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

113 篇 会议
10 篇 期刊文献

馆藏范围

123 篇 电子文献
0 种 纸本馆藏

日期分布

学科分类号

88 篇 工学
- 51 篇 航空宇航科学与技...
- 19 篇 机械工程
- 18 篇 控制科学与工程
- 15 篇 计算机科学与技术...
- 14 篇 力学（可授工学、理...
- 14 篇 软件工程
- 13 篇 电气工程
- 11 篇 电子科学与技术（可...
- 9 篇 仪器科学与技术
- 9 篇 交通运输工程
- 9 篇 安全科学与工程
- 8 篇 土木工程
- 6 篇 动力工程及工程热...
- 6 篇 生物工程
- 5 篇 信息与通信工程
- 5 篇 建筑学
- 5 篇 化学工程与技术
- 4 篇 冶金工程
- 3 篇 材料科学与工程（可...
- 2 篇 光学工程
31 篇 理学
- 13 篇 物理学
- 10 篇 数学
- 6 篇 生物学
- 5 篇 大气科学
- 4 篇 统计学（可授理学、...
- 3 篇 系统科学
10 篇 管理学
- 9 篇 管理科学与工程(可...
- 6 篇 工商管理
4 篇 经济学
- 4 篇 应用经济学
1 篇 军事学

主题

9 篇 aircraft
7 篇 flight simulator...
5 篇 aircraft power s...
4 篇 accuracy
4 篇 atmospheric mode...
3 篇 cockpits (aircra...
3 篇 aircraft propuls...
3 篇 certification
3 篇 aircraft control
3 篇 aerospace electr...
2 篇 strain gages
2 篇 flight testing
2 篇 snow
2 篇 reverberation
2 篇 safety
2 篇 aerospace contro...
2 篇 hazards
2 篇 analytical model...
2 篇 aircraft hydraul...
2 篇 data models

机构

49 篇 state key labora...
14 篇 shanghai aircraf...
10 篇 state key labora...
9 篇 comac shanghai a...
6 篇 shanghai aircraf...
6 篇 shanghai aircraf...
5 篇 school of civil ...
5 篇 comac shanghai a...
4 篇 state key labora...
4 篇 state key labora...
3 篇 college of logis...
3 篇 state key labora...
3 篇 state key labora...
3 篇 state key labora...
3 篇 shanghai aircraf...
3 篇 shanghai aircraf...
2 篇 commercial aircr...
2 篇 shanghai aircraf...
2 篇 comac shanghai a...
2 篇 college of mathe...

作者

6 篇 wang hongxin
6 篇 yu liang
5 篇 chen wenjie
4 篇 dai zheng
4 篇 xie gangtao
4 篇 qu xiaoyu
4 篇 wenjie chen
4 篇 xu desheng
3 篇 min huang
3 篇 wang ran
3 篇 xie dianhuang
3 篇 zhou qiongyao
3 篇 hu xiaowei
3 篇 li tao
3 篇 jin jiangchen
3 篇 xiaowei hu
3 篇 chu ning
3 篇 huang min
3 篇 liu qianqian
3 篇 wang hao

语言

103 篇 英文
20 篇 其他

检索条件"机构=State Key Laboratory of Aircraft Systems Integration Technology and Flight Simulation"

共 123 条记录，以下是11-20 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：

THE DECOUPLING AND simulation ANALYSIS OF THE SIX-FORCE SENSORS STRUCTURE FOR aircraft WHEEL IN GROUND DYNAMIC TESTING

THE DECOUPLING AND SIMULATION ANALYSIS OF THE SIX-FORCE SENS...

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Jiang, Bo Li, Tao Shao, YiFan Shanghai Aircraft Design and Research Institute ofCOMAC State Key Laboratory of Airliner Integration Technology and Flight Simulation Shanghai China

To meet the needs of aircraft ground dynamics testing, a six-force sensors decoupling structure is designed and simulated for verification. The core unit is a six-force sensors with an elastic body structure composed of several strain beams. The six-force sensor adopts an eight-beam design, with four strain gauges attached to each beam. Through Abaqus simulation analysis, the structural design of the strain gauges enables partial decoupling of the six-forces. The undecoupled forces of the six-force are decoupled by constraining the rotational freedom of the sensor. By designing the structure of the six-force sensor and constraining its rotational freedom, the decoupling of each output channel can be achieved. © The Institution of Engineering & technology 2024.

关键词： Strain gages

来源：评论

学校读者我要写书评

暂无评论

Measurement uncertainty of vertical combustion test of civil aircraft interior materials 2

Measurement uncertainty of vertical combustion test of civil...

引用

2023 2nd International Conference on Aerospace and Control Engineering, ICoACE 2023

作者： Wu, Shuang State Key Laboratory of Airliner Integration Technology and Flight Simulation Shanghai Aircraft Design and Research Institute Shanghai200000 China

The civil cabin interior materials vertical combustion test is the necessary test to verify the flame retardancy ability of the floor coverings, textiles, seat cushions and cushions. It is an inspection step required for cabin interior materials before installation, which is of great significance for the safe flight of civil aircraft. During the experiment process, variable factors such as personnel and equipment are highly likely to impact the test results. To ensure the reliability of test results, it is necessary to summarize and evaluate the factors that may affect the results of the test process. Thus, in this paper, the test method, measurement model, and sources of measurement uncertainty have been analysed, and the calculation case of experimental measurement uncertainty has been introduced. © Published under licence by IOP Publishing Ltd.

