Journal article 244 views 117 downloads
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump
Energies, Volume: 14, Issue: 11, Start page: 3246
Swansea University Author: Dunhui Xiao
-
PDF | Version of Record
Copyright: © 2021 by the authors. This is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license
Download (5.66MB)
DOI (Published version): 10.3390/en14113246
Abstract
This paper designed and optimized a bidirectional three-port valve plate structure for solving the matching problem of flow rate and pressure in the aerospace pump-controlled differential hydraulic cylinder. This design aims to make the valve plate work well under the bidirectional high-speed condit...
Published in: | Energies |
---|---|
ISSN: | 1996-1073 |
Published: |
MDPI AG
2021
|
Online Access: |
Check full text
|
URI: | https://cronfa.swan.ac.uk/Record/cronfa57945 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
first_indexed |
2021-10-18T10:25:52Z |
---|---|
last_indexed |
2021-10-19T03:22:53Z |
id |
cronfa57945 |
recordtype |
SURis |
fullrecord |
<?xml version="1.0"?><rfc1807><datestamp>2021-10-18T13:19:54.3672119</datestamp><bib-version>v2</bib-version><id>57945</id><entry>2021-09-17</entry><title>Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump</title><swanseaauthors><author><sid>62c69b98cbcdc9142622d4f398fdab97</sid><ORCID>0000-0003-2461-523X</ORCID><firstname>Dunhui</firstname><surname>Xiao</surname><name>Dunhui Xiao</name><active>true</active><ethesisStudent>false</ethesisStudent></author></swanseaauthors><date>2021-09-17</date><deptcode>AERO</deptcode><abstract>This paper designed and optimized a bidirectional three-port valve plate structure for solving the matching problem of flow rate and pressure in the aerospace pump-controlled differential hydraulic cylinder. This design aims to make the valve plate work well under the bidirectional high-speed condition. The model was set up using dynamic mesh and sliding mesh, and the simulation is conducted by FLUENT. In addition, the flow field of inlet and outlet flow rate pulsations, pressure pulsation in cylinder, and non-dead-point transition zone of four cases are analyzed to optimize the valve plate in this work. The numerical results show that different angles of non-dead-point transition zones of the valve plate have a big impact on the performance of the piston pump. For example, the flow rate pulsation reaches the minimum when the angle of non-dead point transition zone is greater than or equal to the angle of a cylinder port. However, at this time, the closed compression would occur and the pressure inside the cylinder would rise rapidly as the piston moves to the non-dead point zone, thus resulting in serious pressure overshoot. In addition, if the angle of non-dead point transition zone is reduced within a certain range, the pressure overshoot will be reduced drastically, and the flow pulsation rate will rise a bit. The study suggests that it is necessary to adjust the angle of non-dead point transition zone to balance the pressure overshoot and flow pulsation of the pump to obtain the optimal kidney structure of the valve plate.</abstract><type>Journal Article</type><journal>Energies</journal><volume>14</volume><journalNumber>11</journalNumber><paginationStart>3246</paginationStart><paginationEnd/><publisher>MDPI AG</publisher><placeOfPublication/><isbnPrint/><isbnElectronic/><issnPrint/><issnElectronic>1996-1073</issnElectronic><keywords>three-port piston pump; valve plate design; bidirectional; CFD numerical simulation</keywords><publishedDay>2</publishedDay><publishedMonth>6</publishedMonth><publishedYear>2021</publishedYear><publishedDate>2021-06-02</publishedDate><doi>10.3390/en14113246</doi><url/><notes/><college>COLLEGE NANME</college><department>Aerospace Engineering</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>AERO</DepartmentCode><institution>Swansea University</institution><apcterm/><lastEdited>2021-10-18T13:19:54.3672119</lastEdited><Created>2021-09-17T22:17:26.8902573</Created><path><level id="1">Faculty of Science and Engineering</level><level id="2">School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering</level></path><authors><author><firstname>Xiangyang</firstname><surname>Li</surname><order>1</order></author><author><firstname>Yiting</firstname><surname>Xi</surname><order>2</order></author><author><firstname>Dunhui</firstname><surname>Xiao</surname><orcid>0000-0003-2461-523X</orcid><order>3</order></author><author><firstname>Jiaxin</firstname><surname>Tao</surname><order>4</order></author></authors><documents><document><filename>57945__21205__d4083b8a4ba24544bdee05bdf146f57f.pdf</filename><originalFilename>57945.pdf</originalFilename><uploaded>2021-10-18T11:26:17.5071025</uploaded><type>Output</type><contentLength>5937658</contentLength><contentType>application/pdf</contentType><version>Version of Record</version><cronfaStatus>true</cronfaStatus><documentNotes>Copyright: © 2021 by the authors. This is an open access article distributed under the terms and
conditions of the Creative Commons Attribution (CC BY) license</documentNotes><copyrightCorrect>true</copyrightCorrect><language>eng</language><licence>https://creativecommons.org/licenses/by/4.0/</licence></document></documents><OutputDurs/></rfc1807> |
spelling |
