检索结果-内蒙古大学图书馆

您好，读者！请登录

内蒙古大学图书馆

首页
概况
党建
资源
服务
科研支持
- 论文收录引用证明
- 科技查新
知识产权
档案馆
帮助

咨询与建议

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

您的常用邮箱：*

您的手机号码：*

问题描述：

当前已输入0个字，您还可以输入200个字

全部搜索
期刊论文
图书
学位论文
标准
纸本馆藏
外文资源发现
数据库导航
超星发现

高级检索

时间限定

出版年份：

文献类型

图书期刊文献学位论文多媒体

馆藏选择

电子馆藏纸本馆藏

核心期刊

全部期刊 SCI 收录期刊 SSCI 收录期刊 EI 收录期刊 CSCD 收录期刊 CSSCI 收录期刊

语言

中文英文

文献类型

期刊文献图书学位论文标准纸本馆藏

帮助

文字说明：

T=题名（书名、题名），A=作者（责任者），K=主题词，P=出版物名称，PU=出版社名称，O=机构（作者单位、学位授予单位、专利申请人），L=中图分类号，C=学科分类号，U=全部字段，Y=年（出版发行年、学位年度、标准发布年）

检索规则说明：

AND代表“并且”；OR代表“或者”；NOT代表“不包含”；(注意必须大写,运算符两边需空一格)

检索范例：

范例一：(K=图书馆学 OR K=情报学) AND A=范并思 AND Y=1982-2016
范例二：P=计算机应用与软件 AND (U=C++ OR U=Basic) NOT K=Visual AND Y=2011-2016

分类表

所选分类

>> <<

限定检索结果

文献类型

215 篇 会议
35 篇 期刊文献

馆藏范围

250 篇 电子文献
0 种 纸本馆藏

日期分布

学科分类号

180 篇 工学
- 63 篇 航空宇航科学与技...
- 49 篇 机械工程
- 48 篇 电气工程
- 42 篇 动力工程及工程热...
- 40 篇 控制科学与工程
- 35 篇 计算机科学与技术...
- 30 篇 软件工程
- 29 篇 力学（可授工学、理...
- 20 篇 电子科学与技术（可...
- 18 篇 化学工程与技术
- 15 篇 交通运输工程
- 12 篇 材料科学与工程（可...
- 11 篇 信息与通信工程
- 8 篇 仪器科学与技术
- 8 篇 土木工程
- 8 篇 环境科学与工程（可...
- 7 篇 冶金工程
- 7 篇 石油与天然气工程
- 3 篇 光学工程
- 3 篇 生物工程
76 篇 理学
- 35 篇 物理学
- 32 篇 数学
- 15 篇 化学
- 6 篇 系统科学
- 5 篇 统计学（可授理学、...
- 3 篇 生物学
12 篇 管理学
- 11 篇 管理科学与工程(可...
1 篇 医学

主题

11 篇 aircraft
10 篇 permanent magnet...
7 篇 predictive model...
7 篇 permanent magnet...
6 篇 atmospheric mode...
5 篇 fault tolerance
5 篇 mathematical mod...
5 篇 torque
5 篇 stators
4 篇 rectifiers
4 篇 rotors
4 篇 valves
4 篇 switches
4 篇 permanent magnet...
4 篇 computational mo...
4 篇 synchronous moto...
4 篇 fault tolerant s...
4 篇 actuators
4 篇 maintenance
4 篇 finite element a...

机构

81 篇 aviation key lab...
25 篇 aviation key lab...
8 篇 nanjing engineer...
7 篇 nanjing engineer...
7 篇 fuel system depa...
7 篇 school of automa...
7 篇 school of aerona...
6 篇 the aviation ele...
6 篇 beijing universi...
5 篇 nanjing universi...
5 篇 college of astro...
5 篇 aviation key lab...
4 篇 department of co...
4 篇 aviation key lab...
4 篇 hangzhou institu...
4 篇 provincial key l...
4 篇 aviation key lab...
4 篇 avic jincheng na...
4 篇 national key lab...
4 篇 center for more-...

