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Structural dynamic analysis of the orbiting scroll wrap in the scroll compressor
Yicai LIU, Yubo XIA, Peng YAN, Yinbin LI, Haibo XIE
《能源前沿(英文)》 2013年 第7卷 第1期 页码 19-25 doi: 10.1007/s11708-012-0223-9
关键词: scroll compressor orbiting scroll wrap model analysis harmonic analysis
Analysis of a 1 kW organic Rankine cycle using a scroll expander for engine coolant and exhaust heat
Yiji LU, Anthony Paul ROSKILLY, Long JIANG, Longfei CHEN, Xiaoli YU
《能源前沿(英文)》 2017年 第11卷 第4期 页码 527-534 doi: 10.1007/s11708-017-0516-0
关键词: organic Rankine cycle scroll expander coolant and exhaust recovery internal combustion engine
Application of high-turning bowed compressor stator to redesign of highly loaded fan stage
LI Shaobin, SU Jiexian, WANG Zhongqi
《能源前沿(英文)》 2008年 第2卷 第4期 页码 534-540 doi: 10.1007/s11708-008-0066-6
关键词: off-design different numerical contouring technique high-performance compressor
Centrifugal compressor blade optimization based on uniform design and genetic algorithms
SHU Xinwei, GU Chuangang, XIAO Jun, GAO Chuang
《能源前沿(英文)》 2008年 第2卷 第4期 页码 453-456 doi: 10.1007/s11708-008-0083-5
关键词: information computational centrifugal compressor regression analysis CFD
Performance analysis of a centrifugal compressor with variable inlet guide vanes
XIAO Jun, GU Chuangang, SHU Xinwei, GAO Chuang
《能源前沿(英文)》 2007年 第1卷 第4期 页码 473-476 doi: 10.1007/s11708-007-0070-6
关键词: performance numerical simulation performan centrifugal compressor
Discussion on back-to-back two-stage centrifugal compressor compact design techniques
Lei HUO, Huoxing LIU
《机械工程前沿(英文)》 2013年 第8卷 第4期 页码 390-400 doi: 10.1007/s11465-013-0278-2
Design a small flow back-to-back two-stage centrifugal compressor in the aviation turbocharger, the compressor is compact structure, small axial length, light weighted. Stationary parts have a great influence on their overall performance decline. Therefore, the stationary part of the back-to-back two-stage centrifugal compressor should pay full attention to the diffuser, bend, return vane and volute design. Volute also impact downstream return vane, making the flow in circumferential direction is not uniformed, and several blade angle of attack is drastically changed in downstream of the volute with the airflow can not be rotated to required angle. Loading of high-pressure rotor blades change due to non-uniformed of flow in circumferential direction, which makes individual blade load distribution changed, and affected blade passage load decreased to reduce the capability of work, the tip low speed range increases.
关键词: back-to-back two-stage centrifugal compressor design Internal flow
Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row
JIANG Jian, LIU Bo, WANG Yangang, NAN Xiangyi
《能源前沿(英文)》 2008年 第2卷 第3期 页码 320-325 doi: 10.1007/s11708-008-0041-2
关键词: simulation compressor multistage third-order three-dimensional turbulent
LIU Xiaojia, NING Fangfei
《能源前沿(英文)》 2008年 第2卷 第4期 页码 541-549 doi: 10.1007/s11708-008-0077-3
关键词: definition objective distribution fitting precision combination numerical aerodynamic
Impact analysis of compressor rotor blades of an aircraft engine
Y B SUDHIR SASTRY, B G KIROS, F HAILU, P R BUDARAPU
《结构与土木工程前沿(英文)》 2019年 第13卷 第3期 页码 505-514 doi: 10.1007/s11709-018-0493-3
关键词: axial flow compressor rotor and stator blades aircraft engine stress and impact analysis aluminum alloys
Performance of rolling piston type rotary compressor using fullerenes (C70) and NiFe