关键词： Combustion

来源：评论

学校读者我要写书评

暂无评论

Test research for flap skew on iron bird on a certain type of aircraft

Test research for flap skew on iron bird on a certain type o...

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Wang, Xianyu State Key Laboratory of Airliner Integration Technology and Flight Simulation COMAC Shanghai Aircraft Design and Research Institute Shanghai China

This paper focuses on the flap skew test under the ground-based laboratory environment on the iron bird, taking a certain type of aircraft as an example to introduce the environment and skew malfunction principles about the flap skew test on aircraft. The mechanical devices used to simulate flap skew malfunction and recover flap skew malfunction are designed and applied in the ground simulation test of a certain type of aircraft. According to the results, the designed mechanism can be proved to be used normally and can carry out the flap skew test successfully. © The Institution of Engineering & technology 2024.

关键词： Iron research

来源：评论

学校读者我要写书评

暂无评论

Directional control law functional analysis and design for civil aircraft simulator

Directional control law functional analysis and design for c...

引用

2024 International Conference on Aerospace and Mechanics, ICAM 2024

作者： Xie, Gangtao Chen, Lei Qu, Xiaoyu Shanghai Aircraft Design and Research Institute Commercial Aircraft Corporation of China Ltd. Shanghai China State Key Laboratory of Aircraft Systems Integration Technology and Flight Simulation Shanghai China

Functional analyses of directional flight control law for a typical civil aircraft are conducted, including directional maneuver, rudder limiter, coordinated turn, Yaw Damper, Thrust Asymmetrical Compensation, Gust Alleviation, manual rudder trim, etc. Through inputs of doublet, step input, and sweeping frequency, open loop control characteristics are analyzed based on a linearized state-space matrix. Simulink block architecture of a closed-loop directional control law is constructed, aiming to fulfill flight control functions, including pedal-to-rudder control, Yaw Damper, coordinated turn, and gain-tuned rudder limiter. simulations for the previously designed closed-loop directional control law are performed to verify the characteristics of directional handling qualities in the aspect of the Yaw Damper, directional static and dynamic stability, maneuverability, and sweeping frequency. © 2024 Institute of Physics Publishing. All rights reserved.

关键词： Maneuverability

来源：评论

学校读者我要写书评

暂无评论

BASED ON THE SCENARIO ANALYSIS: THE RESEARCH OF AUXILIARY POWER UNIT (APU) SYSTEM REQUIREMENT DEMONSTRATION ON HIGH PLATEAUS

BASED ON THE SCENARIO ANALYSIS: THE RESEARCH OF AUXILIARY PO...

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Sun, Yuchen State Key Laboratory of Airliner Integration Technology and Flight Simulation Shanghai200126 China

When capturing the design requirements for civil aircraft, it is necessary to analyze them according to the requirements of ARP 4754A, based on the forward design principle of scenario combing. In this paper, the requirements for APU utilization are captured from the actual operation scenarios of civil aircraft at high plateaus in China[1]. For example, the utilization of APU needs to take into account the impact of plateau environments on its performance, such the altitude to start up on the ground and the altitude to provide bleed air,etc.[2-3] Different from plain aircraft, when operating at high plateau, APU s are usually used in takeoff and approaching phases to supplement engine thrust to obtain the performance *** article provides scenarios for using the APU during normal aircraft operation scenario and system failure scenario, and demonstrates the APU ground start height and air supply and bleed air height indicators based on the characteristics of high-altitude airports in China. © The Institution of Engineering & technology 2024.

关键词： Fighter aircraft

来源：评论

学校读者我要写书评

暂无评论

Design and Research of Advanced Test Equipment for Simulating the External Light Environment of aircraft Cockpit 3rd

Design and Research of Advanced Test Equipment for Simulatin...

引用

3rd International Conference on Intelligent systems Design and Engineering Applications, ISDEA 2024

作者： Guo, Weihong Xie, Shuge Wang, Hongxin Li, Tao Yuan, Xiaofeng LI, Mengxun Shanghai Aircraft Design and Research Institute Shanghai China State Key Laboratory of Airliner Integration Technology and Flight Simulation Shanghai China

ISBN: (纸本)9789819792429

A design method for an advanced external light environment simulation system is introduced. Firstly, the design requirements of the external light environment simulation system is analyzed, and the functions of the external light environment simulation system are summarized. Secondly, the design requirements for hardware simulation devices are analyzed. The hardware simulation devices include basic sky light environment simulation system, sun and moon environment simulation system, and specific extreme light environment simulation system. The typical parameter indicators of various simulators have been clearly proposed. Thirdly, the simulation algorithms and simulated scenes of this system are summarized. Then, a series of validation experiments were designed to demonstrate that the system has high uniformity and stability in luminescence. In the test, different luminance and color temperature were selected to form different experimental conditions, and test points were selected at different positions in the aircraft test cockpit, all of which showed good uniformity results. Finally, the design features of the external light environment simulation system were summarized, and the technical fields that this system could be applied to are introduced. © The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2024.

