Loading…

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...

Full description

Saved in:
Bibliographic Details
Published in:Review of scientific instruments 2024-02, Vol.95 (2)
Main Authors: Zhang, Hao-Yuan, Liu, Jian-Ping, Hu, Shao-Gang, Yin, Jin-Huan, Zhong, Yuan, Li, Zhu, Yang, Shan-Qing
Format: Article
Language:English
Subjects:
Citations: Items that this one cites
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites cdi_FETCH-LOGICAL-c343t-c734c380346172baa8de7d1f499a9e92cee08ae76cc47ff4eb440a49df4129a43
container_end_page
container_issue 2
container_start_page
container_title Review of scientific instruments
container_volume 95
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
format article
fullrecord <record><control><sourceid>proquest_pubme</sourceid><recordid>TN_cdi_pubmed_primary_38345452</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2926076804</sourcerecordid><originalsourceid>FETCH-LOGICAL-c343t-c734c380346172baa8de7d1f499a9e92cee08ae76cc47ff4eb440a49df4129a43</originalsourceid><addsrcrecordid>eNp90E1Lw0AQBuBFFFurB_-ALHhRIXW_N3ssxY9CwYuew3YzaVPSpO4mLf57N7R68OBc5vLwMvMidE3JmBLFH-WYUC2VVidoSElqEq0YP0VDQrhIlBbpAF2EsCZxJKXnaMBTLqSQbIhmE7wqlyvsITRV15ZNjW2d432ZA_a2XgLe2WoHuGg83pTONzXs24hcU-V4aQNuV74LLfhwic4KWwW4Ou4R-nh-ep--JvO3l9l0Mk8cF7xNnObC8TRepqhmC2vTHHROC2GMNWCYAyCpBa2cE7ooBCyEIFaYvBCUGSv4CN0dcre--ewgtNmmDA6qytbQdCFjhimiVUp6evuHrpvO1_G6XkkmudIkqvuDit-F4KHItr7cWP-VUZL1_WYyO_Yb7c0xsVtsIP-VP4VG8HAAwZWt7fv8J-0b8u2BNQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2925253670</pqid></control><display><type>article</type><title>A high resolution and wide range valve for micronewton cold gas thrusters</title><source>American Institute of Physics (AIP) Publications</source><source>American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list)</source><creator>Zhang, Hao-Yuan ; Liu, Jian-Ping ; Hu, Shao-Gang ; Yin, Jin-Huan ; Zhong, Yuan ; Li, Zhu ; Yang, Shan-Qing</creator><creatorcontrib>Zhang, Hao-Yuan ; Liu, Jian-Ping ; Hu, Shao-Gang ; Yin, Jin-Huan ; Zhong, Yuan ; Li, Zhu ; Yang, Shan-Qing</creatorcontrib><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.</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). Published under an exclusive license by AIP Publishing.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c343t-c734c380346172baa8de7d1f499a9e92cee08ae76cc47ff4eb440a49df4129a43</cites><orcidid>0000-0002-9672-2803 ; 0000-0002-4440-2357 ; 0009-0007-7424-2773 ; 0000-0002-9934-1272 ; 0009-0005-1123-814X</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/rsi/article-lookup/doi/10.1063/5.0175676$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>314,780,782,784,795,27924,27925,76383</link.rule.ids><backlink>$$Uhttps://www.ncbi.nlm.nih.gov/pubmed/38345452$$D View this record in MEDLINE/PubMed$$Hfree_for_read</backlink></links><search><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><title>A high resolution and wide range valve for micronewton cold gas thrusters</title><title>Review of scientific instruments</title><addtitle>Rev Sci Instrum</addtitle><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.</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>
fulltext fulltext
identifier ISSN: 0034-6748
ispartof Review of scientific instruments, 2024-02, Vol.95 (2)
issn 0034-6748
1089-7623
language eng
recordid cdi_pubmed_primary_38345452
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
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-04T02%3A30%3A00IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_pubme&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20high%20resolution%20and%20wide%20range%20valve%20for%20micronewton%20cold%20gas%20thrusters&rft.jtitle=Review%20of%20scientific%20instruments&rft.au=Zhang,%20Hao-Yuan&rft.date=2024-02-01&rft.volume=95&rft.issue=2&rft.issn=0034-6748&rft.eissn=1089-7623&rft.coden=RSINAK&rft_id=info:doi/10.1063/5.0175676&rft_dat=%3Cproquest_pubme%3E2926076804%3C/proquest_pubme%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c343t-c734c380346172baa8de7d1f499a9e92cee08ae76cc47ff4eb440a49df4129a43%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2925253670&rft_id=info:pmid/38345452&rfr_iscdi=true