Control to reduce the noise level of the supersonic aircraft engine

This paper presents the results of the research on the possibility of providing requirements for the noise of civil supersonic aircraft using its propulsion system controlling. The methods are based on the use of an engine mathematical model embedded in digital automatic control system. The use of E...

Full description

Saved in:
Bibliographic Details
Main Authors: Golberg, Feliks, Gurevich, Oskar
Format: Conference Proceeding
Language:English
Subjects:
Aircraft engines
Aircraft noise
Automatic control systems
Mathematical models
Noise levels
Propulsion systems
Supersonic aircraft
Turbofan engines
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites
container_end_page
container_issue 1
container_start_page
container_title
container_volume 2700
creator Golberg, Feliks
Gurevich, Oskar
description This paper presents the results of the research on the possibility of providing requirements for the noise of civil supersonic aircraft using its propulsion system controlling. The methods are based on the use of an engine mathematical model embedded in digital automatic control system. The use of EMM provides real-time calculation of the engine operation parameters that are not available for the measurement, including those affecting the amount of noise. An important part of the engine mathematical model application is the model identification during the operation of the engine. Focusing on a turbofan engine it is shown that during takeoff and landing the use of such control can significantly reduce the jet velocity, which helps reduce the noise level. At the same time, the thrust is maintained at the required level.
doi_str_mv 10.1063/5.0124999
format conference_proceeding
fullrecord <record><control><sourceid>proquest_scita</sourceid><recordid>TN_cdi_scitation_primary_10_1063_5_0124999</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2784966382</sourcerecordid><originalsourceid>FETCH-LOGICAL-p168t-a6ad74f769b331594f6b7396c57b90309a688fff06e6dbbcd7683fa3e41a6a523</originalsourceid><addsrcrecordid>eNp9kEtLxDAAhIMoWFcP_oOAN6Fr0ryPUnzBghcFbyFtE81Sk5qkC_57d90Fb54Ghm9mYAC4xGiJESc3bIlwQ5VSR6DCjOFacMyPQYWQonVDydspOMt5jVCjhJAVaNsYSoojLBEmO8y9heXDwhB9tnC0GzvC6H6tPE825Rh8D41PfTKuQBvefbDn4MSZMduLgy7A6_3dS_tYr54fntrbVT1hLkttuBkEdYKrjhDMFHW8E0TxnolOIYKU4VI65xC3fOi6fhBcEmeIpXgbZQ1ZgKt975Ti12xz0es4p7Cd1I2QVHFO5I663lO598UUH4Oekv806VtvYtJMHw7S0-D-gzHSu0f_AuQHBhpnbg</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype><pqid>2784966382</pqid></control><display><type>conference_proceeding</type><title>Control to reduce the noise level of the supersonic aircraft engine</title><source>American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list)</source><creator>Golberg, Feliks ; Gurevich, Oskar</creator><contributor>Kovalev, Igor ; Voroshilova, Anna</contributor><creatorcontrib>Golberg, Feliks ; Gurevich, Oskar ; Kovalev, Igor ; Voroshilova, Anna</creatorcontrib><description>This paper presents the results of the research on the possibility of providing requirements for the noise of civil supersonic aircraft using its propulsion system controlling. The methods are based on the use of an engine mathematical model embedded in digital automatic control system. The use of EMM provides real-time calculation of the engine operation parameters that are not available for the measurement, including those affecting the amount of noise. An important part of the engine mathematical model application is the model identification during the operation of the engine. Focusing on a turbofan engine it is shown that during takeoff and landing the use of such control can significantly reduce the jet velocity, which helps reduce the noise level. At the same time, the thrust is maintained at the required level.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0124999</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Aircraft engines ; Aircraft noise ; Automatic control systems ; Mathematical models ; Noise levels ; Propulsion systems ; Supersonic aircraft ; Turbofan engines</subject><ispartof>AIP conference proceedings, 2023, Vol.2700 (1)</ispartof><rights>Author(s)</rights><rights>2023 Author(s). Published by AIP Publishing.