Ruixiang WANG,Yihao ZHANG,Yi LIAO
《能源前沿(英文)》 2020年 第14卷 第3期 页码 644-648 doi: 10.1007/s11708-017-0453-y
关键词: rotary compressor friction coefficient nanocomposite materials coefficient of performance fullerenes (C70)
Optimal ratio of bend channel in centrifugal compressor
WEN Suping, HU Xiaowen, LI Tingbin, ZHANG Yong, WANG Jun
《能源前沿(英文)》 2008年 第2卷 第4期 页码 381-385 doi: 10.1007/s11708-008-0084-4
关键词: specific compressor different centrifugal compressor pressure impeller
Aerodynamic performance of bowed compressor cascades with different camber angles
CHEN Shaowen, CHEN Fu, WANG Keli, GU Jun, WANG Zhongqi
《能源前沿(英文)》 2008年 第2卷 第3期 页码 306-312 doi: 10.1007/s11708-008-0056-8
《能源前沿(英文)》 2022年 第16卷 第6期 页码 1000-1016 doi: 10.1007/s11708-021-0746-z
关键词: inlet air temperature inlet guide vane (IGV) opening part-load equilibrium running line gas turbine (GT) efficiency surge margin (SM)
Damage mechanism and evaluation model of compressor impeller remanufacturing blanks: A review
Haiyang LU, Yanle LI, Fangyi LI, Xingyi ZHANG, Chuanwei ZHANG, Jiyu DU, Zhen LI, Xueju RAN, Jianfeng LI, Weiqiang WANG
《机械工程前沿(英文)》 2019年 第14卷 第4期 页码 402-411 doi: 10.1007/s11465-019-0548-8
关键词: remanufacturing centrifugal compressor impeller remanufacturing blank damage mechanism evaluation model
Haizheng DANG, Dingli BAO, Zhiqian GAO, Tao ZHANG, Jun TAN, Rui ZHA, Jiaqi LI, Ning LI, Yongjiang ZHAO, Bangjian ZHAO
《能源前沿(英文)》 2019年 第13卷 第3期 页码 450-463 doi: 10.1007/s11708-018-0569-8
关键词: single-compressor-driven three-stage Stirling-type pulse tube cryocooler theoretical modeling experimental verification
标题 作者 时间 类型 操作
Structural dynamic analysis of the orbiting scroll wrap in the scroll compressor
Yicai LIU, Yubo XIA, Peng YAN, Yinbin LI, Haibo XIE
期刊论文
Analysis of a 1 kW organic Rankine cycle using a scroll expander for engine coolant and exhaust heat
Yiji LU, Anthony Paul ROSKILLY, Long JIANG, Longfei CHEN, Xiaoli YU
期刊论文
Application of high-turning bowed compressor stator to redesign of highly loaded fan stage
LI Shaobin, SU Jiexian, WANG Zhongqi
期刊论文
Centrifugal compressor blade optimization based on uniform design and genetic algorithms
SHU Xinwei, GU Chuangang, XIAO Jun, GAO Chuang
期刊论文
Performance analysis of a centrifugal compressor with variable inlet guide vanes
XIAO Jun, GU Chuangang, SHU Xinwei, GAO Chuang
期刊论文
Discussion on back-to-back two-stage centrifugal compressor compact design techniques
Lei HUO, Huoxing LIU
期刊论文
Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row
JIANG Jian, LIU Bo, WANG Yangang, NAN Xiangyi
期刊论文
New response surface model and its applications in aerodynamic optimization of axial compressor blade
LIU Xiaojia, NING Fangfei
期刊论文
Impact analysis of compressor rotor blades of an aircraft engine
Y B SUDHIR SASTRY, B G KIROS, F HAILU, P R BUDARAPU
期刊论文
Performance of rolling piston type rotary compressor using fullerenes (C70) and NiFe
Ruixiang WANG,Yihao ZHANG,Yi LIAO
期刊论文
Optimal ratio of bend channel in centrifugal compressor
WEN Suping, HU Xiaowen, LI Tingbin, ZHANG Yong, WANG Jun
期刊论文
Aerodynamic performance of bowed compressor cascades with different camber angles
CHEN Shaowen, CHEN Fu, WANG Keli, GU Jun, WANG Zhongqi
期刊论文
Improvement of part-load performance of gas turbine by adjusting compressor inlet air temperature and
期刊论文
Damage mechanism and evaluation model of compressor impeller remanufacturing blanks: A review
Haiyang LU, Yanle LI, Fangyi LI, Xingyi ZHANG, Chuanwei ZHANG, Jiyu DU, Zhen LI, Xueju RAN, Jianfeng LI, Weiqiang WANG
期刊论文