多彎管阻力系數(shù)計(jì)算方法…………………………………………………………………………成鋒娜,常海萍,田興江,張鏡洋,陸海鷹(1-6)
Calculation Method of Resistance Coefficient in 90°Combined Bends……………………………………………………………CHENG Feng-na,CHANG Hai-ping,TIAN Xing-jiang,ZHANG Jing-yang,LU Hai-ying(1-6)
塞錐形狀和偏轉(zhuǎn)角對(duì)軸對(duì)稱塞式噴管氣動(dòng)性能的影響…………………………………………………………………王旭,張靖周,單勇(1-11)
Effects of Plug Shape and Vectoring Angle on Aerodynamic Performance of Axisymmetric Plug Nozzle…WANG Xu,ZHANG Jing-zhou,SHAN Yong(1-11)
渦軸發(fā)動(dòng)機(jī)雙回路PI控制器多發(fā)功率匹配…………………………………………………………楊超,王曦,時(shí)瑞軍,周劍波,高世煌(1-16)
Power Balance for Multiple Engines Based on Double-Loop PI Controller for Turboshaft………………………………………………………………………………YANG Chao,WANG Xi,SHI Rui-jun,ZHOU Jian-bo,GAO Shi-huang(1-16)
替代燃料對(duì)航空發(fā)動(dòng)機(jī)燃燒室性能影響的計(jì)算研究………………………………………………郭瑞卿,唐正府,尚守堂,呂付國(guó),李鋒(1-21)
Simulation on Influence of Alternative Fuel on Combustor Performance for Aeroengine…………………………………………………………………………GUO Rui-qing,TANG Zheng-fu,SHANG Shou-tang,LYU Fu-guo,LI Feng(1-21)
基于共振分析的發(fā)動(dòng)機(jī)附件傳動(dòng)系統(tǒng)危險(xiǎn)齒輪的確定…………………………………………………………………歐陽(yáng)旭靖,郭梅,王建軍(25)
Determine the Dangerous Gear in Accessory Gear System of Engine Based on Resonance Analysis……OUYANG Xu-jing,GUO Mei,WANG Jian-jun(1-25)
薄壁構(gòu)件試驗(yàn)?zāi)P偷膭?dòng)力學(xué)相似設(shè)計(jì)方法……………………………………………………………王有,羅忠,曲濤,王德友,劉永泉(1-32)
Dynamic Similitude Design Method of Experimental Models for Thin Walled Structures…………………………………………………………………………………WANG You,LUO Zhong,QU Tao,WANG De-you,LIU Yong-quan(1-32)
基于燃?xì)夥治龇ǖ暮娇瞻l(fā)動(dòng)機(jī)燃燒室性能研究……………………………………………李亞娟,王明瑞,葛新,韓冰,馬征,賈琳妍(1-37)
Research on Aeroengine Combustor Performance Based on Gas Analysis Method…………………………………………………………………………LI Ya-juan,WANG Ming-rui,GE Xin,HAN Bing,MA Zheng,JIA Lin-yan(1-37)
燃油管路系統(tǒng)振動(dòng)特性有限元模擬技術(shù)…………………………………………………………………………………………趙偉志,陳志英(1-42)
Research on Finite Element Simulation Technology of Fuel Pipe System Vibration Characteristics…………………ZHAO Wei-zhi,CHEN Zhi-ying(1-42)
變壁厚氣冷渦輪葉片結(jié)構(gòu)參數(shù)化設(shè)計(jì)方法………………………………………………………………………………鐘治魁,郝艷華,黃致建(1-48)
Parametric Design Method of Air-Cooled Turbine Blade Structure with Variable Thickness……ZHONG Zhi-kui,HAO Yan-hua,HUANG Zhi-jian(1-48)
基于微分進(jìn)化算法的航空發(fā)動(dòng)機(jī)模型修正……………………………………………………………………朱正琛,李秋紅,王元,潘鵬飛(1-53)
Correction of Aeroengine Model Based on Differential Evolution Algorithm………………ZHU Zheng-chen,LI Qiu-hong,WANG Yuan,Pan Peng-fe(i1-53)
液態(tài)水含量對(duì)防冰表面水膜流動(dòng)換熱的影響……………………………………………………………………………鄭梅,朱劍鋆,董威(1-59)
Influence of Liquid Water Content on Flow and Heat Transfer of Water Filmon Anti-Icing Surfaces………ZHENG Mei,ZHU Jian-jun,DONG We(i1-59)