关键词： Cockpits (aircraft)

来源：评论

学校读者我要写书评

暂无评论

STUDY ON THE IMPACT OF APU INLET DOOR ANGLE ON AERODYNAMIC PERFORMANCE OF INLET SYSTEM

STUDY ON THE IMPACT OF APU INLET DOOR ANGLE ON AERODYNAMIC P...

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Zhu, Ting Zhou, Chengsi Wang, Runzhou Sha, Jingtian Wang, Han Chen, Yaxin Shanghai Aircraft Design and Research Institute Shanghai China State Key Laboratory of Airliner Integration Technology and Flight Simulation Shanghai China

The Auxiliary Power Unit (APU) of civil aircraft primarily provides generator shaft power for the electrical system and bleed air for the air source system both on the ground and in the air. The APU inlet system draws airflow from outside the fuselage through inlet duct and ventilation cooling duct, supplying the APU with the required airflow under various operating conditions and ensuring proper ventilation and cooling of the compartment. The inlet system also aims to minimize pressure loss and inlet distortion at the APU's entrance. This study uses numerical simulation to study the impact of APU inlet door angle on aerodynamic performance of inlet system. The results show that within the study range, under the flight condition,the total pressure recovery coefficient and the ram recovery coefficient of the APU inlet duct outlet first increase and then decrease with increasing inlet door angle,reaching maximum values at door angle of 40°;under the ground condition, the total pressure recovery coefficient of the APU inlet duct outlet continuously increase with larger door angles;The inlet door angle has no significant regular impact on the magnitude of APU inlet distortion. © The Institution of Engineering & technology 2024.

关键词： Ventilation ducts

来源：评论

学校读者我要写书评

暂无评论

Research on real time simulation test method of civil aircraft ground deceleration requirements validation

Research on real time simulation test method of civil aircra...

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Chen, Li Li, Linwen Xie, Dianhuang Wang, Hongxin COMAC Shanghai Aircraft Design & Research Institute Shanghai China State Key Laboratory of Airliner Integration Technology and Flight Simulation China

In view of the requirements of ground deceleration functional requirements and safety requirements validation during civil aircraft design, an automated ground deceleration test method based on distributed real-time simulation is proposed, which takes the functional logic model of ground deceleration related systems as the test infrastructure, develops test cases based on key parameters of ground deceleration requirements, develops automated test models and fault injection models based on test cases, and integrates automated test models, fault injection models and related system models to conduct distributed real-time simulation tests. The technology digitizes key parameters that need to be confirmed in ground deceleration requirements, effectively covers the scope of requirements confirmation by arranging combined parameter development test cases, simplifies the process of testing and requirements confirmation in the form of automated simulation testing, and efficiently supports aircraft ground deceleration requirements confirmation efforts. © The Institution of Engineering & technology 2024.

关键词： Automatic testing

来源：评论

学校读者我要写书评

暂无评论

Design of 5G ATG system for civil aircraft

Design of 5G ATG system for civil aircraft

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Tang, Zexian Shanghai Aircraft Design and research Institute Shanghai China State Key Laboratory of Airliner Integration Technology and Flight Simulation Shanghai China

The 5G ATG technology has been engineered to fulfill the civil aviation requirements for swift and reliable internet services. This article delves into the operational scenarios of 5G ATG, elucidating the principal constituents of the on-board 5G ATG system. It outlines the critical considerations for system development and the tests employed for system verification. © The Institution of Engineering & technology 2024.

关键词： 5G mobile communication systems

来源：评论

学校读者我要写书评

暂无评论

STUDY ON ICING ENVIROMENT OF TYPICAL CIVIL aircraft BOARDING GATE

STUDY ON ICING ENVIROMENT OF TYPICAL CIVIL AIRCRAFT BOARDING...

引用

2024 CSAA/IET International Conference on aircraft Utility systems, AUS 2024

作者： Zhu, Yifan Qiu, Xudong State Key Laboratory of Airliner Integration Technology and Flight Simulation COMAC Shanghai Aircraft Design and Research Institute Shanghai200126 China

In order to verify the compliance requirements of typical civil aircraft cabin doors to airworthiness provisions in cold weather, a high and low temperature experimental cabin was built with the boarding door as the research object. The freezing opening test of the cabin door's inner handle and outer handle was carried out by means of rain in a low temperature environment. It is found that the ice surface faults are orderly, there is no stuck and no noise during the test, the mechanism is intact, and the hatch door can be closed normally. The opening time of the inner handle after icing is 6.17 s, which meets the requirements of the airworthiness clause. The test results can provide a basis for the design index of the model gate under the icy environment. © The Institution of Engineering & technology 2024.

关键词： aircraft

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13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：