Aero-engine scale deposition simulation experiment test equipment and use method thereof

Aero-engine scale deposition simulation experiment test equipment and use method thereof

The invention discloses aero-engine scale deposition simulation experiment test equipment which comprises a powder feeding system, a measuring system and a wind tunnel system, the powder feeding system is installed at the top of the air inlet end of the wind tunnel system, a power device is installe...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HUO JINJIAN, WANG LIWEN, LU XIN, TANG JIE, SHI XUDONG
Format: Patent
Sprache:chi ; eng
Schlagworte:
MEASURING
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
creator HUO JINJIAN
WANG LIWEN
LU XIN
TANG JIE
SHI XUDONG
description The invention discloses aero-engine scale deposition simulation experiment test equipment which comprises a powder feeding system, a measuring system and a wind tunnel system, the powder feeding system is installed at the top of the air inlet end of the wind tunnel system, a power device is installed at the tail end of the wind tunnel system, and the measuring system is installed at the upper end of the middle of the wind tunnel system; the powder feeding system is used for conveying scale deposition particles into the wind tunnel system; the measuring system is used for measuring experimental parameters; and the power device is used for providing stable airflow required by an experiment. The device highly restores the scale deposition condition of an aircraft under the flight environment condition, is high in measurement precision, can visually observe the scale deposition process, is small in size, is high in automation degree, is simple and convenient in operation process, can simulate different scale depo
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN115420511A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN115420511A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN115420511A3</originalsourceid><addsrcrecordid>eNqNjDsKwkAURdNYiLqHlwUEHDULCEGxsrKwC0PmxgzMz3lvwOUrwQVY3XPgcNfVo0OODcLTBhCP2oEMUmQrNgZi64vTC-KdkK1HEBKwEF7FpkV1MFQY5CFzNCQzMuK0rVaTdozdbzdVfTnf-2vzfR_ASY8IkKG_KdWeDvtWqe74T_MB94w64w</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aero-engine scale deposition simulation experiment test equipment and use method thereof</title><source>esp@cenet</source><creator>HUO JINJIAN ; WANG LIWEN ; LU XIN ; TANG JIE ; SHI XUDONG</creator><creatorcontrib>HUO JINJIAN ; WANG LIWEN ; LU XIN ; TANG JIE ; SHI XUDONG</creatorcontrib><description>The invention discloses aero-engine scale deposition simulation experiment test equipment which comprises a powder feeding system, a measuring system and a wind tunnel system, the powder feeding system is installed at the top of the air inlet end of the wind tunnel system, a power device is installed at the tail end of the wind tunnel system, and the measuring system is installed at the upper end of the middle of the wind tunnel system; the powder feeding system is used for conveying scale deposition particles into the wind tunnel system; the measuring system is used for measuring experimental parameters; and the power device is used for providing stable airflow required by an experiment. The device highly restores the scale deposition condition of an aircraft under the flight environment condition, is high in measurement precision, can visually observe the scale deposition process, is small in size, is high in automation degree, is simple and convenient in operation process, can simulate different scale depo</description><language>chi ; eng</language><subject>MEASURING ; PHYSICS ; TESTING ; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES ; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20221202&amp;DB=EPODOC&amp;CC=CN&amp;NR=115420511A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20221202&amp;DB=EPODOC&amp;CC=CN&amp;NR=115420511A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUO JINJIAN</creatorcontrib><creatorcontrib>WANG LIWEN</creatorcontrib><creatorcontrib>LU XIN</creatorcontrib><creatorcontrib>TANG JIE</creatorcontrib><creatorcontrib>SHI XUDONG</creatorcontrib><title>Aero-engine scale deposition simulation experiment test equipment and use method thereof</title><description>The invention discloses aero-engine scale deposition simulation experiment test equipment which comprises a powder feeding system, a measuring system and a wind tunnel system, the powder feeding system is installed at the top of the air inlet end of the wind tunnel system, a power device is installed at the tail end of the wind tunnel system, and the measuring system is installed at the upper end of the middle of the wind tunnel system; the powder feeding system is used for conveying scale deposition particles into the wind tunnel system; the measuring system is used for measuring experimental parameters; and the power device is used for providing stable airflow required by an experiment. The device highly restores the scale deposition condition of an aircraft under the flight environment condition, is high in measurement precision, can visually observe the scale deposition process, is small in size, is high in automation degree, is simple and convenient in operation process, can simulate different scale depo</description><subject>MEASURING</subject><subject>PHYSICS</subject><subject>TESTING</subject><subject>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</subject><subject>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjDsKwkAURdNYiLqHlwUEHDULCEGxsrKwC0PmxgzMz3lvwOUrwQVY3XPgcNfVo0OODcLTBhCP2oEMUmQrNgZi64vTC-KdkK1HEBKwEF7FpkV1MFQY5CFzNCQzMuK0rVaTdozdbzdVfTnf-2vzfR_ASY8IkKG_KdWeDvtWqe74T_MB94w64w</recordid><startdate>20221202</startdate><enddate>20221202</enddate><creator>HUO JINJIAN</creator><creator>WANG LIWEN</creator><creator>LU XIN</creator><creator>TANG JIE</creator><creator>SHI XUDONG</creator><scope>EVB</scope></search><sort><creationdate>20221202</creationdate><title>Aero-engine scale deposition simulation experiment test equipment and use method thereof</title><author>HUO JINJIAN ; WANG LIWEN ; LU XIN ; TANG JIE ; SHI XUDONG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN115420511A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>MEASURING</topic><topic>PHYSICS</topic><topic>TESTING</topic><topic>TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES</topic><topic>TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR</topic><toplevel>online_resources</toplevel><creatorcontrib>HUO JINJIAN</creatorcontrib><creatorcontrib>WANG LIWEN</creatorcontrib><creatorcontrib>LU XIN</creatorcontrib><creatorcontrib>TANG JIE</creatorcontrib><creatorcontrib>SHI XUDONG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUO JINJIAN</au><au>WANG LIWEN</au><au>LU XIN</au><au>TANG JIE</au><au>SHI XUDONG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aero-engine scale deposition simulation experiment test equipment and use method thereof</title><date>2022-12-02</date><risdate>2022</risdate><abstract>The invention discloses aero-engine scale deposition simulation experiment test equipment which comprises a powder feeding system, a measuring system and a wind tunnel system, the powder feeding system is installed at the top of the air inlet end of the wind tunnel system, a power device is installed at the tail end of the wind tunnel system, and the measuring system is installed at the upper end of the middle of the wind tunnel system; the powder feeding system is used for conveying scale deposition particles into the wind tunnel system; the measuring system is used for measuring experimental parameters; and the power device is used for providing stable airflow required by an experiment. The device highly restores the scale deposition condition of an aircraft under the flight environment condition, is high in measurement precision, can visually observe the scale deposition process, is small in size, is high in automation degree, is simple and convenient in operation process, can simulate different scale depo</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN115420511A
source esp@cenet
subjects MEASURING
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
title Aero-engine scale deposition simulation experiment test equipment and use method thereof
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-19T14%3A37%3A48IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=HUO%20JINJIAN&rft.date=2022-12-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN115420511A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true