基于ADAMS的靜葉聯(lián)調(diào)機(jī)構(gòu)參數(shù)化設(shè)計(jì)………………………………………………………………………………梁爽,印雪梅,王華(1-65)
Parametric Design of Stator Blade Jointly Adjusting Mechanism Based on ADAMS………………………LIANG Shuang,YIN Xue-mei,WANG Hua(1-65)
某型發(fā)動(dòng)機(jī)潤(rùn)滑供油系統(tǒng)流量仿真分析…………………………………………………………………………………蘇媛媛,毛福榮,路彬(1-70)
Analysis of Flow Simulation on an Aeroengine Lubrication System……………………………………………SU Yuan-yuan,MAO Fu-rong,LU Bin(1-70)
前緣半徑對(duì)鈦合金葉片抗外物損傷能力影響的數(shù)值分析………………………………………………………………孫護(hù)國(guó),李永建,葉斌(2-1)
Numerical Analysis of Effects of Leading Edge Radius on Resistance to Foreign Object Damage Capability of Titanium Alloy Blade……………………………………………………………………………………………………………………SUN Hu-guo,LI Yong-jian,YE Bin(2-1)
氣液2相離心甩油盤(pán)設(shè)計(jì)……………………………………………………………………………………………………………………蔣雪輝(2-7)
Design ofa Gas-liquid Two-phase Slinger……………………………………………………………………………………………JIANG Xue-hu(i2-7)
低排放燃燒室化學(xué)反應(yīng)器網(wǎng)絡(luò)模型的參數(shù)化…………………………………………………………劉闖,李鵬飛,劉勇,朱冬清,金仁瀚(2-11)
Parameterized Chemical Reactor Networks Molds of Low-Emission Combustor…LIU Chuang,LI Peng-fei,LIU Yong,ZHU Dong-qing,JIN Ren-han(2-11)
射流角度對(duì)M-TIB燃燒性能影響分析……………………………………………………………………………………………張?chǎng)?,唐豪?-17)
Analysis of Influence of Air Injection Angle on Combustion Performance for M-TIB Combustor……………………………ZHANG Xin,TANG Hao(2-17)
基于體積力模型的1維渦輪特性評(píng)估方法………………………………………………………………………………何杰,鄒正平,姚李超(2-22)
AOne-Dimensional Simulation Method to Evaluate Turbine Performance Based on Body Forced Model……HE Jie,ZOU Zheng-ping,YAO Li-chao(2-22)
面向方案設(shè)計(jì)階段的發(fā)動(dòng)機(jī)質(zhì)量評(píng)估方法……………………………………………………………胡殿印,胡丹,霍楓,樊江,陳高翔(2-27)
Estimation Method of Aeroengine Weight at Concept Design Stage…………………HU Dian-yin,HU Dan,HUO Feng,F(xiàn)AN Jiang,CHEN Gao-xiang(2-27)
考慮限制保護(hù)的航空發(fā)動(dòng)機(jī)起動(dòng)控制技術(shù)…………………………………………………殷鍇,魏芳,張榮,黃瀏,李志鵬,王曦(2-34)
Starting Control Strategy Considering Limit Protection for Turbofan Engine…YIN Kai,WEI Fang,ZHANG Rong,HUANG Liu,LI Zhi-peng,WANGX(i2-34)
鼠籠式彈性支承結(jié)構(gòu)參數(shù)分步優(yōu)化設(shè)計(jì)方法……………………………………………………………唐瑞,郭健,羅忠,王德友,劉永泉(2-38)
Optimal Design Method of Squirrel Cage Elastic Support by Stages……………TANG Rui,GUO Jian,LUO Zhong,WANG De-you,LIU Yong-quan(2-38)
基于熱管理技術(shù)的航空發(fā)動(dòng)機(jī)滑油系統(tǒng)熱分析方法……………………………………………………………………蘇壯,毛宏圖,宋冠麟(2-44)
Thermoanalysis Method of Aeroengine Lubrication System Based on Heat Management Technology……SU Zhuang,MAO Hong-tu,SONG Guan-lin(2-44)
基于優(yōu)化智能網(wǎng)絡(luò)的發(fā)動(dòng)機(jī)推力指令模型……………………………………………………………………潘陽(yáng),李秋紅,顧書(shū)文,李業(yè)波(2-51)
Aeroengine Thrust Command Model Based on Optimized Intelligent Networks……………………PANYang,LI Qiu-hong,GU Shu-wen,LI Ye-bo(2-51)
