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The Devil is in Details: Delving Into Lite FFN Design for Vision Transformers
会议论文
Seoul, Korea, 2024-4-14
作者:
Chen, Zhiyang
;
Zhu, Yousong
;
Li, Zhaowen
;
Yang, Fan
;
Zhao, Chaoyang
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2024/05/28
Vision Transformer
Light-Weight Structure
Feed-Forward Networks
Light-Weight Design Method for Force-Performance-Structure of Complex Structural Part Based Co-operative Optimization
期刊论文
CHINESE JOURNAL OF MECHANICAL ENGINEERING, 2018, 卷号: 31
作者:
Ma, Ya-Li
;
Tan, Jian-Rong
;
Wang, De-Lun
;
Liu, Zi-Zhe
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/02
Light-weight design
Part structure
Topology optimization
Size optimization
Force
Performance
Exceptional ring topology makes diamond allotropes as light-weight superhard materials
期刊论文
DIAMOND AND RELATED MATERIALS, 2017, 卷号: 80, 页码: 140-146
作者:
Chi, Baoqian[1]
;
Liu, Yi[2]
;
Li, Xiaowu[3]
;
Qin, Xuming[4]
;
Zhao, Xinluo[5]
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/04/24
Superhard carbon
Diamond-related materials
Light-weight structure materials
Ring topology
Density functional calculations
Wear Mechanism of Iron-based Alloy Coating by Arc Spraying
期刊论文
JOURNAL OF IRON AND STEEL RESEARCH INTERNATIONAL, 2016, 卷号: 23, 期号: 8, 页码: 834-841
作者:
Li Zengrong
;
Li Deyuan
;
Zhang Nannan
;
Huang He
;
Wang Xin
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2021/02/02
CARBIDE-FORMING ELEMENTS
CHROMIUM CAST-IRON
STEEL
BEHAVIOR
GLASS
iron-based coating
pore structure
wear resistance
engine cylinder block
light weight
Aluminum Lithium Alloys (Al-Li-Cu-X)-New Generation Material for Aerospace Applications
会议论文
International Conference on Advanced Materials and Sports Equipment Design, SINGAPORE, 2014-01-01
作者:
Ahmed, Bilal
;
Wu, Sujun
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
Aluminum-lithium alloys
Aerospace structure
Light weight
Young' modulus
Physical metallurgy
Study on ultra-light secondary baffle for coaxial two-mirror telescope (EI CONFERENCE)
会议论文
2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China
Zhang L.
;
Jia X.
;
Xie P.
;
Xing L.
收藏
  |  
浏览/下载:50/0
  |  
提交时间:2013/03/25
The coaxial two-mirror telescope consists of two mirrors facing each other. Classical two-mirror arrangements are Gregorian and Cassegrain. These systems are usually applied to space telescopes and often have optical baffles to prevent stray light from entering the focal plane. The optical baffles consist of concentric rings suspended between the secondary and the primary mirror. The secondary baffle for a large two-mirror optical system is designed and analyzed in this paper. According to mission of a telescope
the structure should have high stiffness and high reliability and light weight. Compared with invar
aluminum alloy and titanium alloy
carbon fiber composite is currently the best material in terms of weight-to-strength ratio. It also has advantages of high temperature tolerance and low thermal expansion. So carbon fiber composite is chosen as material to meet requirements of the coaxial telescope. In this paper
optimization method based on finite element analysis (FEA) is used for design the secondary baffle. Minimum weight of the baffle is chosen as an objective function. Thicknesses of former tube and vanes are chosen as variables. Analysis results show that the designed secondary baffle has maximum diameter of 180mm
total length of 120mm and weighs 142g. And its fundamental frequency reaches 651Hz. Therefore the baffle has many advantages
such as ultra-light weight
high stiffness and dimensional stability
etc. The optimization method and the baffle design can be helpful to other coaxial telescopes
such as Cassegrain
Gregorian and their subdivisions. 2012 IEEE.
Application of carbon fibre reinforced plastic for optical camera structure (EI CONFERENCE)
会议论文
2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China
An Y.
;
Yao J.-S.
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  |  
浏览/下载:15/0
  |  
提交时间:2013/03/25
Optical camera is a high-precision optical instrument
and the optical lens must be always stable under various environments
so the structural materials of optical camera should have good stability and machining performance characteristics. Generally
the weight of the camera increases with the increasing size of optical camera aperture. The application of carbon fibre reinforced plastic(CFRP) in optical camera can help to improve the situation and meet the requirements of large volume and light weight. In this paper
the properties of several kind of materials used in camera structure were compared
the advantages of CFRP used in optical camera were analyzed
the CFRP application profiles of domestic and international were introduced
and the reason of gap was pointed out. There is a conclusion that CFRP will be widely used in the optical camera in China. 2012 IEEE.
Preliminary research on seismic behavior of low-rise light-weight residential buildings with composite wall
期刊论文
Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2012, 卷号: 44, 期号: SUPPL.1, 页码: 313-316
作者:
Shi, Yan-Li
;
Wang, Wen-Da
;
Jin, Yao
;
Zhang, Peng-Peng
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/11/14
Behavioral research
Earthquakes
Elastoplasticity
Housing
Rare earths
Seismic waves
Stiffness
Thin walled structures
Cold formed thin-walled steels
Dynamic time history analysis
Elastic-plastic dynamics
Low-rise light-weight steel structure buildings
Material nonlinear
Residential building
Seismic Performance
Structural systems
The structure design and analysis of predigest laser combine bind and extend bind flat roof (EI CONFERENCE)
会议论文
2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011, July 29, 2011 - July 31, 2011, Sanya, China
Han X.
;
Wang B.
;
Shi K.
;
Liu C.
;
Wang H.
;
Chen Z.
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2013/03/25
This paper put forward a kind of predigest laser combine bind and extend bind flat roof structure
which is founded as fission flat roof
and can be built in an little room 1280mm990mm815mm. This flat roof space location can be adjusted. This kind of seat can ensure the system complete laser combine and close as high precision. In this paper we designed the laser combine and close whole structure and install design. At last we did some finite statics analysis to some important parts. This design can ensure every laser fire directional adjust mete lower 30'
and the flat roof quality is 770kg. The transition benchmark flat roof system most meet and emergency is 0.005mm at the premise of bear the weight of turn flat laden. It can be seen that this structure can satisfy the request of many lasers small space laser extend bind and adjust. This kind can be extended to other light combine bind and extend bind structure design. (2011) Trans Tech Publications
Switzerland.
Structure optimization of strap-down inertial navigation system support (EI CONFERENCE)
会议论文
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
Sun H.
;
Jia H.
;
Wang J.
;
Hao X.
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/03/25
In order to meet the requirement of inertial navigation components and minimizing the system's weight
and topological optimization was conducted. Then
topological optimization and size optimization were conducted under conditions of random vibration and impact. Firstly
according to the dynamic characteristics of missile and requirement of inertial navigation system
the structure of inertial navigation support was designed according to types of missile connection and space arrangement of electronic components
the method of transforming multi-loading cases to multi-loading constraints was used to optimizing the size of the support under conditions of random vibration and impact. Comparing to the original support structures
RMS accelerations in installed points reduced by 25.2% under random vibration
the weight of optimal structures reduced by 28.1%
the structures also met the requirement of inertial navigation system under condition of impact. The support structure shows improvements in both dynamic characteristic and light weight comparing with the original one. 2011 IEEE.
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