Hu Yanlin
Harbin Institute of Technology
28 Papers
38 Citations
Hu Yanlin is an academic researcher from Harbin Institute of Technology. The author has contributed to research in topics: Anode & Cathode. The author has an hindex of 4, co-authored 28 publications.
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Papers
Study of multi-cusped plasma thruster applied to Air-Breathing Electric Propulsion
TL;DR: In this article, a Multi-cusped field thruster MCFT-2139 is designed and a nitrogen ignition experiment is conducted to evaluate the feasibility of this technology, the thruster could operate in an extremely large power range from 6 × 10−2 W to 1.3 × 103 W.
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Influence of heating mode on life reliability of a hollow cathode heater
Zhongxi Ning,Liu Xiaoyu,Wang Yanan,Zhi-wei Zhao,Wang Fufeng,Hu Yanlin,Mao Wei,Yan Shen,Daren Yu +8 more
TL;DR: In this article, the authors compare multiple groups of constant voltage power supply mode (U mode) and traditional constant current power supply (I mode) for the same structural heater, and reliability analysis is performed using two-parameter Weibull distribution.
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Patent
Double-layer pore plate type gas distributor easy to assemble
Hu Yanlin,Mao Wei,Hu Dawei,Shen Yan,Chen Jun,Wu Peng'an,Shan Shihua,Zang Juanwei,Li Shengjun,Wu Yaowu +9 more
- 10 May 2017
TL;DR: In this paper, a double-layer pore plate type gas distributor is presented, which consists of a gas guiding column, a distributor base, a first-layer plate, a second-layer pipe, an outer baffle, an inner baffle and a fixing column.
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Measurement method for plume divergence angle of Hall thrusters
TL;DR: In this article, a torus-source model was established for error analysis of the plume divergence angle measurement with different measuring radii when the arc measurement method is adopted, and a corresponding correction method was proposed.
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Patent
Anode magnetic screen integrated structure for Hall thruster
Hu Yanlin,Mao Wei,Yang Jian,Geng Jinyue,Hu Dawei,Shen Yan,Chen Jun,Li Dong,Wei Fuzhi,Shan Shihua,Wu Peng'an,Wu Yaowu,Zang Juanwei,Li Shengjun,Zhou Lei,Xie Jixiang,Zhen Lipeng +16 more
- 03 Nov 2017
TL;DR: In this paper, an anode magnetic screen integrated structure for a Hall thruster is presented, where holes are evenly formed in the outer circle of the anode, with the largest maximum of anode having the gas homogenization effect, and the magnetically soft alloy material is adopted to achieve the magnetic conductive function, the magnet exciting coil manner is adopted in the magnetic source, the permanent magnet manner was adopted, and therefore building of an insulation acceleration channel of the Hall thrusters is achieved.
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