民用發(fā)動(dòng)機(jī)空中慢車性能設(shè)計(jì)方法…………………………………………………………………………………………………………曾濤(2-57)
Design Method of Commercial Aircraft Engine Flight Idle……………………………………………………………………………………ZENG Tao(2-57)
典型工況下低排放燃燒室的壓力振蕩特性………………………………………………………………………………李文朝,林宇震,秦皓(2-61)
Pressure Oscillation Characteristics of Low Emissions Combustor in Typical Conditions………………………LI Wen-zhao,LIN Yu-zhen,Qin Hao(2-61)
基于響應(yīng)面法的齒輪容差設(shè)計(jì)方法研究…………………………………………………………………………王桂華,井海龍,史妍妍,陳云霞(3-1)
Methods of Tolerance Design for Gears Based on Response Surface Methodology……WANG Gui-hua,JING Hai-long,SHI Yan-yan,CHEN Yun-xia(3-1)
支承剛度和軸向位置對(duì)某型對(duì)轉(zhuǎn)發(fā)動(dòng)機(jī)低壓轉(zhuǎn)子臨界轉(zhuǎn)速的影響…………………………鄧旺群,王毅,聶衛(wèi)健,何萍,徐友良,楊海(3-7)
Influence of Supporting Stiffness and Axial Location on Critical Speeds of a Low-pressure Rotor of a Counter Rotating Engine……………………………………………………………………DENG Wang-qun,WANGYi,NIE Wei-jian,HE Ping,XU You-liang,YANG Ha(i3-7)
壓差控制器的穩(wěn)定性分析和設(shè)計(jì)參數(shù)的研究…………………………………………………………李洪勝,王曦,王華威,黨偉,張耿(3-12)
Differential Pressure Controller Stability Analysis and Research of Design Parameters……………………………………………………………………………LI Hong-sheng,WANG Xi,WANG Hua-wei,DANG Wei,ZHANG Geng(3-12)
航空發(fā)動(dòng)機(jī)渦輪噪聲適航性評(píng)估平臺(tái)設(shè)計(jì)及應(yīng)用………………………………………………………………………張鴻,江朝振,閆國(guó)華(3-17)
Design and Application of Turbine Noise Airworthiness Assessment Platform of Aeroengine ………ZHANG Hong,JIANG Chao-zhen,YAN Guo-hua(3-17)
2級(jí)渦輪內(nèi)部流動(dòng)定常與非定常計(jì)算差異研究…………………………………………………………………楊杰,周穎,潘尚能,盧聰明(3-21)
Study of Differences between Steady and Unsteady Computation for Two-Stage Turbine Internal Flow……………………………………………………………………………………………YANG Jie,ZHOU Ying,PAN Shang-neng,LU Cong-ming(3-21)
高轉(zhuǎn)速大長(zhǎng)徑比傳動(dòng)桿動(dòng)態(tài)特性研究…………………………………………………………………………郭霞,章煥章,程小勇,王少波(3-28)
Dynamic Characteristics Study on Transmission Rod with High Speed and Large Aspect Ratio………………………………………………………………………………GUO Xia,ZHANG Huan-zhang,CHENG Xiao-yong,WANG Shao-bo(3-28)
基于機(jī)載實(shí)時(shí)模型的發(fā)動(dòng)機(jī)執(zhí)行機(jī)構(gòu)故障狀態(tài)參數(shù)估計(jì)………………………………………………………………何佳倩,李建榕,張志舒(3-33)
Actuator Fault State Parameter Estimation of Aeroengine based on On-Board Real Time Model…………HE Jia-qian,LI Jian-rong,ZHANG Zhi-shu(3-33)
基于振動(dòng)能量積奇異值分解的航空發(fā)動(dòng)機(jī)振動(dòng)狀態(tài)識(shí)別………………………………………………………………………秦海勤,徐可君(3-38)
Recognition of Different Vibration States of Aeroengine Based on the Vibration Energy Product SVD………………………QIN Hai-qin,XU Ke-jun(3-38)
2元超聲速混壓式進(jìn)氣道的設(shè)計(jì)及進(jìn)-發(fā)匹配分析………………………………………………………………………………余天寧,吳虎(3-43)