2021-10-18T13:19:54.3672119 v2 57945 2021-09-17 Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump 62c69b98cbcdc9142622d4f398fdab97 0000-0003-2461-523X Dunhui Xiao Dunhui Xiao true false 2021-09-17 AERO This paper designed and optimized a bidirectional three-port valve plate structure for solving the matching problem of flow rate and pressure in the aerospace pump-controlled differential hydraulic cylinder. This design aims to make the valve plate work well under the bidirectional high-speed condition. The model was set up using dynamic mesh and sliding mesh, and the simulation is conducted by FLUENT. In addition, the flow field of inlet and outlet flow rate pulsations, pressure pulsation in cylinder, and non-dead-point transition zone of four cases are analyzed to optimize the valve plate in this work. The numerical results show that different angles of non-dead-point transition zones of the valve plate have a big impact on the performance of the piston pump. For example, the flow rate pulsation reaches the minimum when the angle of non-dead point transition zone is greater than or equal to the angle of a cylinder port. However, at this time, the closed compression would occur and the pressure inside the cylinder would rise rapidly as the piston moves to the non-dead point zone, thus resulting in serious pressure overshoot. In addition, if the angle of non-dead point transition zone is reduced within a certain range, the pressure overshoot will be reduced drastically, and the flow pulsation rate will rise a bit. The study suggests that it is necessary to adjust the angle of non-dead point transition zone to balance the pressure overshoot and flow pulsation of the pump to obtain the optimal kidney structure of the valve plate. Journal Article Energies 14 11 3246 MDPI AG 1996-1073 three-port piston pump; valve plate design; bidirectional; CFD numerical simulation 2 6 2021 2021-06-02 10.3390/en14113246 COLLEGE NANME Aerospace Engineering COLLEGE CODE AERO Swansea University 2021-10-18T13:19:54.3672119 2021-09-17T22:17:26.8902573 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering Xiangyang Li 1 Yiting Xi 2 Dunhui Xiao 0000-0003-2461-523X 3 Jiaxin Tao 4 57945__21205__d4083b8a4ba24544bdee05bdf146f57f.pdf 57945.pdf 2021-10-18T11:26:17.5071025 Output 5937658 application/pdf Version of Record true Copyright: © 2021 by the authors. This is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license true eng https://creativecommons.org/licenses/by/4.0/ |
title |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump |
spellingShingle |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump Dunhui Xiao |
title_short |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump |
title_full |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump |
title_fullStr |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump |
title_full_unstemmed |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump |
title_sort |
Valve Plate Structural Optimal Design and Flow Field Analysis for the Aviation Bidirectional Three-Port Piston Pump |
author_id_str_mv |
62c69b98cbcdc9142622d4f398fdab97 |
author_id_fullname_str_mv |
62c69b98cbcdc9142622d4f398fdab97_***_Dunhui Xiao |
author |
Dunhui Xiao |
author2 |
Xiangyang Li Yiting Xi Dunhui Xiao Jiaxin Tao |
format |
Journal article |
container_title |
Energies |
container_volume |
14 |
container_issue |
11 |
container_start_page |
3246 |
publishDate |
2021 |
institution |
Swansea University |
issn |
1996-1073 |
doi_str_mv |
10.3390/en14113246 |
publisher |
MDPI AG |
college_str |
Faculty of Science and Engineering |
hierarchytype |
|
hierarchy_top_id |
facultyofscienceandengineering |
hierarchy_top_title |
Faculty of Science and Engineering |
hierarchy_parent_id |
facultyofscienceandengineering |
hierarchy_parent_title |
Faculty of Science and Engineering |
department_str |
School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering |
document_store_str |
1 |
active_str |
0 |
description |
This paper designed and optimized a bidirectional three-port valve plate structure for solving the matching problem of flow rate and pressure in the aerospace pump-controlled differential hydraulic cylinder. This design aims to make the valve plate work well under the bidirectional high-speed condition. The model was set up using dynamic mesh and sliding mesh, and the simulation is conducted by FLUENT. In addition, the flow field of inlet and outlet flow rate pulsations, pressure pulsation in cylinder, and non-dead-point transition zone of four cases are analyzed to optimize the valve plate in this work. The numerical results show that different angles of non-dead-point transition zones of the valve plate have a big impact on the performance of the piston pump. For example, the flow rate pulsation reaches the minimum when the angle of non-dead point transition zone is greater than or equal to the angle of a cylinder port. However, at this time, the closed compression would occur and the pressure inside the cylinder would rise rapidly as the piston moves to the non-dead point zone, thus resulting in serious pressure overshoot. In addition, if the angle of non-dead point transition zone is reduced within a certain range, the pressure overshoot will be reduced drastically, and the flow pulsation rate will rise a bit. The study suggests that it is necessary to adjust the angle of non-dead point transition zone to balance the pressure overshoot and flow pulsation of the pump to obtain the optimal kidney structure of the valve plate. |
published_date |
2021-06-02T04:14:04Z |
_version_ |
1763753951734267904 |
score |
11.037581 |