作者

11 篇 yaohua hu
11 篇 xi xiao
9 篇 hu yaohua
8 篇 shushu zhu
7 篇 yang yang
6 篇 pengfei zhang
6 篇 wang yangyang
6 篇 guangzhao luo
6 篇 weilin li
5 篇 xiaoping ouyang
5 篇 zhang pengfei
5 篇 meng fanxin
5 篇 fanxin meng
5 篇 zhu shushu
5 篇 xiao xi
5 篇 jiang fan
5 篇 gao zanjun
5 篇 tian qilong
4 篇 yeming yao
4 篇 ming cheng

语言

223 篇 英文
22 篇 其他
4 篇 中文

检索条件"机构=Aviation Key Laboratory of Science and Technology on Aero Utility System Integration"

共 250 条记录，以下是21-30 订阅

全选清除本页清除全部题录导出标记到"检索档案"

详细简洁

排序：

Functional simulation of the cabin pressure control system based on stateflow 3

Functional simulation of the cabin pressure control system b...

引用

2024 3rd International Conference on aerospace and Control Engineering, ICoACE 2024

作者： Wang, Yehao Meng, Fanxin Yang, Yonghui Wang, Shun Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Jiangsu Nanjing211106 China AVIC Nanjing Engineering Institute of Aircraft Systems Jiangsu Nanjing211106 China

The cabin pressure control system(CPCS) is an important part of the aircraft environmental control system. In the actual flight process, it needs to achieve different functions according to the working scene. In this paper, the architecture and working principle of the CPCS system are summarized, and the functions of the system are analyzed;the control logic of each function is designed and simulated by the Stateflow platform. The results show that the control logic and its transition constraints designed in this paper can meet the functional requirements of the system, and the dynamic response is rapid, which can be used for the cabin pressure control system of civil aircraft system function design and verification to provide a reference. © 2025 Institute of Physics Publishing. All rights reserved.

关键词： Aircraft control

来源：评论

学校读者我要写书评

暂无评论

Semi-Physical Simulation of EHA Electric Drive system 7

Semi-Physical Simulation of EHA Electric Drive System

引用

7th IEEE International Electrical and Energy Conference, CIEEC 2024

作者： Mi, ChangBao Zhao, ZhiWen Zhou, JingXing Avic Nanjing Engineering Institute of Aircraft Systems Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing China Hangzhou Institute of Technology Xidian University Xian China

ISBN: (纸本)9798350359558

Electro-hydrostatic actuator (EHA) electric drive system is commonly used in more electric aircraft (MEA) and can improve aircraft performance. This article designs a high-speed permanent magnet synchronous motor (PMSM) with a rated speed of 12,000 rpm for EHA. It establishes the design and system simulation of a semi-physical real-time simulation model based on the EHA electric drive model, verifying the normal operation of the EHA electric drive system's load spectrum. This provides a reliable basis for the highly integrated and high-performance design of the EHA system, thus improving the research and development efficiency. © 2024 IEEE.

关键词： More electric aircraft

来源：评论

学校读者我要写书评

暂无评论

Research on Fault-Tolerant Reconstruction technology for aerospace Electromechanical systems Based on CPLD 7

Research on Fault-Tolerant Reconstruction Technology for Aer...

引用

7th IEEE International Electrical and Energy Conference, CIEEC 2024

作者： Zhang, Xiaokai Zhao, ZhiWen Wei, Qian Liu, Chunqiang A Vic Nanjing Engineering Institute of Aircraft Systems Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing China Hangzhou Institute of Technology Xidian University Xian China

ISBN: (纸本)9798350359558

To address the high reliability requirements of aviation electromechanical control systems, this paper focuses on exploring control reconfiguration strategies for aviation electromechanical control systems. The article first establishes a reconfiguration strategy combining redundancy switching with robustness and adaptive capabilities for typical electromechanical control systems. Building upon this foundation, a fault-tolerant strategy is proposed specifically for the core controller of electromechanical control systems in aviation. © 2024 IEEE.

关键词： Fault tolerance

来源：评论

学校读者我要写书评

暂无评论

Robust Deadbeat Finite-Set Predictive Torque and Flux Control for PMSM with Dynamic Model

Robust Deadbeat Finite-Set Predictive Torque and Flux Contro...