Design for Two-Dimensional Supersonic Mixed Compression Inlet and Analysis of Inlet-Engine Matching……………………YU Tian-ning,WU Hu(3-43)
失調(diào)葉盤(pán)結(jié)構(gòu)模態(tài)特性及抗共振可靠度分析…………………………………………………………王鷂瑋,白廣忱,白斌,姚偉,高海峰(3-48)
Analysis of Modal Characteristics and Anti-Resonance of Mistuned Bladed Disk………………………………………………………………………………WANG Yao-wei,BAI Guang-chen,BAI Bin,YAO Wei,GAO Hai-feng(3-48)
基于氣動(dòng)性能優(yōu)化的某型發(fā)動(dòng)機(jī)外涵機(jī)匣結(jié)構(gòu)設(shè)計(jì)…………………………………………………田大可,袁長(zhǎng)龍,徐雪,張德志,王海龍(4-43)
Research on Structure Design of the Bypass Casing for a Certain Type Aeroengine Based on Aerodynamic Performance Optimization………………………………………………………………………TIAN Da-ke,YUAN Chang-long,XU Xue,ZHANG De-zhi,WANG Hai-long(4-43)
燃?xì)廨啓C(jī)燃燒室火焰筒耐溫技術(shù)的發(fā)展與應(yīng)用………………………………………………………………趙傳亮,呼姚,馬宏宇,尚守堂(4-47)
Development and Application of Heat Resisting Techniques for Gas Turbine Combustor Liner………………………………………………………………………………………ZHAO Chuan-liang,HU Yao,MA Hong-yu,SHANG Shou-tang(4-47)
點(diǎn)火參數(shù)對(duì)煤油活塞發(fā)動(dòng)機(jī)燃燒影響的數(shù)值模擬……………………………………………………貝太學(xué),魏民祥,劉銳,李冰林,牛燕華(4-55)
Numerical Simulation on Influence of Ignition Parameters on Combustion of Kerosene Piston Engine……………………………………………………………………………………BEI Tai-xue,WEI Min-xiang,LIU Rui,LI Bing-lin,NIU Yan-hua(4-55)
圓弧端齒對(duì)渦輪螺栓連接影響的數(shù)值研究……………………………………………………………羅莉,施一長(zhǎng),李杰,王克菲,陳亞龍(4-60)
Numerical Study on the Influence of Curvic Couplings on Turbine Bolt Connection……LUO Li,SHI Yi-chang,LI Jie,WANG Ke-fei,CHEN Ya-long(4-60)
某型燃?xì)廨啓C(jī)樅樹(shù)形榫接結(jié)構(gòu)多齒形參數(shù)優(yōu)化分析…………………………………………………………宗洪明,陶海亮,高慶,譚春青(4-64)
Structural Analysis and Optimization of Gas Turbine Fir-Tree Attachment with Various Tooth Profile Parameters………………………………………………………………………………………ZONG Hong-ming,TAO Hai-liang,GAO Qing,TAN Chun-qing(4-64)
基于歸一化參數(shù)模型的渦輪盤(pán)和渦輪葉片蠕變分析……………………………………………………………………李宏新,王延榮,程域釗(5-48)
Analysis of Creep Based on Normalized-Parameter Model for Turbine Disk and Blade……………LI Hong-xin,WANG Yan-rong,CHENG Yu-zhao(5-48)
單邊膨脹球面2元噴管雷達(dá)隱身修形研究……………………………………………………………………楊勝男,邵萬(wàn)仁,尚守堂,鄧洪偉(5-55)
Study on Radar Stealth Shaping for Single Expansion Ramp with Spherical 2-DNozzle……………………………………………………………………………YANG Sheng-nan,SHAO Wan-ren,SHANG Shou-tang,DENG Hong-we(i5-55)
防冰引氣對(duì)組合壓氣機(jī)性能影響的數(shù)值模擬研究……………………………………………………………賀丹,李杜,張錦綸,鄒學(xué)奇(5-63)
Numerical Simulation Investigation on Influence of Anti-icing Bleed on Performance of Combined Compressor………………………………………………………………………………………………………HE Dan,LI Du,ZHANG Jin-lun,ZOU Xue-q(i5-63)
旋轉(zhuǎn)帽罩表面積冰甩脫位置的數(shù)值模擬…………………………………………………………………………………傅亮,陳勇,王安正(5-70)
