Browse Topic: Fabrics and textiles

Items (879)
Composite materials have become widely adopted in commercial aviation, as aerospace manufacturers look to use them to drive weight reduction and improved fuel efficiency in new aircraft designs. In the case of aircraft rotary blades, the poor wear properties of these materials have necessitated the development of metal leading edge guards that can provide critical protection against erosion and impact damage during flight. Electroforming has been a leading process for the manufacture of these protective guards, with nickel parts providing excellent wear resistance that significantly extends the service life of the rotary blade assembly. Currently there has not been a focus on utilizing direct electrodeposition of metal on to carbon filled epoxy composite structures, as traditional plating-on-plastics approaches require considerable effort in surface preparation and normally do not provide adequate adhesion to the underlying structure. Alpha Metalcraft Group has been working in cooperation with aerospace suppliers in the design of an electroplating ready composite structure that would allow for direct nickel deposition, provide excellent adhesion, and significantly reduce both the time and cost for the manufacture of ready-to-assembly rotary blade structures. Test panels were constructed of commercially available prepreg materials or by resin infusion of dry fabrics that incorporated different metal containing conductive layers to allow for the direct deposition through a nickel sulfamate electrodeposition process. Different surface modification strategies were investigated to expose the metal conducting layer and thereby provide the metal-to-metal bonding surfaces required for successful electrodeposition.
Cazzaniga, Luigi
This SAE Aerospae Recommended Practice (ARP) covers visible surface defects on aerospace hose assemblies which have been installed and are functioning within a working environment at the time of visual inspection. This document is intended to help those who are conducting periodic visual inspections of hose assemblies used in aerospace systems and ground servicing equipment to determine time for replacement by condition of hose assemblies at time of inspection. This practice is intended to augment existing procedures for replacement of hose assemblies based on service time. A constant surveillance of all hose assemblies for visible wear, defects, and/or damage shall be routine at all times of maintenance. When wear, defects, or damage to installed hose assemblies is detected, the hose assemblies shall be tagged or replaced in accordace with Section 4 of this document.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Thermoplastic composites are serious competitor for classic epoxy composites. They have comparable properties to epoxy composites, but characterize much lower processing costs. There are several methods of manufacturing the components from thermoplastic composites. One of the most interesting method in terms of efficiency is thermoforming on a press. This technology allows to product of the aircraft parts such as: ribs, brackets, covers, stiffeners. Thermoplastic composites are resistant to most solvents such as grease, oil and aviation fuel. They are also non-flammable and heat-resistant. This all makes them suitable for use in aircraft as upholstery, casing or elements around the tank. PZL Mielec has been developing press thermoforming technologies since 2016 and is the owner of the several patents in this area.
Głodzik, MarcinWojtuszewski, RadosławFarbaniec, KonradSienicki, JarosławBanaś, AleksanderGałaczyński, Tomasz
Lopez, AlfonsoKariyawasam, SupunPostera, RichardCarrol, BrennanSpangler, JoeSeneviratne, WarunaLeach, DavidWood, Billy
This SAE Recommended Practice is applicable for determining the cold characteristics of flexible plastic materials, as applicable. It consists of three different methods for determining low-temperature properties of materials depending on type of material and end use. The method used shall be as specified by the contractual parties.
Textile and Flexible Plastics Committee
The intent of this specification is for the procurement of carbon fiber and fiberglass epoxy prepreg products with 350 °F (177 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (4.3) of this base specification, AMS6891.
AMS P17 Polymer Matrix Composites Committee
This test can be used to determine the resistance to scuffing of test specimens such as fiberboards, fabrics, vinyl-coated fabrics, leathers, and similar trim materials.
Textile and Flexible Plastics Committee
Researchers have developed biomaterial-based inks that respond to and quantify chemicals released from the body (e.g., in sweat and potentially other biofluids) or in the surrounding environment by changing color. The inks can be screen printed onto textiles such as clothes, shoes, or even face masks in complex patterns and at high resolution, providing a detailed map of human response or exposure.
EPFL researchers have developed electronic fibers that, when embedded in textiles, can collect a wealth of information about our bodies by measuring subtle and complex fabric deformations. Their technology relies on transmission line theory and offers a host of applications, such as in healthcare and robotics.
Effects of Helical Carbon Nanotubes on Mechanical Performance of Laminated Composites and Bonded Joints2020-01-00293/10/2020
Most composite assemblies and structures generally fail due to weak interlaminar properties and poor performance of their bonded joints that are assembled together with an adhesive layer. Adhesive failure and cohesive failure are among the most commonly observed failure modes in composite bonded joint assemblies. These failure modes occur due to the lack of reinforcement within the adhesive layer in transverse direction. In addition, the laminated composites fail due to the same reason that is the lack of reinforcement through the thickness direction between the laminae. The overall performance of any composite structures and assemblies largely depends on the interlaminar properties and the performance of its bonded joints. Various techniques and processes were developed in recent years to improve mechanical performance of the composite structures and assemblies, one of which includes the use of nanoscale reinforcements in between the laminae and within the adhesive layer. However, most prior research has been focused on use of straight carbon nanotubes (CNTs) and other nanomaterials in particle forms. The goal of this research was to improve the properties of the adhesive film and the interfacial bonding effectiveness between the laminae. Because CNTs are inert in nature, their interaction with the resin and adhesive polymer molecules is very weak. In this research we have used CNTs with various geometrical configuration (straight and helical geometries) and various weight percentages as additional reinforcements. The objective was to investigate the effectiveness of helical geometries of the CNTs to form interlocking mechanisms with the resin and the traditional microfiber reinforcements to improve the overall performance of the composite structures and assemblies. Single lap joint test specimens and flexural test specimens were prepared based on the ASTM standard D5868-01 and ASTM standard D790 and then tested and analyzed. The experimental results showed that the samples with CNT reinforcements performed considerably better than neat epoxy samples. Among the two different CNT geometries, helical CNTs performed better than the straight CNTs.
