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...
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Veröffentlicht in: | IOP conference series. Materials Science and Engineering 2018-10, Vol.408 (1), p.12017 |
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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 |
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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 & 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> |
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subjects | Aircraft Airports Hydraulics Injury prevention Mathematical analysis |
title | Design and Calculation Analysis on a New Type of Aircraft Hydraulic Chocks |
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