Design of flow controller for aviation electric fuel pump
In order to meet the demand of high-precision flow control and modular design of aviation electric fuel pump control system, the flow controller is analyzed and designed from the demand of aviation engines for electric fuel pump. Tests show that the steady-state control deviation of the controller i...
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| Veröffentlicht in: | Journal of physics. Conference series 2023-05, Vol.2472 (1), p.12054 |
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| creator | Wenlong, Zhang Xiao, Ding Jianghong, Li |
| description | In order to meet the demand of high-precision flow control and modular design of aviation electric fuel pump control system, the flow controller is analyzed and designed from the demand of aviation engines for electric fuel pump. Tests show that the steady-state control deviation of the controller is no more than 1% for mass flow rate, and the dynamic control deviation of mass flow rate is no more than 3% in the range of 50kg/h~2000kg/h. A flow controller with high integration degree, high control accuracy and excellent dynamic characteristics for new pump-control system was designed for aero engine. |
| doi_str_mv | 10.1088/1742-6596/2472/1/012054 |
| format | Article |
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Tests show that the steady-state control deviation of the controller is no more than 1% for mass flow rate, and the dynamic control deviation of mass flow rate is no more than 3% in the range of 50kg/h~2000kg/h. A flow controller with high integration degree, high control accuracy and excellent dynamic characteristics for new pump-control system was designed for aero engine.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/2472/1/012054</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aviation ; Control systems design ; Controllers ; Deviation ; Dynamic characteristics ; Dynamic control ; Flow control ; Fuel pumps ; Mass flow rate ; Modular design ; Physics</subject><ispartof>Journal of physics. 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A flow controller with high integration degree, high control accuracy and excellent dynamic characteristics for new pump-control system was designed for aero engine.</description><subject>Aviation</subject><subject>Control systems design</subject><subject>Controllers</subject><subject>Deviation</subject><subject>Dynamic characteristics</subject><subject>Dynamic control</subject><subject>Flow control</subject><subject>Fuel pumps</subject><subject>Mass flow rate</subject><subject>Modular design</subject><subject>Physics</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNqFkE1LxDAQQIMouK7-BgPehNokTZP0KKvrBwsK6jlk04x06TY1aRX_vS2VFUFw5jAD82YGHkKnlFxQolRKJWeJyAuRMi5ZSlNCGcn5HprtJvu7XqlDdBTjhpBsCDlDxZWL1WuDPWCo_Qe2vumCr2sXMPiAzXtluso32NXOdqGyGHpX47bftsfoAEwd3cl3naOX5fXz4jZZPdzcLS5Xic3yoksEM1JIIx0Qy1XJgYqSML7mwDKj1iZTQHLHLAPBOTNcOFsw6yQnKodCsWyOzqa7bfBvvYud3vg-NMNLzRQds-B0oORE2eBjDA50G6qtCZ-aEj160qMBPdrQoydN9eRp2DyfNivf_py-f1w8_QZ1W8IAZ3_A_734Ak-wdn8</recordid><startdate>20230501</startdate><enddate>20230501</enddate><creator>Wenlong, Zhang</creator><creator>Xiao, Ding</creator><creator>Jianghong, Li</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20230501</creationdate><title>Design of flow controller for aviation electric fuel pump</title><author>Wenlong, Zhang ; Xiao, Ding ; Jianghong, Li</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c359t-62a767a7ef0c48d4f16d024b4f23a8ba38f05e2c2f6442a46ec92ce74085f9823</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aviation</topic><topic>Control systems design</topic><topic>Controllers</topic><topic>Deviation</topic><topic>Dynamic characteristics</topic><topic>Dynamic control</topic><topic>Flow control</topic><topic>Fuel pumps</topic><topic>Mass flow rate</topic><topic>Modular design</topic><topic>Physics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wenlong, Zhang</creatorcontrib><creatorcontrib>Xiao, Ding</creatorcontrib><creatorcontrib>Jianghong, Li</creatorcontrib><collection>Institute of Physics Open Access Journal Titles</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>Proquest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>Access via ProQuest (Open Access)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Journal of physics. 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| subjects | Aviation Control systems design Controllers Deviation Dynamic characteristics Dynamic control Flow control Fuel pumps Mass flow rate Modular design Physics |
| title | Design of flow controller for aviation electric fuel pump |
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