Sritharan, RamananAskari, Davood
Natural and Artificial Weathering of Automotive Leather, Leatherette and Textile2019-28-009110/11/2019
This paper presents the natural and artificial weathering behavior of different soft skin materials such as leather, leatherette and textiles used for automotive seat cover applications. The objective of this study was to understand the physical and aesthetical changes occurring at these flexible materials under sun UV light and heat exposure. The natural weathering study under glass exposure was carried out as per ASTM G 24 at natural weathering site location and artificial weathering as per SAE J2412 at lab. The material was observed for surface changes such as color, texture, crack and physical changes like flexibility and hardness during the exposure. The sample exposed at natural weathering data for every 15 days were recorded, and artificial weathering for every 100 hours were recorded. Light and dark color materials were tested to understand the effect of color and UV light resistance as well as various textures were studied to understand the effect of various texture and texture retention under UV. The study was also carried out at two different period in a year and the data were recorded. The weathering of leather, leatherette and textiles exposed at different time showed different degradation behavior. Further the UV resistance of leatherette was found better than leather and textiles. The effect UV on leather, leatherette and textiles under natural and artificial weathering condition were correlated.
Palaniappan, Elavarasan
Mechanical and Corrosion Behaviour of Al 7075 Composite Reinforced with TiC and Al 2 O 3 Particles2019-28-009410/11/2019
Various research regarding new types of fabrication and modifications of Aluminium alloy to improve the existing properties are going on. The wide range application of aluminium alloy is in aerospace and Automobile Industries. The demand for this material improved by mechanical properties with little to zero increment in weight. The current work is based on the fabrication of hybrid aluminium metal matrix composites with the addition of TiC (Titanium Carbide) and Al2O3 (Aluminium Oxide) reinforcement particle using stir casting technique. Three types of hybrid composite samples were prepared based on the weight percentage 5% Al2O3+0% TiC (sample-1), 8% Al2O3 + 12% TiC (sample-2), 20% Al2O3+15% TiC (sample-3). The objective of the study is to analyze the mechanical and corrosion properties of the hybrid composite with the influence of the reinforcement and varying the weight fraction of the particles. Overall, It is observed that a gradual increase in the hardness value in sample-1(83 BHN), Sample-2 (88 BHN) and sample-3 (96 BHN). This trend can be explained by the particulate strengthening of TiC over the soft ductile Al7075 during stir casting. The microstructure also provides a convincing explanation of the increased hardness. The tensile test shows that an increasing trend of yield strength in sample-1 to 3, and a decreasing trend of UTS and YS in sample-2 to 3. This is due to the high content of Al2O3. The corrosion behavior is tested by weight loss method using salt spray test. The sample-3 with the highest content of Al2O3 have the least weight loss and highest corrosion resistance than the other samples.
Jaiswal, SubhamRajamurugan, GovindasamyKrishnasamy, PrabuShaswat, YashwardhanKaushik, Mishra
Advanced structural analysis methods, known as progressive damage and failure analysis (PDFA) tools, are being developed to predict initiation and propagation of damage under repeated loading based on capturing individual and interacting damage modes. This work shows the ability of the PDFA implemented in CDMat software developed at the University of Texas Arlington Advanced Materials and Structures Lab (AMSL) to predict strength and fatigue failure of a Common Feature Test Component (CFTC) - representative of flight-critical structural attributes and failure modes - without a priori knowledge of the test result. CFTC advanced structural features include a composite skin made of unidirectional tape, a fabric hat stiffener, and a mechanically fastened aluminum rib. CFTC, developed by Boeing under the Air Force Research Laboratory (AFRL) Composite Airframe Life Extension (CALE) Program, Assessing the Durability and Damage Tolerance of Advanced Composite Structural Features, has been the most complex PDFA validation article to date.
Nikishkov, YuriyNikishkov, GennadiySeon, GuillaumeShonkwiler, BrianMakeev, Andrew
An Experimental Investigation of Squeak Noise for the Fabric and Plastic of Automotive Seat2019-01-14293/25/2019
Recently, one of major problems in automotive industry is squeak noise between two different materials. It is the most severe case that the noise between automobile seat and other relative parts (or within seat parts). Especially, seat covering is generated to unfavorable sound by friction of other parts. The purpose of this research is to verify and suggest a way to reduce squeak noise between seat covering and plastic at relative parts. Test results were reported with 1 to 10 Risk Priority Number (RPN) which was proposed by VDA (Verband der Automotilindustrie). It was conducted as a test with two different types of seat trim cover (knit) and plastics (PC+ABS) applied at arm rest in automotive interior. Through the principle test, the knit were more advantageous for squeak noise than other fabrics around relative part of seat particularly with suede, tricot and PC+ABS. We also optimized the concentration of soft agent in knit for slipping through stick-slip test to moderate noise. The concentration of soft agent is about 5% that squeak noise was below 3 for all case of plastic and seat covering. If the concentration of soft agent in knit is more or less than 5%, a fabric is excessively contracted or changed into different characteristics. Additionally, dense system of knit can decrease noise compare to loose organization. Based on these results, we developed an improved knit for squeak noise to apply of meeting parts at seat. This fabric can prevent the squeak noise even though abrasion and environmental conditions. The result of this study could be used to decrease in noise and be useful for selection of the materials at seat and relative parts.
Choi, HyerinSong, JunhoJeong, Kie Youn
Items per page:
1 – 50 of 879