引用

2023 IEEE International Conference on Predictive Control of Electrical Drives and Power Electronics, PRECEDE 2023

作者： Wang, Taoming Zhang, Mengbo Chen, Lijun Xiao, Xi Chen, Zhe Luo, Guangzhao Northwestern Polytechnical University School of Automation Xi'an China Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing China

ISBN: (纸本)9798350396867

Deadbeat finite-set predictive torque and flux control has the advantages of fast dynamic response and reduced computational burden, but the system robustness is still a challenge in real-time implementation. This paper presents a novel deadbeat finite-set predictive torque and flux control strategy with a modified dynamical predictive model for permanent magnet synchronous motor (PMSM) drives to improve the robustness against mismatched parameters. By establishing sensitivity functions, the robustness of the system can be digitally quantified. The torque and flux predictive models with dynamic weighting factors are proposed to minimize phase current distortions and torque tracking errors caused by parameter variations. Finally, the simulation results verify the improved robustness of the proposed method. © 2023 IEEE.

关键词： Model predictive control

来源：评论

学校读者我要写书评

暂无评论

The Simulation Analysis of a Control Strategy for the Multi-Cabin Helicopter Vapor Compression Cycle system with the Amesim

The Simulation Analysis of a Control Strategy for the Multi-...

引用

2022 CSAA/IET International Conference on Aircraft utility systems, AUS 2022

作者： Deng, Weishi Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing211106 China

ISBN: (数字)9781839537769

ISBN: (纸本)9781839537769

In order to improve the dynamic temperature regulation performances of a vapor compression cycle in multi-cabin helicopter, a control strategy is proposed and theoretically evaluated by using Amesim software. A model for a vapor compression cycle system of a certain type helicopter is established to verify this strategy. Dynamic response performances of the system when the cabin heat load sharply increases or decreases are studied. Results found that the target temperature can be controlled within ± 1 °C, which shows the system has a good dynamic response by using the strategy. © 2022 IET Conference Proceedings. All rights reserved.

关键词： Dynamic response

来源：评论

学校读者我要写书评

暂无评论

Research On Stability Characteristics Of Three-Wheel Refrigeration system

Research On Stability Characteristics Of Three-Wheel Refrige...

引用

2022 CSAA/IET International Conference on Aircraft utility systems, AUS 2022

作者： Zhou, Yue Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing211106 China

ISBN: (数字)9781839537769

ISBN: (纸本)9781839537769

Simulation on three-wheel refrigeration system is carried out, the result of which is compared with the existing research data. Further, the temperature disturbance characteristics of the system is analysed combined with the main system disturbance source. Simulation results indicate that the temperature or moisture of the bleed air or ram air disturbance brings changes of system outlet temperature, the degree of which agrees with the disturbance element. Meanwhile the bleed air pressure disturbance to the three-wheel refrigeration system influence is most intense. This paper provides reference for the design and optimization of the environmental control system. © 2022 IET Conference Proceedings. All rights reserved.

关键词： Environmental management

来源：评论

学校读者我要写书评

暂无评论

SIMULATION CALCULATION AND OPTIMIZATION OF AERIAL REFUELING OF AIRCRAFT FUEL system

SIMULATION CALCULATION AND OPTIMIZATION OF AERIAL REFUELING ...

引用

2024 CSAA/IET International Conference on Aircraft utility systems, AUS 2024

作者： Wang, Chenchen Wang, Yangyang Gu, Lixin AVIC Nanjing Engineering Institute of Aircraft Systems The Aviation Electromechanical System Integration of Aviation Science and Technology Key Laboratory Nanjing211106 China

In order to ensure that the initial design of the fuel system meets the requirements of aircraft aerial refueling and related standards, a simulation model of an aircraft fuel system was established based on the AMESim simulation platform. The aerial refueling process was calculated under given conditions, and the initial design of the fuel system is optimized based on the calculation results. Results showed that both the initial and optimized fuel systems meet the requirements for refueling time, and the requirements of electrostatic protection for the fuel flow rate inside the pipeline and inlet of the fuel tank during refueling. The optimized fuel system has a more similar refueling rate for each fuel tank and can effectively reduce the weight of fuel system's pipelines. The calculation results can provide guidance for the initial design of fuel system. © The Institution of Engineering & technology 2024.

