机构

• 工程热物理研究所 [8]
• 长春光学精密机械与物... [4]
• 广州能源研究所 [1]

采集方式

• OAI收割 [13]

内容类型

• 期刊论文 [9]
• 会议论文 [4]

发表日期

• 2019 [1]
• 2015 [1]
• 2014 [1]
• 2013 [1]
• 2012 [4]
• 2011 [2]
• 更多

学科主题

筛选

浏览/检索结果: 共13条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 A solar-assisted double absorption heat transformer: Off-design performance and optimum control strategy 期刊论文  OAI收割 ENERGY CONVERSION AND MANAGEMENT, 2019, 卷号: 196, 页码: 614-622 作者:  Wang, Hanzhi;  Li, Huashan;  Wang, Lingbao;  Bu, Xianbiao;  Zeng, Jie   |  收藏  |  浏览/下载：31/0  |  提交时间：2020/10/29 Solar thermal system  Double absorption heat transformer  Off-design performance  Optimization  Control strategy   Steady-state off-design thermodynamic performance analysis of a SCCP system 期刊论文  OAI收割 APPLIED THERMAL ENGINEERING, 2015, 卷号: 90, 页码: 221-231 作者:  Xu, Yu-jie;  Zhang, Shi-jie;  Chi, Jin-ling;  Xiao, Yun-han 收藏  |  浏览/下载：38/0  |  提交时间：2016/03/09 SCCP  Micro gas turbine  Absorption chiller  Cooling tower  Off-design performance   The exergy and energy level analysis of a combined cooling, heating and power system driven by a small scale gas turbine at off design condition 期刊论文  OAI收割 APPLIED THERMAL ENGINEERING, 2014, 卷号: 66, 期号: 1-2, 页码: 590-602 作者:  Chen, Qiang;  Han, Wei;  Zheng, Jian-jiao;  Sui, Jun;  Jin, Hong-guang 收藏  |  浏览/下载：58/0  |  提交时间：2015/12/10 CCHP system  Off-design performance  Energy level analysis  Exergy  Distributed energy system   Triple cycle for solar thermal power system adapted to periods with varying insolation 期刊论文  OAI收割 ENERGY, 2013, 卷号: 60, 页码: 129-138 作者:  Peng, Shuo;  Hong, Hui;  Jin, Hongguang 收藏  |  浏览/下载：32/0  |  提交时间：2015/10/23 Triple cycle  Solar gas turbine  Steam Rankine cycle  Kalina cycle  Off-design performance   Energy and exergy analyses on the off-design performance of an absorption heat transformer 期刊论文  OAI收割 Applied Thermal Energineering, 2012, 卷号: 48, 期号: *, 页码: 506-514 作者:  Guo, Peijun;  Sui, Jun;  Han W(韩巍);  Zheng, Jianjiao;  Jin, Hongguang 收藏  |  浏览/下载：28/0  |  提交时间：2016/02/05 Absorption heat transformer  Off-design performance  Vertical falling film  Energy  Exergy   Design and fabrication of imaging optical systems with freeform surfaces (EI CONFERENCE) 会议论文  OAI收割 Current Developments in Lens Design and Optical Engineering XIII, August 13, 2012 - August 15, 2012, San Diego, CA, United states 作者:  Zhang F.;  Wang L.;  Wang L.;  Wang L.;  He X. 收藏  |  浏览/下载：33/0  |  提交时间：2013/03/25 Freeform surfaces provide more degrees of freedom for design of optical systems  and enhance the ability of compensation and correction aberrations. Freeform surfaces are of advantage to balance the unsymmetrical aberrations  especially for the wide-field off-axis optical systems. This paper focus on an off-axis reflective optical system  which focal length is 550mm  F# is 6.5 and field of view (FOV) is 76. The system adopts some freeform surfaces. We discuss the problems we noticed in processes of design  manufacture  measurement and alignment  and the solutions. At last  the periodical research result and the expected performance are given. 2012 SPIE.   Aircraft flight simulation with landing gear based on multi-domain modeling technology (EI CONFERENCE) 会议论文  OAI收割 2012 2nd International Conference on Computer Application and System Modeling, ICCASM 2012, July 27, 2012 - July 29, 2012, Shenyang, China 作者:  Li M. 收藏  |  浏览/下载：16/0  |  提交时间：2013/03/25 This paper create a full aircraft flight simulation model for accurately analyzing the performance and influence of landing gear system. The use of multi-domain modeling technology enables detailed modeling of the flight dynamic and landing gear dynamic. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is actual in the physical process. The parameter design space is easily searched by considering a number of different landing scenarios to optimize the design. the authors.   Performance Back-deduction from a Loading to Flow Coefficient Map:Application to Radial Turbine 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 6, 页码: 509,517 Xavier CARBONNEAU; Nicolas BINDER 收藏  |  浏览/下载：12/0  |  提交时间：2013/04/27 Radial turbine  off-design  flow coefficient  load coefficient  performance   Establishment of airplane flight model and simulation analysis of landing behavior (EI CONFERENCE) 会议论文  OAI收割 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China 作者:  Li L.;  Li M. 收藏  |  浏览/下载：25/0  |  提交时间：2013/03/25 This paper create a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation for accurately analyzing the performance and influence of landing gear system. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic  aerodynamic  landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first  to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is actual in the physical process. 2011 IEEE.   Aircraft landing gear simulation using multidomain modeling technology (EI CONFERENCE) 会议论文  OAI收割 2011 International Conference on Information Technology, Computer Engineering and Management Sciences, ICM 2011, September 24, 2011 - September 25, 2011, Nanjing, Jiangsu, China 作者:  Li M. 收藏  |  浏览/下载：40/0  |  提交时间：2013/03/25 In order to accurately analyze the performance and influence of landing gear system  this paper presents a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic  aerodynamic  landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first  to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is improve the precision of flight simulation. 2011 IEEE.