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A high resolution and wide range valve for micronewton cold gas thrusters
Numerous scientific satellites require micronewton thrusters for compensating environmental disturbances. The mass flow control proportional valve plays a crucial role in precisely regulating the thrust. To meet the high resolution and wide range requirements of the thrusters, this paper introduces...
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Published in: | Review of scientific instruments 2024-02, Vol.95 (2) |
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creator | Zhang, Hao-Yuan Liu, Jian-Ping Hu, Shao-Gang Yin, Jin-Huan Zhong, Yuan Li, Zhu Yang, Shan-Qing |
description | Numerous scientific satellites require micronewton thrusters for compensating environmental disturbances. The mass flow control proportional valve plays a crucial role in precisely regulating the thrust. To meet the high resolution and wide range requirements of the thrusters, this paper introduces a novel proportional valve with two sets of independently controllable piezoelectric stack. One set of the piezo-stack is used to compensate the stroke loss of the valve core, mainly caused by the deformation of the valve seat. The valve sealing mechanism is carefully analyzed to reduce the stroke loss. Another set of the stack works as the primary actuator, enabling the high mass flow control resolution. Two sets of independently controlled piezoelectric stacks not only expand the range and improve the range ratio but also provide redundancy and enhance reliability. This means that the actuator can still operate at lower ranges even if one piezo-stack is damaged. The piezo-actuators are assembled using U-shaped connectors, creating a compact and space-efficient overall design. Experimental tests have been conducted to verify the performance of the valve, which demonstrated a mass flow range of 0–675 μg/s with a resolution better than 0.1 μg/s and a flow noise below 0.1 μg/s/Hz1/2 at 0.1 mHz–1 Hz. |
doi_str_mv | 10.1063/5.0175676 |
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The mass flow control proportional valve plays a crucial role in precisely regulating the thrust. To meet the high resolution and wide range requirements of the thrusters, this paper introduces a novel proportional valve with two sets of independently controllable piezoelectric stack. One set of the piezo-stack is used to compensate the stroke loss of the valve core, mainly caused by the deformation of the valve seat. The valve sealing mechanism is carefully analyzed to reduce the stroke loss. Another set of the stack works as the primary actuator, enabling the high mass flow control resolution. Two sets of independently controlled piezoelectric stacks not only expand the range and improve the range ratio but also provide redundancy and enhance reliability. This means that the actuator can still operate at lower ranges even if one piezo-stack is damaged. The piezo-actuators are assembled using U-shaped connectors, creating a compact and space-efficient overall design. Experimental tests have been conducted to verify the performance of the valve, which demonstrated a mass flow range of 0–675 μg/s with a resolution better than 0.1 μg/s and a flow noise below 0.1 μg/s/Hz1/2 at 0.1 mHz–1 Hz.</description><identifier>ISSN: 0034-6748</identifier><identifier>EISSN: 1089-7623</identifier><identifier>DOI: 10.1063/5.0175676</identifier><identifier>PMID: 38345452</identifier><identifier>CODEN: RSINAK</identifier><language>eng</language><publisher>United States: American Institute of Physics</publisher><subject>Cold gas ; Connectors ; Controllability ; Flow control ; High resolution ; Mass flow ; Piezoelectric actuators ; Piezoelectricity ; Pneumatics ; Redundancy ; Scientific satellites ; Thrusters ; Valve seats</subject><ispartof>Review of scientific instruments, 2024-02, Vol.95 (2)</ispartof><rights>Author(s)</rights><rights>2024 Author(s). 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The mass flow control proportional valve plays a crucial role in precisely regulating the thrust. To meet the high resolution and wide range requirements of the thrusters, this paper introduces a novel proportional valve with two sets of independently controllable piezoelectric stack. One set of the piezo-stack is used to compensate the stroke loss of the valve core, mainly caused by the deformation of the valve seat. The valve sealing mechanism is carefully analyzed to reduce the stroke loss. Another set of the stack works as the primary actuator, enabling the high mass flow control resolution. Two sets of independently controlled piezoelectric stacks not only expand the range and improve the range ratio but also provide redundancy and enhance reliability. This means that the actuator can still operate at lower ranges even if one piezo-stack is damaged. The piezo-actuators are assembled using U-shaped connectors, creating a compact and space-efficient overall design. Experimental tests have been conducted to verify the performance of the valve, which demonstrated a mass flow range of 0–675 μg/s with a resolution better than 0.1 μg/s and a flow noise below 0.1 μg/s/Hz1/2 at 0.1 mHz–1 Hz.