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金属研究所 [4]
长春光学精密机械与物... [2]
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期刊论文 [8]
会议论文 [2]
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Advances in Flexible Robotic Manipulator Systems - Part II: Planning, Control, Applications, and Perspectives
期刊论文
OAI收割
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2024, 页码: 10
作者:
Li, Bai
;
Li, Xinyuan
;
Gao, Hejia
;
Wang, Fei-Yue
  |  
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2024/07/03
Planning
Vibrations
Trajectory
Uncertainty
Neural networks
End effectors
Splines (mathematics)
Artificial intelligence
flexible material
flexible robotic manipulator
vibration suppression
Flexible SiC nanowire aerogel with excellent thermal insulation properties
期刊论文
OAI收割
CERAMICS INTERNATIONAL, 2022, 卷号: 48, 期号: 15, 页码: 22172-22178
作者:
Liang, Xianpeng
;
Shao, Zhuojie
;
Wu, Zhen
;
Wang, Jingyang
  |  
收藏
  |  
浏览/下载:54/0
  |  
提交时间:2022/09/16
SiC Nanowire aerogel
Freeze-drying
High temperature resistance
Flexible
Thermal insulation material
A new model based on the in-plane deformation for the conformal piezoelectric systems for characterization of soft tissue modulus
期刊论文
OAI收割
EXTREME MECHANICS LETTERS, 2022, 卷号: 55, 页码: 7
作者:
Zhao HY(赵宏宇)
;
Dagdeviren, Canan
;
Liu GD(刘国栋)
;
Cao, Peng
;
Wang, Jianru
  |  
收藏
  |  
浏览/下载:45/0
  |  
提交时间:2022/12/26
Skin modulus
Flexible electronics
Piezoelectric material
Actuator and sensor
Stress release in high-capacity flexible lithium-ion batteries through nested wrinkle texturing of graphene
期刊论文
OAI收割
JOURNAL OF ENERGY CHEMISTRY, 2021, 卷号: 61, 页码: 243-249
作者:
Chen, Jing
;
Wen, Lei
;
Fang, Ruopian
;
Wang, Da-Wei
;
Cheng, Hui-Ming
  |  
收藏
  |  
浏览/下载:50/0
  |  
提交时间:2021/10/15
Wrinkling graphene
Structural design
Stress release
High-capacity active material
Flexible electrodes
Flexible and Tunable Dielectric Color Meta-hologram
期刊论文
OAI收割
PLASMONICS, 2020, 卷号: 15, 期号: 1, 页码: 217-223
作者:
Guo, Xiaoyi
;
Pu, Mingbo
;
Guo, Yinghui
;
Ma, Xiaoliang
;
Li, Xiong
  |  
收藏
  |  
浏览/下载:33/0
  |  
提交时间:2021/05/11
Hologram
Flexible Material
Color Tunable
Metasurface
Asymmetric Hybrid Capacitor Based on NiCo2O4 Nanosheets Electrode
期刊论文
OAI收割
ACTA PHYSICO-CHIMICA SINICA, 2020, 卷号: 36, 期号: 7
作者:
Tong Yongli
;
Dai Meizhen
;
Xing Lei
;
Liu Hengqi
;
Sun Wanting
  |  
收藏
  |  
浏览/下载:31/0
  |  
提交时间:2021/02/02
FLEXIBLE CARBON-FIBERS
HIGH-PERFORMANCE
ENERGY-STORAGE
SUPERCAPACITOR ELECTRODES
NANONEEDLE ARRAYS
PHOTOCATALYSTS
TRANSITION
NANORODS
NI
NiCo2O4 nanosheet
Electrochemical performance
Asymmetrical supercapacitor
Cathode material
Cycle stability
Targeted design, analysis and experimental characterization of flexible microwave absorber for window application
期刊论文
OAI收割
MATERIALS & DESIGN, 2019, 卷号: 162, 页码: 119
作者:
Deng, Ruixiang
;
Zhang, Ke
;
Li, Meiling
;
Song, Lixin
;
Zhang, Tao
  |  
收藏
  |  
浏览/下载:60/0
  |  
提交时间:2019/12/26
Microwave absorber
Design method
Window material
Wideband
Flexible
A Self-Standing and Flexible Electrode of Li4Ti5O12 Nanosheets with a N-Doped Carbon Coating for High Rate Lithium Ion Batteries
期刊论文
OAI收割
Advanced Functional Materials, 2013, 卷号: 23, 期号: 43, 页码: 5429-5435
N. Li
;
G. M. Zhou
;
F. Li
;
L. Wen
;
H. M. Cheng
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2014/02/19
flexible electrode
Li4Ti5O12
lithium ion battery
nanosheets
anode material
performance
storage
spinel
paper
composite
insertion
capacity
nanocomposite
architectures
Design and test of pointing mirror assembly for spaceborne remote sensing camera (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
作者:
Chen W.
收藏
  |  
浏览/下载:35/0
  |  
提交时间:2013/03/25
In order to ensure the surface figure of the pointing mirror (460mm long
290mm wide) in spaceborne remote sensing camera
Silicon Carbide was selected as the mirror material. The form of composite triangular and rectangular and the combination of open and closed back was explored in the lightweight design. A new kinematic mount and flexible structure in axis is used to hold the mirror around the lateral surface. The structure can minimize distortions induced by coefficient of thermal expansion mismatch among the materials. This eliminates the bending of the integral mount under the weight of the mirror. Optical performance of the mirror was analyzed under gravity load and temperature load using finite element method. Predicted surface figure error based on the removal of bias
tilt and power was calculated using an in-house Matlab script for mirrors. The pointing mirror assembly was tested using open loop servo control. And the surface figure was checked using interferometer. Surface figure accuracy is better than 1/30 ( 632.8nm
rms). The results show that the kinematic mount induces minimal figure error on the optical surface. 2011 IEEE.
Thermal-structure analysis of supersonic dome based on three materials (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Jiang Z.
;
Ai X.
;
Wei Q.
;
Liu B.
;
Jia H.
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2013/03/25
To a supersonic missile
a seeker could enhance the aerodynamic ability due to decrease the resistance in flying. At the same time
the primary function of a seeker has been considered as the most important equipment for a missile
due to the importance for cueing of targets and tracking for the final approach. However
the dome of a seeker
which is made up of glass
has poor mechanical performance. Especially
in the higher altitude
for a dome
in which the aerothermal and pressure loads could destroy the structure easily
it is necessary to do the thermal-structure coupled analysis due to varied materials. In the paper
to take the spherical dome of a seeker as a example
the analysis has been completed according to the varied materials consist of MgF2
Al2O3 and ZnS. The temperature loads and the pressure loads derived from the results of fluent analysis has been forced on the surface of dome
which simulates the actual Mach 2.5 in flying. According to the results of coupled analysis
the SEQV stress of the dome radium 80mm based on three materials had reached to 31MPa
which shows that the strength is sufficient for Mach 2.5
and offered the warranty to design the attaching to missile for the dome. At the same time
the results required the flexible mounting for the dome due to the displacements results
which the crystal material couldn't accept. 2011 IEEE.