关键词： Aircraft fuels

来源：评论

学校读者我要写书评

暂无评论

STUDY ON THE PERMEATION MECHANISM OF HOLLOW FIBER MEMBRANES

STUDY ON THE PERMEATION MECHANISM OF HOLLOW FIBER MEMBRANES

引用

2024 CSAA/IET International Conference on Aircraft utility systems, AUS 2024

作者： Zhou, Yu Wang, Yangyang Fuel System Department Nanjing Engineering Institute of Aircraft Systems AVIC Nanjing China The Aviation Electromechanical System Integration of Aviation Science and Technology Key Laboratory Nanjing China

After the fiber membrane material is determined, the aircraft is more concerned about the flow rate of nitrogen-rich gas under a certain nitrogen-rich gas (NEA) concentration, thereby determining the inerting time of the fuel tank. This paper mainly introduces the separation principle and related parameters of fiber membranes, as well as the types and separation performance of different fiber membranes. The asymmetric polyimide membrane, which is more commonly used in airborne nitrogen inerting, is used to verify the effects of different temperatures, pressures, and altitudes on the separation efficiency of the fiber membranes through experiments. The results of the research can provide a basis for the design of subsequent high-efficiency hollow fiber membranes. © The Institution of Engineering & technology 2024.

关键词： Nafion membranes

来源：评论

学校读者我要写书评

暂无评论

ARCHITECTURE DESIGN AND VERIFICATION OF INERT GAS DISTRIBUTION system

ARCHITECTURE DESIGN AND VERIFICATION OF INERT GAS DISTRIBUTI...

引用

2024 CSAA/IET International Conference on Aircraft utility systems, AUS 2024

作者： Wang, Yangyang Wang, Chenchen Fuel System Department Nanjing Engineering Institute of Aircraft Systems AVIC Nanjing China The Aviation Electromechanical System Integration of Aviation Science and Technology Key Laboratory Nanjing China

This study addresses the requirements for tank inerting and proposes application-oriented architectures for inert gas distribution system. Utilizing AMEsim, a multi-tank simulation model is constructed. The accuracy of the model was validated through experimental data,demonstrating its applicability for engineering calculations. Furthermore,the model was utilized to analyze both series and parallel schemes of the distribution system. Results suggest that the series scheme effectively reduces tank oxygen concentration, enhances system reliability and oxygen concentration uniformity, and achieves higher inert gas utilization rates with simplified pipeline arrangements. Consequently, we recommend adopting the series scheme for inert gas distribution system. These findings provide a basis for designing and optimizing inerting system. © The Institution of Engineering & technology 2024.

关键词： Tanks (containers)

来源：评论

学校读者我要写书评

暂无评论

Electromagnetic Design of a Six-Phase Low-Inertia Fault-Tolerant Permanent Magnet Synchronous Machine 7

Electromagnetic Design of a Six-Phase Low-Inertia Fault-Tole...

引用

7th IEEE International Electrical and Energy Conference, CIEEC 2024

作者： Zhou, Ziyu Sui, Yi Qiu, Xiaoying Zheng, Ping Ma, Hui School of Electrical Engineering and Automation Harbin Institute of Technology Harbin China Avic Nanjing Engineering Institute of Aircraft Systems Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration Nanjing China

ISBN: (纸本)9798350359558

Multiphase permanent magnet (PM) synchronous machine features the advantages of high reliability and high fault-tolerant capability, which has great potential in the fields like aviation servo and electric vehicles. In order to meet the design criteria of low moment of inertia and high post-fault torque performance, three different rotor structures are analyzed and compared for a low-inertia fault-tolerant permanent magnet synchronous machine(SLIFT-PMSM) by finite-element method. The influence of winding structure on torque performance is investigated, and the winding structure is optimized to improve the post-fault torque performance. The electromagnetic performance of the improved scheme is evaluated under both the normal and fault conditions. © 2024 IEEE.

关键词： Permanent magnets

来源：评论

学校读者我要写书评

暂无评论

没有更多数据了...

全选清除本页清除全部题录导出标记到“检索档案”

共25页 << < 1 2 3 4 5 6 7 8 9 10 > >>

检索报告对象比较合并检索0

隐藏清空

合并搜索

回到顶部

执行限定条件

内容：

评分：

请选择保存的检索档案：

请选择收藏分类：

订阅名称：

通借通还

温馨提示：

图书名称：

借书校区：

取书校区：

手机号码：

邮箱地址：

一卡通帐号：

电话和邮箱必须正确填写，我们会与您联系确认。

联系人：

所在院系：

联系邮箱：

联系电话：

内蒙古自治区呼和浩特市赛罕区大学西街235号邮编: 010021

建议与咨询 留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

请选择保存的检索档案： 新增检索档案 确定 取消

请选择收藏分类： 新增自定义分类 确定 取消

通借通还

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

请选择保存的检索档案：

请选择收藏分类：