</description><subject>Cold gas</subject><subject>Connectors</subject><subject>Controllability</subject><subject>Flow control</subject><subject>High resolution</subject><subject>Mass flow</subject><subject>Piezoelectric actuators</subject><subject>Piezoelectricity</subject><subject>Pneumatics</subject><subject>Redundancy</subject><subject>Scientific satellites</subject><subject>Thrusters</subject><subject>Valve seats</subject><issn>0034-6748</issn><issn>1089-7623</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNp90E1Lw0AQBuBFFFurB_-ALHhRIXW_N3ssxY9CwYuew3YzaVPSpO4mLf57N7R68OBc5vLwMvMidE3JmBLFH-WYUC2VVidoSElqEq0YP0VDQrhIlBbpAF2EsCZxJKXnaMBTLqSQbIhmE7wqlyvsITRV15ZNjW2d432ZA_a2XgLe2WoHuGg83pTONzXs24hcU-V4aQNuV74LLfhwic4KWwW4Ou4R-nh-ep--JvO3l9l0Mk8cF7xNnObC8TRepqhmC2vTHHROC2GMNWCYAyCpBa2cE7ooBCyEIFaYvBCUGSv4CN0dcre--ewgtNmmDA6qytbQdCFjhimiVUp6evuHrpvO1_G6XkkmudIkqvuDit-F4KHItr7cWP-VUZL1_WYyO_Yb7c0xsVtsIP-VP4VG8HAAwZWt7fv8J-0b8u2BNQ</recordid><startdate>20240201</startdate><enddate>20240201</enddate><creator>Zhang, Hao-Yuan</creator><creator>Liu, Jian-Ping</creator><creator>Hu, Shao-Gang</creator><creator>Yin, Jin-Huan</creator><creator>Zhong, Yuan</creator><creator>Li, Zhu</creator><creator>Yang, Shan-Qing</creator><general>American Institute of Physics</general><scope>NPM</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7X8</scope><orcidid>https://orcid.org/0000-0002-9672-2803</orcidid><orcidid>https://orcid.org/0000-0002-4440-2357</orcidid><orcidid>https://orcid.org/0009-0007-7424-2773</orcidid><orcidid>https://orcid.org/0000-0002-9934-1272</orcidid><orcidid>https://orcid.org/0009-0005-1123-814X</orcidid></search><sort><creationdate>20240201</creationdate><title>A high resolution and wide range valve for micronewton cold gas thrusters</title><author>Zhang, Hao-Yuan ; Liu, Jian-Ping ; Hu, Shao-Gang ; Yin, Jin-Huan ; Zhong, Yuan ; Li, Zhu ; Yang, Shan-Qing</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c343t-c734c380346172baa8de7d1f499a9e92cee08ae76cc47ff4eb440a49df4129a43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Cold gas</topic><topic>Connectors</topic><topic>Controllability</topic><topic>Flow control</topic><topic>High resolution</topic><topic>Mass flow</topic><topic>Piezoelectric actuators</topic><topic>Piezoelectricity</topic><topic>Pneumatics</topic><topic>Redundancy</topic><topic>Scientific satellites</topic><topic>Thrusters</topic><topic>Valve seats</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhang, Hao-Yuan</creatorcontrib><creatorcontrib>Liu, Jian-Ping</creatorcontrib><creatorcontrib>Hu, Shao-Gang</creatorcontrib><creatorcontrib>Yin, Jin-Huan</creatorcontrib><creatorcontrib>Zhong, Yuan</creatorcontrib><creatorcontrib>Li, Zhu</creatorcontrib><creatorcontrib>Yang, Shan-Qing</creatorcontrib><collection>PubMed</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>MEDLINE - Academic</collection><jtitle>Review of scientific instruments</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhang, Hao-Yuan</au><au>Liu, Jian-Ping</au><au>Hu, Shao-Gang</au><au>Yin, Jin-Huan</au><au>Zhong, Yuan</au><au>Li, Zhu</au><au>Yang, Shan-Qing</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A high resolution and wide range valve for micronewton cold gas thrusters</atitle><jtitle>Review of scientific instruments</jtitle><addtitle>Rev Sci Instrum</addtitle><date>2024-02-01</date><risdate>2024</risdate><volume>95</volume><issue>2</issue><issn>0034-6748</issn><eissn>1089-7623</eissn><coden>RSINAK</coden><abstract>Numerous scientific satellites require micronewton thrusters for compensating environmental disturbances. The mass flow control proportional valve plays a crucial role in precisely regulating the thrust. To meet the high resolution and wide range requirements of the thrusters, this paper introduces a novel proportional valve with two sets of independently controllable piezoelectric stack. One set of the piezo-stack is used to compensate the stroke loss of the valve core, mainly caused by the deformation of the valve seat. The valve sealing mechanism is carefully analyzed to reduce the stroke loss. Another set of the stack works as the primary actuator, enabling the high mass flow control resolution. Two sets of independently controlled piezoelectric stacks not only expand the range and improve the range ratio but also provide redundancy and enhance reliability. This means that the actuator can still operate at lower ranges even if one piezo-stack is damaged. The piezo-actuators are assembled using U-shaped connectors, creating a compact and space-efficient overall design. Experimental tests have been conducted to verify the performance of the valve, which demonstrated a mass flow range of 0–675 μg/s with a resolution better than 0.1 μg/s and a flow noise below 0.1 μg/s/Hz1/2 at 0.1 mHz–1 Hz.</abstract><cop>United States</cop><pub>American Institute of Physics</pub><pmid>38345452</pmid><doi>10.1063/5.0175676</doi><tpages>8</tpages><orcidid>https://orcid.org/0000-0002-9672-2803</orcidid><orcidid>https://orcid.org/0000-0002-4440-2357</orcidid><orcidid>https://orcid.org/0009-0007-7424-2773</orcidid><orcidid>https://orcid.org/0000-0002-9934-1272</orcidid><orcidid>https://orcid.org/0009-0005-1123-814X</orcidid><oa>free_for_read</oa></addata></record> |
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source | American Institute of Physics (AIP) Publications; American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list) |
subjects | Cold gas Connectors Controllability Flow control High resolution Mass flow Piezoelectric actuators Piezoelectricity Pneumatics Redundancy Scientific satellites Thrusters Valve seats |
title | A high resolution and wide range valve for micronewton cold gas thrusters |
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