Numerical Simulation of Ice Shedding from Spinning Cone…………………………………………………FU Liang,CHEN Yong,WANG An-zheng(5-70)
基于有效面積作用的膜盒式壓力比敏感元件設(shè)計(jì)………………………………………………………………………………王戰(zhàn)生,崔國(guó)序(5-76)
Design of Capsule Pressure-Ratio Sensitive Element Based on Effect of Effective Area……………………………WANG Zhan-sheng,CUI Guo-xu(5-76)
開(kāi)式轉(zhuǎn)子發(fā)動(dòng)機(jī)計(jì)算模型及調(diào)節(jié)研究…………………………………………………………………屠秋野,倪力偉,楊祥明,鄭恒,蔣平(6-36)
Research on Open Rotor Engine Caculating Model and Control Schedule……TU Qiu-ye,NI Li-wei,YANG Xiang-ming,ZHENG Heng,JIANG Ping(6-36)
航空發(fā)動(dòng)機(jī)套齒結(jié)構(gòu)配合穩(wěn)健性優(yōu)化設(shè)計(jì)………………………………………………………………………………劉宏蕾,陳志英,周平(6-44)
Robust Optimization Design of Aeroengine Mating Spline Structure………………………………………LIU Hong-lei,CHEN Zhi-ying,ZHOU Ping(6-44)
3外涵變循環(huán)發(fā)動(dòng)機(jī)循環(huán)參數(shù)匹配模擬…………………………………………………………………………………劉勤,李剛團(tuán),黃紅超(6-51)
Matching Simulation on Cycle Parameter of Triple Bypass Variable Cycle Engine………………………LIU Qin,LI Gang-tuan,HUANG Hong-chao(6-51)
渦輪葉片徑向槽軸向長(zhǎng)度對(duì)超緊湊燃燒室性能的影響…………………………………………………………………王力軍,周輝,江金濤(6-55)
Effects of Cavity Length of Turbine Radial Vane Cavity on Performance of Ultra-Compact Combustor……WANG Li-jun,ZHOU Hui,JIANG Jin-tao(6-55)
試驗(yàn)Experiment
大擴(kuò)張角渦輪過(guò)渡段性能試驗(yàn)和數(shù)值研究……………………………………………………………………施鎏鎏,羅華玲,張顏,劉火星(1-75)
Experimental and Numerical Investigation on the Performance of an Aggressive Intermediate Turbine Duct……………………………………………………………………………………………SHI Liu-liu,LUO Hua-ling,ZHANG Yan,LIU Huo-xing(1-75)
AZ31B鎂合金大應(yīng)變循環(huán)變形行為研究………………………………………………………………耿長(zhǎng)建,師俊東,李曉欣,王志宏,滕佰秋(1-79)
Cyclic Deformation Behavior of AZ31B Magnesium Alloy at Large Amplitude……………………………………………………………………GENG Chang-jian,SHI Jun-dong,LI Xiao-xin,WANG Zhi-hong,TENG Bai-qiu(1-79)
多斜孔冷卻火焰筒燃燒性能試驗(yàn)研究……………………………………………………………………………………………刁瑤朋,王少波(1-84)
Experimental Study on Combustion Performance of Multiple Incline Holes Cooling Flame Tube……………………DIAO Yao-peng,WANG Shao-bo(1-84)
某壓氣機(jī)試驗(yàn)件轉(zhuǎn)子平衡精度分析………………………………………………………………………………………………紀(jì)福森,翟賢超(1-88)
Analysis of Balance Precision for a Compressor Test Rig…………………………………………………………………JI Fu-sen,ZHAI Xian-chao(1-88)
欠頻響壓力探針測(cè)量壓氣機(jī)動(dòng)態(tài)流場(chǎng)的結(jié)果分析……………………………………………………………馬宏偉,魏巍,張良,官輝(2-67)
Analysis of the Measured Unsteady Flow Field Using a Quasi Fast Response Pressure Probe……MA Hong-wei,WEI Wei,ZHANG Liang,GUAN Hu(i2-67)
航空發(fā)動(dòng)機(jī)機(jī)匣包容試驗(yàn)葉片飛脫方法………………………………………………………………………郭明明,呂登洲,洪偉榮,曹繼來(lái)(2-73)
Blade out Methods of Aeroengine Case Containment Test…………………………GUO Ming-ming,LYU Deng-zhou,HONG Wei-rong,CAO Ji-la(i2-73)
