Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks

In order to facilitate the rapid drainage of airport apron in the special weather (such as heavy rain and snow), the apron is usually designed to have a certain slope. However, this slope leads to a difficult problem that chocks are not easy to take out when the airplane leave airport. In order to s...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:IOP conference series. Materials Science and Engineering 2018-10, Vol.408 (1), p.12017
Hauptverfasser: Kesheng, Meng, Fengyu, Li, Bin, Xia, Pandeng, Chen, Qizhao, Lin, Chen, Chen
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue 1
container_start_page 12017
container_title IOP conference series. Materials Science and Engineering
container_volume 408
creator Kesheng, Meng
Fengyu, Li
Bin, Xia
Pandeng, Chen
Qizhao, Lin
Chen, Chen
description In order to facilitate the rapid drainage of airport apron in the special weather (such as heavy rain and snow), the apron is usually designed to have a certain slope. However, this slope leads to a difficult problem that chocks are not easy to take out when the airplane leave airport. In order to solve this problem, a hydraulic chocks design scheme is firstly proposed. The aircraft hydraulic chock involves two systems, which are named the slider system and the rod system Taking Boeing 737-800 as an example, this paper firstly makes reasonable assumptions. And then uses a hydraulic chocks to analyze the aircraft's stress situation. Through the calculation and analysis of the scheme, the feasibility of the scheme is verified, it also completely solve problem that chocks are not easy to take out. At the same time, the use of the hydraulic wheel block also avoids injury to personnel and waste of time.
doi_str_mv 10.1088/1757-899X/408/1/012017
format Article
fullrecord <record><control><sourceid>proquest_iop_j</sourceid><recordid>TN_cdi_proquest_journals_2557078807</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2557078807</sourcerecordid><originalsourceid>FETCH-LOGICAL-c402t-c21e43d9a31f62739a09e4904dc3b810c4e7891a461704b4089d1efd53927c633</originalsourceid><addsrcrecordid>eNqFUMFKxDAQDaLguvoLEvDipXbSpE1yXOrqKqseXMFbyKapdq1tTVqkf2-XyoogeJo3zHtvZh5CpwQuCAgREh7zQEj5HDIYuhBIBITvoclusL_DghyiI-83AAlnDCbo9tL64qXCuspwqkvTlbot6grPKl32vvB4wBrf20-86huL6xzPCmeczlu86DOnu7IwOH2tzZs_Rge5Lr09-a5T9HQ1X6WLYPlwfZPOloFhELWBiYhlNJOakjyJOJUapGUSWGboWhAwzHIhiWYJ4cDWw08yIzbPYiojbhJKp-hs9G1c_dFZ36pN3bnhXq-iOObAhQA-sJKRZVztvbO5alzxrl2vCKhtbmobidrGo4Ydiqgxt0EYjcKibn6c_xWd_yG6e5z_oqkmy-kXSzJ6jA</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2557078807</pqid></control><display><type>article</type><title>Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks</title><source>IOP Publishing Free Content</source><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><source>IOPscience extra</source><source>Free Full-Text Journals in Chemistry</source><creator>Kesheng, Meng ; Fengyu, Li ; Bin, Xia ; Pandeng, Chen ; Qizhao, Lin ; Chen, Chen</creator><creatorcontrib>Kesheng, Meng ; Fengyu, Li ; Bin, Xia ; Pandeng, Chen ; Qizhao, Lin ; Chen, Chen</creatorcontrib><description>In order to facilitate the rapid drainage of airport apron in the special weather (such as heavy rain and snow), the apron is usually designed to have a certain slope. However, this slope leads to a difficult problem that chocks are not easy to take out when the airplane leave airport. In order to solve this problem, a hydraulic chocks design scheme is firstly proposed. The aircraft hydraulic chock involves two systems, which are named the slider system and the rod system Taking Boeing 737-800 as an example, this paper firstly makes reasonable assumptions. And then uses a hydraulic chocks to analyze the aircraft's stress situation. Through the calculation and analysis of the scheme, the feasibility of the scheme is verified, it also completely solve problem that chocks are not easy to take out. At the same time, the use of the hydraulic wheel block also avoids injury to personnel and waste of time.</description><identifier>ISSN: 1757-8981</identifier><identifier>ISSN: 1757-899X</identifier><identifier>EISSN: 1757-899X</identifier><identifier>DOI: 10.1088/1757-899X/408/1/012017</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Aircraft ; Airports ; Hydraulics ; Injury prevention ; Mathematical analysis</subject><ispartof>IOP conference series. Materials Science and Engineering, 2018-10, Vol.408 (1), p.12017</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>2018. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c402t-c21e43d9a31f62739a09e4904dc3b810c4e7891a461704b4089d1efd53927c633</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://iopscience.iop.org/article/10.1088/1757-899X/408/1/012017/pdf$$EPDF$$P50$$Giop$$Hfree_for_read</linktopdf><link.rule.ids>314,776,780,27901,27902,38845,38867,53815,53842</link.rule.ids></links><search><creatorcontrib>Kesheng, Meng</creatorcontrib><creatorcontrib>Fengyu, Li</creatorcontrib><creatorcontrib>Bin, Xia</creatorcontrib><creatorcontrib>Pandeng, Chen</creatorcontrib><creatorcontrib>Qizhao, Lin</creatorcontrib><creatorcontrib>Chen, Chen</creatorcontrib><title>Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks</title><title>IOP conference series. Materials Science and Engineering</title><addtitle>IOP Conf. Ser.: Mater. Sci. Eng</addtitle><description>In order to facilitate the rapid drainage of airport apron in the special weather (such as heavy rain and snow), the apron is usually designed to have a certain slope. However, this slope leads to a difficult problem that chocks are not easy to take out when the airplane leave airport. In order to solve this problem, a hydraulic chocks design scheme is firstly proposed. The aircraft hydraulic chock involves two systems, which are named the slider system and the rod system Taking Boeing 737-800 as an example, this paper firstly makes reasonable assumptions. And then uses a hydraulic chocks to analyze the aircraft's stress situation. Through the calculation and analysis of the scheme, the feasibility of the scheme is verified, it also completely solve problem that chocks are not easy to take out. At the same time, the use of the hydraulic wheel block also avoids injury to personnel and waste of time.