Engineering Tests of T14 Plastic Airplane Landing Mat

Engineering Tests of T14 Plastic Airplane Landing Mat

Author:

Publisher:

Published: 1967

Total Pages: 0

ISBN-13:

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An investigation was conducted at the U.S. Army Engineer Waterways Experiment Station (WES) to evaluate a commercially fabricated, plastic mat designated as the T14. The mat is a sandwich-type structure fabricated from epoxy-impregnated, high-density, foam-filled, glass-reinforced core material and glass, filament-wound, glass-fiber facings impregnated with polyester resin. The panels have extruded aluminum side and end connectors secured to the panel edges by the filament winding female connectors. End connections are made with locking-type connectors that are secured by aluminum locking beams. The investigation consisted of both laboratory and engineering traffic tests to determine various properties of the mat in an overall evaluation for comparison with previously tested mats and with project requirements. The results of the laboratory tests indicated that the mat as fabricated failed to meet all technical design requirements of the technical specifications. However, since the mat represented a new design concept, it was traffic tested to complete the evaluation of the design and fabrication. During traffic tests, the T14 mat placed on a 4.2-CBR subgrade sustained a maximum of 12 coverages of a 25,000-lb single-wheel load with 250-psi tire pressure, thus failing to meet it was calculated that an 11.5-CBR subgrade would be required to support the mat for 200 coverages. In view of the more severe operational requirements for present-day airfield surfacing, it was concluded that a reevaluation of new plastic mat designs, fabrication techniques, and plastics technology should be made prior to procurement of any additional plastic loading mats for testing. (Author).


Engineering Tests of Modified T12 Plastic Airplane Landing Mat

Engineering Tests of Modified T12 Plastic Airplane Landing Mat

Author: Hugh L. Green

Publisher:

Published: 1968

Total Pages: 82

ISBN-13:

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This report describes an investigation conducted for the purpose of evaluating an experimental quantity of commercially fabricated plastic mat. The mat is a sandwich structure fabricated from glass-fabric-reinforced honeycomb core material bonded on top and bottom with epoxy adhesive to polyester-resin-impregnated, glass-fabric, laminated facings. Glass-fabric-reinforced tongue-and-groove side and end connectors are fabricated as integral parts of the panels. Laboratory and engineering traffic tests were conducted to determine various properties of the mat in an overall evaluation for comparison with the original T12 mat and with the project requirements. The service-life criteria under which the mat was tested required 200 coverages of a 25,000-lb single-wheel load with a tire-inflation pressure of 250 psi when placed on a subgrade with a California Bearing Ratio (CBR) of 4. This was more critical than the original criteria under which the T12 was tested, which specified 700 coverages of a 50,000-lb single-wheel load with tire-inflation pressures up to 200 psi when placed on a 15-CBR subgrade. (Author).