1 種用于渦輪出口總溫測(cè)量的新型熱電偶的設(shè)計(jì)………………………………………………………………………劉緒鵬,劉忠奎,孫琪(2-77)
Design of Thermocouple Probe for Measurement of Turbine Outlet Total Temperature…………………………LIU Xu-peng,LIU Zhong-kui,SUNQ(i2-77)
內(nèi)機(jī)匣故障對(duì)燃燒室性能影響的數(shù)值與試驗(yàn)研究………………………………………………………………………王文波,岳明,金捷(2-83)
Numerical and Experimental Study of Effect of Inner Casing Failure on Combustor Performance…………………WANG Wen-bo,YUE Ming,JIN Jie(2-83)
基于損傷力學(xué)的GH4169合金低循環(huán)裂紋萌生壽命預(yù)測(cè)……………………………………………初金陽(yáng),胡殿印,毛建興,王榮橋,申秀麗(2-88)
Prediction of GH4169 Low Cycle Crack Initiation Life based on Damage Mechanics……………………………………………………………………CHU Jin-yang,HU Dian-yin,MAO Jian-xing,WANG Rong-qiao,SHEN Xiu-l(i2-88)
級(jí)負(fù)荷系數(shù)為0.42的小流量軸流壓氣機(jī)設(shè)計(jì)與試驗(yàn)驗(yàn)證……………………………………………………王立志,陽(yáng)誠(chéng)武,張香華,路縱橫(3-54)
Design and Measurements for a Small Flow Rate Axial Compressor with Stage Work Coefficient of0.42…………………………………………………………………………………WANG Li-zhi,YANG Cheng-wu,ZHAN Gxiang-hua,LU Zong-heng(3-54)
圓弧形榫連結(jié)構(gòu)高/低循環(huán)疲勞試驗(yàn)研究……………………………………………………………李迪,王延榮,廖連芳,王家廣,衛(wèi)飛飛(3-61)
Investigation of High and Low Cycle Fatigue Experiment for a Curved Dovetail Assembly……………………………………………………………………………LI Di,WANG Yan-rong,LIAO Lian-fang,WANG Jia-guang,WEI Fei-fe(i3-61)
7孔復(fù)合探針在平面葉柵流場(chǎng)測(cè)量中的應(yīng)用…………………………………………………王東,雷志軍,劉建明,馬磊,武卉,郝晟淳(3-67)
Application of Seven-Holes Composite Probe in Measurement of Plane Cascade Flow Field……………………………………………………………………WANG Dong,LEI Zhi-jun,LIU Jian-ming,MA Lei,WU Hui,HAO Sheng-chun(3-67)
扇形段與全環(huán)燃燒室熄火性能換算研究………………………………………………………………楊志民,趙明龍,林宇震,葛新,劉金林(3-74)
Conversion Investigation on Blowout Performance for Multi-Sector and Full Annular Combustors………………………………………………………………………………YANG Zhi-min,ZHAO Ming-long,LIN Yu-zhen,GE Xin,LIU Jin-lin(3-74)
基于飛行試驗(yàn)數(shù)據(jù)的雙轉(zhuǎn)子航空發(fā)動(dòng)機(jī)加減速瞬態(tài)模型辨識(shí)…………………………………………………………潘鵬飛,馬明明,許艷芝(3-78)
Throttling-Transient Model Identification of Twin Spool Aeroengine Based on Flight Test Data…………PAN Peng-fei,MA Ming-ming,XU Yan-zh(i3-78)
航空發(fā)動(dòng)機(jī)轉(zhuǎn)速傳感器振動(dòng)試驗(yàn)載荷確定及應(yīng)用……………………………………………………………王志會(huì),劉海年,翟月,張生(3-82)
Formulation and Application for Vibration Test Loading Spectrum of an Aeroengine Revolution Transmitter……………………………………………………………………………………………WANG Zhi-hui,LIU Hai-nian,ZHAI Yue,ZHANGSheng(3-82)
航空發(fā)動(dòng)機(jī)液壓管路靜壓力損失分析及試驗(yàn)驗(yàn)證………………………………………………………………………………陸浩,周毅博(3-88)
Investigation and Experimental Validation on Static Pressure Loss of Aeroengine Hydraulic Pipe………………………………LU Hao,ZHOU Yi-bo(3-88)
變幅載荷對(duì)高溫合金裂紋萌生及擴(kuò)展壽命的影響……………………………………………………初金陽(yáng),申秀麗,毛建興,胡殿印,王榮橋(4-70)
