EVALUATION OF DOW CHEMICAL EXTRUDED LANDING MAT

The report describes an investigation conducted to evaluate an experimental quantity of extruded aluminum alloy landing mat. The mats are one-piece hollow extrusions fabricated from 6061 (designated MX18-B) and 7005 (designated MX18-C) aluminum alloys, artificially aged to the T6 condition. The pane...

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Hauptverfasser: Green, Hugh L, Carr, Gordon L
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Carr, Gordon L
description The report describes an investigation conducted to evaluate an experimental quantity of extruded aluminum alloy landing mat. The mats are one-piece hollow extrusions fabricated from 6061 (designated MX18-B) and 7005 (designated MX18-C) aluminum alloys, artificially aged to the T6 condition. The panels are interlocked along the sides by means of a hinge-type connector, the components of which are an integral part of the basic panel extrusion. End connectors are composed of extruded connectors welded to the basic panel, and consist of an overlap and underlap section secured by a locking bar after individual panels have been joined together. This investigation consisted of traffic tests to obtain information for use in comparing the performance of the mats with project requirements. The traffic tests were conducted on a prepared subgrade, with a rolling wheel load simulating actual aircraft operations. These tests were conducted with a 25,000-lb single-wheel load with a tire inflation pressure of 250 psi on a mat-surfaced subgrade with a rated CBR of 3.7 and 4.0 for the MX18-B and MX18-C, respectively. (Author)
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The mats are one-piece hollow extrusions fabricated from 6061 (designated MX18-B) and 7005 (designated MX18-C) aluminum alloys, artificially aged to the T6 condition. The panels are interlocked along the sides by means of a hinge-type connector, the components of which are an integral part of the basic panel extrusion. End connectors are composed of extruded connectors welded to the basic panel, and consist of an overlap and underlap section secured by a locking bar after individual panels have been joined together. This investigation consisted of traffic tests to obtain information for use in comparing the performance of the mats with project requirements. The traffic tests were conducted on a prepared subgrade, with a rolling wheel load simulating actual aircraft operations. These tests were conducted with a 25,000-lb single-wheel load with a tire inflation pressure of 250 psi on a mat-surfaced subgrade with a rated CBR of 3.7 and 4.0 for the MX18-B and MX18-C, respectively. 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(Author)</description><subject>ALUMINUM ALLOY 6061</subject><subject>ALUMINUM ALLOY 7005</subject><subject>ALUMINUM ALLOYS</subject><subject>DEGRADATION</subject><subject>EVALUATION</subject><subject>EXTRUSION</subject><subject>LANDING FIELDS</subject><subject>LANDING MATS</subject><subject>LOADS(FORCES)</subject><subject>LOCKING FASTENER DEVICES</subject><subject>MATHEMATICAL MODELS</subject><subject>Metallurgy and Metallography</subject><subject>PANELS</subject><subject>PERFORMANCE(ENGINEERING)</subject><subject>PORTABLE EQUIPMENT</subject><subject>Terminal Flight Facilities</subject><subject>TRAFFICABILITY</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1968</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZNB3DXP0CXUM8fT3U_B3U3DxD1dw9nD19XR29FFwjQgJCnVxdVHwcfRz8fRzV_B1DOFhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4GFsYWlkZmxgSkAXwhIuk</recordid><startdate>196807</startdate><enddate>196807</enddate><creator>Green, Hugh L</creator><creator>Carr, Gordon L</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196807</creationdate><title>EVALUATION OF DOW CHEMICAL EXTRUDED LANDING MAT</title><author>Green, Hugh L ; Carr, Gordon L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD08389263</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1968</creationdate><topic>ALUMINUM ALLOY 6061</topic><topic>ALUMINUM ALLOY 7005</topic><topic>ALUMINUM ALLOYS</topic><topic>DEGRADATION</topic><topic>EVALUATION</topic><topic>EXTRUSION</topic><topic>LANDING FIELDS</topic><topic>LANDING MATS</topic><topic>LOADS(FORCES)</topic><topic>LOCKING FASTENER DEVICES</topic><topic>MATHEMATICAL MODELS</topic><topic>Metallurgy and Metallography</topic><topic>PANELS</topic><topic>PERFORMANCE(ENGINEERING)</topic><topic>PORTABLE EQUIPMENT</topic><topic>Terminal Flight Facilities</topic><topic>TRAFFICABILITY</topic><toplevel>online_resources</toplevel><creatorcontrib>Green, Hugh L</creatorcontrib><creatorcontrib>Carr, Gordon L</creatorcontrib><creatorcontrib>ARMY ENGINEER WATERWAYS EXPERIMENT STATION VICKSBURG MS</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Green, Hugh L</au><au>Carr, Gordon L</au><aucorp>ARMY ENGINEER WATERWAYS EXPERIMENT STATION VICKSBURG MS</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>EVALUATION OF DOW CHEMICAL EXTRUDED LANDING MAT</btitle><date>1968-07</date><risdate>1968</risdate><abstract>The report describes an investigation conducted to evaluate an experimental quantity of extruded aluminum alloy landing mat. The mats are one-piece hollow extrusions fabricated from 6061 (designated MX18-B) and 7005 (designated MX18-C) aluminum alloys, artificially aged to the T6 condition. The panels are interlocked along the sides by means of a hinge-type connector, the components of which are an integral part of the basic panel extrusion. End connectors are composed of extruded connectors welded to the basic panel, and consist of an overlap and underlap section secured by a locking bar after individual panels have been joined together. This investigation consisted of traffic tests to obtain information for use in comparing the performance of the mats with project requirements. The traffic tests were conducted on a prepared subgrade, with a rolling wheel load simulating actual aircraft operations. These tests were conducted with a 25,000-lb single-wheel load with a tire inflation pressure of 250 psi on a mat-surfaced subgrade with a rated CBR of 3.7 and 4.0 for the MX18-B and MX18-C, respectively. 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source DTIC Technical Reports
subjects ALUMINUM ALLOY 6061
ALUMINUM ALLOY 7005
ALUMINUM ALLOYS
DEGRADATION
EVALUATION
EXTRUSION
LANDING FIELDS
LANDING MATS
LOADS(FORCES)
LOCKING FASTENER DEVICES
MATHEMATICAL MODELS
Metallurgy and Metallography
PANELS
PERFORMANCE(ENGINEERING)
PORTABLE EQUIPMENT
Terminal Flight Facilities
TRAFFICABILITY
title EVALUATION OF DOW CHEMICAL EXTRUDED LANDING MAT
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