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>309,310,314,776,780,785,786,23909,23910,25118,27901,27902</link.rule.ids></links><search><contributor>Kovalev, Igor</contributor><contributor>Voroshilova, Anna</contributor><creatorcontrib>Golberg, Feliks</creatorcontrib><creatorcontrib>Gurevich, Oskar</creatorcontrib><title>Control to reduce the noise level of the supersonic aircraft engine</title><title>AIP conference proceedings</title><description>This paper presents the results of the research on the possibility of providing requirements for the noise of civil supersonic aircraft using its propulsion system controlling. The methods are based on the use of an engine mathematical model embedded in digital automatic control system. The use of EMM provides real-time calculation of the engine operation parameters that are not available for the measurement, including those affecting the amount of noise. An important part of the engine mathematical model application is the model identification during the operation of the engine. Focusing on a turbofan engine it is shown that during takeoff and landing the use of such control can significantly reduce the jet velocity, which helps reduce the noise level. At the same time, the thrust is maintained at the required level.</description><subject>Aircraft engines</subject><subject>Aircraft noise</subject><subject>Automatic control systems</subject><subject>Mathematical models</subject><subject>Noise levels</subject><subject>Propulsion systems</subject><subject>Supersonic aircraft</subject><subject>Turbofan engines</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2023</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kEtLxDAAhIMoWFcP_oOAN6Fr0ryPUnzBghcFbyFtE81Sk5qkC_57d90Fb54Ghm9mYAC4xGiJESc3bIlwQ5VSR6DCjOFacMyPQYWQonVDydspOMt5jVCjhJAVaNsYSoojLBEmO8y9heXDwhB9tnC0GzvC6H6tPE825Rh8D41PfTKuQBvefbDn4MSZMduLgy7A6_3dS_tYr54fntrbVT1hLkttuBkEdYKrjhDMFHW8E0TxnolOIYKU4VI65xC3fOi6fhBcEmeIpXgbZQ1ZgKt975Ti12xz0es4p7Cd1I2QVHFO5I663lO598UUH4Oekv806VtvYtJMHw7S0-D-gzHSu0f_AuQHBhpnbg</recordid><startdate>20230309</startdate><enddate>20230309</enddate><creator>Golberg, Feliks</creator><creator>Gurevich, Oskar</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20230309</creationdate><title>Control to reduce the noise level of the supersonic aircraft engine</title><author>Golberg, Feliks ; Gurevich, Oskar</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p168t-a6ad74f769b331594f6b7396c57b90309a688fff06e6dbbcd7683fa3e41a6a523</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aircraft engines</topic><topic>Aircraft noise</topic><topic>Automatic control systems</topic><topic>Mathematical models</topic><topic>Noise levels</topic><topic>Propulsion systems</topic><topic>Supersonic aircraft</topic><topic>Turbofan engines</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Golberg, Feliks</creatorcontrib><creatorcontrib>Gurevich, Oskar</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Golberg, Feliks</au><au>Gurevich, Oskar</au><au>Kovalev, Igor</au><au>Voroshilova, Anna</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Control to reduce the noise level of the supersonic aircraft engine</atitle><btitle>AIP conference proceedings</btitle><date>2023-03-09</date><risdate>2023</risdate><volume>2700</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>This paper presents the results of the research on the possibility of providing requirements for the noise of civil supersonic aircraft using its propulsion system controlling. The methods are based on the use of an engine mathematical model embedded in digital automatic control system. The use of EMM provides real-time calculation of the engine operation parameters that are not available for the measurement, including those affecting the amount of noise. An important part of the engine mathematical model application is the model identification during the operation of the engine. Focusing on a turbofan engine it is shown that during takeoff and landing the use of such control can significantly reduce the jet velocity, which helps reduce the noise level. At the same time, the thrust is maintained at the required level.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0124999</doi><tpages>6</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0094-243X
ispartof AIP conference proceedings, 2023, Vol.2700 (1)
issn 0094-243X
1551-7616
language eng
recordid cdi_scitation_primary_10_1063_5_0124999
source American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list)
subjects Aircraft engines
Aircraft noise
Automatic control systems
Mathematical models
Noise levels
Propulsion systems
Supersonic aircraft
Turbofan engines
title Control to reduce the noise level of the supersonic aircraft engine
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T20%3A03%3A16IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_scita&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Control%20to%20reduce%20the%20noise%20level%20of%20the%20supersonic%20aircraft%20engine&rft.btitle=AIP%20conference%20proceedings&rft.au=Golberg,%20Feliks&rft.date=2023-03-09&rft.volume=2700&rft.issue=1&rft.issn=0094-243X&rft.eissn=1551-7616&rft.coden=APCPCS&rft_id=info:doi/10.1063/5.0124999&rft_dat=%3Cproquest_scita%3E2784966382%3C/proquest_scita%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-p168t-a6ad74f769b331594f6b7396c57b90309a688fff06e6dbbcd7683fa3e41a6a523%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2784966382&rft_id=info:pmid/&rfr_iscdi=true