Effect of Crack Initiation and Propagation Life of High Temperature Alloyunder Variable Amplitude……………………………………………………………………CHU Jin-yang,SHEN Xiu-li,MAO Jian-xing,HU Dian-yin,WANG Rong-qiao(4-70)
航空發(fā)動(dòng)機(jī)推力測(cè)量臺(tái)架原理誤差分析…………………………………………………………………………………張有,吳鋒,何培壘(4-76)
Principle Errors Analysis of Thrust Measurement Test Bench System for Aeroengine……………………………ZHANG You,WU Feng,HE Pei-le(i4-76)
DD6鎳基單晶渦輪轉(zhuǎn)子葉片失效分析…………………………………………………………………………胡霖,佟文偉,高志坤,韓振宇(4-81)
Failure Analysis of the Turbine Blade of DD6 Nickel-Base Single Crystal…………………HU Lin,TONG Wen-wei,GAO Zhi-kun,HAN Zhen-yu(4-81)
單液滴破碎流動(dòng)機(jī)理試驗(yàn)研究…………………………………………………………………………………劉闖,金仁瀚,劉勇,龔勛(4-87)
Experimental Investigation on Flow Mechanism of Single Droplet Deformation and Breakage………LIU Chuang,JIN Ren-han,LIU Yong,GONG Xun(4-87)
低速軸流壓氣機(jī)旋轉(zhuǎn)失速演化機(jī)制研究………………………………………………………………賀象,銀越千,黃生勤,馬宏偉,魏?。?-81)
Investigation on the Rotating Stall in a Low-Speed Axial Compressor………HE Xiang,YIN Yue-qian,HUANG Sheng-qin,MA Hong-wei,WEI We(i5-81)
航空發(fā)動(dòng)機(jī)主燃燒室高溫測(cè)試技術(shù)王……………………………………………………………………明瑞,王振華,韓冰,李亞娟,葛新(5-87)
High Temperature Measurement Technology for Main Combustion Chamber of Aeroengine…………………………………………………………………………………WANG Ming-rui,WANG Zhen-hua,HAN Bing,LI Ya-juan,GE Xin(5-87)
航空發(fā)動(dòng)機(jī)火焰筒矩形點(diǎn)焊換段修理技術(shù)研究…………………………………………………………………………梁鍵,趙海,許勇剛(5-94)
Technology Studyon Section-Change Repair with Rectangular Spot Welding of Combustor Liner for Aeroengine………………………………………………………………………………………………………………LIANG Jian,ZHAO Hai,XU Yong-gang(5-94)
1 種葉片氣膜冷卻效果試驗(yàn)評(píng)估的新方法……………………………………………………………曹智順,王洪斌,張樹(shù)林,張聯(lián)合,徐曉利(6-61)
A New Method for Experimental Assessment of Film-Cooling Effectiveness for a Blade…………………………………………………………………CAO Zhi-shun,WANG Hong-bin,ZHANG Shu-lin,ZHANG Lian-he,XU Xiao-l(i6-61)
直射式噴嘴流動(dòng)特性的數(shù)值和試驗(yàn)研究……………………………………………………熊溢威,李鋒,高偉偉,羅衛(wèi)東,趙凱,王昌盛(6-68)
Numerical and Experimental Study of Flow Characteristic of Direct Sprayed Nozzle…………………………………………………………XIONG Yi-wei,LI Feng,GAO Wei-wei,LUO Wei-dong,ZHAO Kai,WANG Chang-sheng(6-68)
制造Manufacture
壓氣機(jī)葉片型面精密數(shù)控銑加工技術(shù)應(yīng)用研究…………………………………………………………………………陳亞莉,李美榮,宋成(4-93)
Investigation on Precision NC Milling Technology of Compressor Blade Surface……………………………CHEN Ya-li,LI Mei-rong,SONG Cheng(4-93)
保障Support
基于.NET的小型渦扇發(fā)動(dòng)機(jī)故障判讀系統(tǒng)設(shè)計(jì)與實(shí)現(xiàn)………………………………………………馬同玲,焦華賓,魯峰,朱鐵濱,余海生(1-92)
Design and Implement of Monitoringand Fault Diagnosis System for Small Turbofan Engine Based on.NET Plat form………………………………………………………………………………MA Tong-ling,JIAO Hua-bin,LU Feng,ZHU Tie-bin,YU Hai-sheng(1-92)
