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CAS IR Grid
机构
力学研究所 [3]
长春光学精密机械与物... [1]
宁波材料技术与工程研... [1]
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OAI收割 [5]
内容类型
期刊论文 [4]
会议论文 [1]
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2023 [1]
2022 [1]
2021 [1]
2016 [1]
2010 [1]
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Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster
期刊论文
OAI收割
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 4, 页码: 120-133
作者:
Guo, Yuntao
;
Sun, Wei
;
Sun, Zhenning
;
Wu, Zhiwen
;
He JW(贺建武)
  |  
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2023/06/15
Asymmetric performance
Direct thrust test
Ionic liquid electrospray thruster
Time of flight mass spec-trometry
Torsional thrust stand
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
作者:
Liu, Mingjiang
;
Sun, Mingbo
;
Zhao, Guoyan
;
Meng Y(孟宇)
;
Huang, Yuhui
  |  
收藏
  |  
浏览/下载:45/0
  |  
提交时间:2022/12/20
Tandem-cavity
Scramjet combustor
Combustion mode
Thrust performance
Effect of Pitch Error on Static and Dynamic Characteristics of Hydrostatic Worm-Rack-Drive
期刊论文
OAI收割
JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 2021, 卷号: 143, 期号: 11
作者:
Zhang, Yongtao
;
Liu, Yupeng
;
Deng, Junjun
;
Song, Rongxiang
;
Zhu, Yingdan
  |  
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2021/12/01
HYDRODYNAMIC LUBRICATION
SLIDING LEADSCREWS
JOURNAL BEARINGS
THRUST-BEARINGS
PERFORMANCE
FRICTION
MOTIONS
MODEL
PAD
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
OAI收割
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
作者:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2016/09/14
Dual-mode scramjet
Engine performance
Thrust
Optimization
Heat release distribution
Simulated annealing algorithm
Study on the azimuth bearing scheme of a large Alt-azimuth telescope (EI CONFERENCE)
会议论文
OAI收割
5th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Large Mirrors and Telescopes, April 26, 2010 - April 29, 2010, Dalian, China
作者:
Wang H.
;
Dai S.
;
Zhang J.
;
Wang H.
;
Zhang J.
收藏
  |  
浏览/下载:38/0
  |  
提交时间:2013/03/25
The azimuth bearing schemes in typical large Alt-azimuth telescopes
especially the 3.5-m APO telescope and the 4.1-m SOAR telescope were analyzed. A scheme of high-angular contacted thrust ball bearing integrated with a radial ball bearing was put forward. According to the Hertz contact theory
the corresponding parameters were designed for engineering application. The static performance parameters
within the range of 60 85 original contact angle were calculated. Compared with the traditional plane thrust ball bearing
the results shows that the high-angular (80) contact thrust ball bearing has more benefits at bearing strength and rigidity for large telescope. The 1500mm diameter prototyping bearing shows good performance
including the axial jitter is 0.009mm
the radial jitter is 0.006mm
the maximum starting torque without load is 30N·m
and the load capacity is more than 30t
which offers advanced technique path for the buildup of the high precision azimuth shafting and the whole telescope system. 2010 Copyright SPIE - The International Society for Optical Engineering.