</description><subject>Aircraft</subject><subject>Airports</subject><subject>Hydraulics</subject><subject>Injury prevention</subject><subject>Mathematical analysis</subject><issn>1757-8981</issn><issn>1757-899X</issn><issn>1757-899X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>BENPR</sourceid><recordid>eNqFUMFKxDAQDaLguvoLEvDipXbSpE1yXOrqKqseXMFbyKapdq1tTVqkf2-XyoogeJo3zHtvZh5CpwQuCAgREh7zQEj5HDIYuhBIBITvoclusL_DghyiI-83AAlnDCbo9tL64qXCuspwqkvTlbot6grPKl32vvB4wBrf20-86huL6xzPCmeczlu86DOnu7IwOH2tzZs_Rge5Lr09-a5T9HQ1X6WLYPlwfZPOloFhELWBiYhlNJOakjyJOJUapGUSWGboWhAwzHIhiWYJ4cDWw08yIzbPYiojbhJKp-hs9G1c_dFZ36pN3bnhXq-iOObAhQA-sJKRZVztvbO5alzxrl2vCKhtbmobidrGo4Ydiqgxt0EYjcKibn6c_xWd_yG6e5z_oqkmy-kXSzJ6jA</recordid><startdate>20181001</startdate><enddate>20181001</enddate><creator>Kesheng, Meng</creator><creator>Fengyu, Li</creator><creator>Bin, Xia</creator><creator>Pandeng, Chen</creator><creator>Qizhao, Lin</creator><creator>Chen, Chen</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>KB.</scope><scope>L6V</scope><scope>M7S</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20181001</creationdate><title>Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks</title><author>Kesheng, Meng ; Fengyu, Li ; Bin, Xia ; Pandeng, Chen ; Qizhao, Lin ; Chen, Chen</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c402t-c21e43d9a31f62739a09e4904dc3b810c4e7891a461704b4089d1efd53927c633</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Aircraft</topic><topic>Airports</topic><topic>Hydraulics</topic><topic>Injury prevention</topic><topic>Mathematical analysis</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kesheng, Meng</creatorcontrib><creatorcontrib>Fengyu, Li</creatorcontrib><creatorcontrib>Bin, Xia</creatorcontrib><creatorcontrib>Pandeng, Chen</creatorcontrib><creatorcontrib>Qizhao, Lin</creatorcontrib><creatorcontrib>Chen, Chen</creatorcontrib><collection>IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science &amp; Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection (ProQuest)</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>Materials Science Database</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>Materials Science Collection</collection><collection>Publicly Available Content Database</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><collection>Engineering Collection</collection><jtitle>IOP conference series. Materials Science and Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kesheng, Meng</au><au>Fengyu, Li</au><au>Bin, Xia</au><au>Pandeng, Chen</au><au>Qizhao, Lin</au><au>Chen, Chen</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks</atitle><jtitle>IOP conference series. Materials Science and Engineering</jtitle><addtitle>IOP Conf. Ser.: Mater. Sci. Eng</addtitle><date>2018-10-01</date><risdate>2018</risdate><volume>408</volume><issue>1</issue><spage>12017</spage><pages>12017-</pages><issn>1757-8981</issn><issn>1757-899X</issn><eissn>1757-899X</eissn><abstract>In order to facilitate the rapid drainage of airport apron in the special weather (such as heavy rain and snow), the apron is usually designed to have a certain slope. However, this slope leads to a difficult problem that chocks are not easy to take out when the airplane leave airport. In order to solve this problem, a hydraulic chocks design scheme is firstly proposed. The aircraft hydraulic chock involves two systems, which are named the slider system and the rod system Taking Boeing 737-800 as an example, this paper firstly makes reasonable assumptions. And then uses a hydraulic chocks to analyze the aircraft's stress situation. Through the calculation and analysis of the scheme, the feasibility of the scheme is verified, it also completely solve problem that chocks are not easy to take out. At the same time, the use of the hydraulic wheel block also avoids injury to personnel and waste of time.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1757-899X/408/1/012017</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 1757-8981
ispartof IOP conference series. Materials Science and Engineering, 2018-10, Vol.408 (1), p.12017
issn 1757-8981
1757-899X
1757-899X
language eng
recordid cdi_proquest_journals_2557078807
source IOP Publishing Free Content; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; IOPscience extra; Free Full-Text Journals in Chemistry
subjects Aircraft
Airports
Hydraulics
Injury prevention
Mathematical analysis
title Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-31T14%3A09%3A53IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_iop_j&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Design%20and%20Calculation%20Analysis%20on%20a%20New%20Type%20of%20Aircraft%20Hydraulic%20Chocks&rft.jtitle=IOP%20conference%20series.%20Materials%20Science%20and%20Engineering&rft.au=Kesheng,%20Meng&rft.date=2018-10-01&rft.volume=408&rft.issue=1&rft.spage=12017&rft.pages=12017-&rft.issn=1757-8981&rft.eissn=1757-899X&rft_id=info:doi/10.1088/1757-899X/408/1/012017&rft_dat=%3Cproquest_iop_j%3E2557078807%3C/proquest_iop_j%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2557078807&rft_id=info:pmid/&rfr_iscdi=true