航空發(fā)動(dòng)機(jī)CCAR33-R2.75條款適航符合性驗(yàn)證方法……………………………………喬磊,李艷軍,曹愈遠(yuǎn),趙蘇陽(yáng),許振騰,汪雷(1-99)
Research on Airworthiness Certification Method of Aeroengine Complying with CCAR33-R2.75…………………………………………………………………QIAO Lei,LI Yan-jun,CAO Yu-yuan,ZHAO Su-yang,XU Zheng-teng,WANG Le(i1-99)
美國(guó)第6代戰(zhàn)斗機(jī)發(fā)動(dòng)機(jī)關(guān)鍵技術(shù)綜述…………………………………………………………………………………梁春華,索德軍,孫明霞(2-93)
A Review on the Key Technologies of the Sixth Generation Fighter Engines in the US…………LIANG Chun-hua,SUO De-jun,SUN Ming-xia(2-93)
AATE和ITEP計(jì)劃下的渦軸發(fā)動(dòng)機(jī)分階段研發(fā)綜述………………………………………………………………………………………肖蔓(2-98)
Review of Research and Development for Turboshaft Engine Based on AATE and ITEP Program………………………………………XIAO Man(2-98)
壓氣機(jī)轉(zhuǎn)子葉片葉根斷裂故障分析………………………………………………………………………………………………劉國(guó)庫(kù),劉冬(3-93)
Fracture Failure Analysis for Blade Root of Compressor……………………………………………………………………LIU Guo-ku,LIU Dong(3-93)
1 種發(fā)動(dòng)機(jī)自適應(yīng)模型的修正方法………………………………………………………………………………………楊天南,吳森,王征(3-98)
A Correction Method for Aeroengine Adaptive Model……………………………………………………YANG Tian-nan,WU Sen,WANG Zheng(3-98)
某型發(fā)動(dòng)機(jī)材料控制標(biāo)準(zhǔn)體系的研究建立………………………………………………………………………………王曄,王剛,滕佰秋(4-98)
Establishment of Material Control Standard System for an Aeroengine…………………………………WANG Ye,WANG Gang,TENG Bai-qiu(4-98)
基于層次分析法的民用客機(jī)發(fā)動(dòng)機(jī)技術(shù)評(píng)價(jià)與選型…………………………………………………………王鵬,陳迎春,司江濤,何必海(5-98)
Technology Evaluation and Choice of Civil Aircraft Engine Based on Analytic Hierarchy Process……………………………………………………………………………………………WANG Peng,CHEN Ying-chun,SI Jiang-tao,HE Bi-ha(i5-98)
民用航空發(fā)動(dòng)機(jī)型號(hào)合格審定方法研究………………………………………………………………………張麗娜,張建,李艷軍,曹愈遠(yuǎn)(6-76)
Research of Type Certification Method for Civil Aviation Engine………………………ZHANG Li-na,ZHANG Jian,LI Yan-jun,CAO YU-yuan(6-76)
美國(guó)戰(zhàn)斗機(jī)發(fā)動(dòng)機(jī)技術(shù)研究與產(chǎn)品研制的發(fā)展特點(diǎn)及趨勢(shì)分析……………………………………………索德軍,孫明霞,梁春華,梁彩云(6-82)
Review on Technical Investigation and Product Development of Fighter Engine in US…………………………………………………………………………………SUO De-jun,SUN Ming-xia,LIANG Chun-hua,LIANG Cai-yun(6-82)
航空發(fā)動(dòng)機(jī)技術(shù)成熟度評(píng)價(jià)方法應(yīng)用研究……………………………………………………………劉曉松,王桂華,劉慶東,賈淑芝,史妍妍(6-90)
Study of Technology Readiness Assessment Methods in the Development of Aeroengine………………………………………………………………………LIU Xiao-song,WANG Gui-hua,LIU Qing-dong,JIA Su-zhi,SHI Yan-yan(6-90)
航空發(fā)動(dòng)機(jī)風(fēng)車不平衡適航符合性驗(yàn)證…………………………………………………………………………………賈惟,何文博,劉帥(6-95)
Airworthiness Compliance Demonstration for Aeroengine Windmilling Imbalance ………………………………JIA Wei,HE Wen-bo,LIU Shua(i6-95)