Functionally Grade Composite Material Production

Author(s):  
Shubhajit Das ◽  
Sangeeta Das ◽  
Tage Nampi ◽  
Kakoli Roy
BioResources ◽  
2016 ◽  
Vol 11 (3) ◽  
Author(s):  
Nima Zarrinbakhsh ◽  
Tao Wang ◽  
Arturo Rodriguez-Uribe ◽  
Manjusri Misra ◽  
Amar K. Mohanty

2012 ◽  
Vol 501 ◽  
pp. 104-107
Author(s):  
Qian Wang ◽  
Peng Cheng Xie ◽  
Wei Min Yang ◽  
Yu Mei Ding

The new micro-nano lamination technology is developed to produce composite materials with alternating layers structure. After polymer melt enter into the unit passing the process of stream-reverse-superimposed, it produces functional composites with dozens or even thousands of alternating layers, it obtains barrier performance that general multi-layer co-extrusion can not compare with. Equipment cost is low and production process is simple in the barrier composite material production process.


2019 ◽  
Vol 11 ◽  
pp. 31-35 ◽  
Author(s):  
Sergey Gorbatyuk ◽  
Alexey Pashkov ◽  
Nikolay Chichenev

2019 ◽  
Vol 8 (1) ◽  
pp. 20180025 ◽  
Author(s):  
Ferdausee Rahman Anannya ◽  
Md. Arif Mahmud

Author(s):  
E. Sukedai ◽  
H. Mabuchi ◽  
H. Hashimoto ◽  
Y. Nakayama

In order to improve the mechanical properties of an intermetal1ic compound TiAl, a composite material of TiAl involving a second phase Ti2AIN was prepared by a new combustion reaction method. It is found that Ti2AIN (hexagonal structure) is a rod shape as shown in Fig.1 and its side surface is almost parallel to the basal plane, and this composite material has distinguished strength at elevated temperature and considerable toughness at room temperature comparing with TiAl single phase material. Since the property of the interface of composite materials has strong influences to their mechanical properties, the structure of the interface of intermetallic compound and nitride on the areas corresponding to 2, 3 and 4 as shown in Fig.1 was investigated using high resolution electron microscopy and image processing.


Author(s):  
O. Popoola ◽  
A.H. Heuer ◽  
P. Pirouz

The addition of fibres or particles (TiB2, SiC etc.) into TiAl intermetallic alloys could increase their toughness without compromising their good high temperature mechanical and chemical properties. This paper briefly discribes the microstructure developed by a TiAl/TiB2 composite material fabricated with the XD™ process and forged at 960°C.The specimens for transmission electron microscopy (TEM) were prepared in the usual way (i.e. diamond polishing and argon ion beam thinning) and examined on a JEOL 4000EX for microstucture and on a Philips 400T equipped with a SiLi detector for microanalyses.The matrix was predominantly γ (TiAl with L10 structure) and α2(TisAl with DO 19 structure) phases with various morphologies shown in figure 1.


2019 ◽  
pp. 9-13
Author(s):  
V.Ya. Mendeleyev ◽  
V.A. Petrov ◽  
A.V. Yashin ◽  
A.I. Vangonen ◽  
O.K. Taganov

Determining the surface temperature of materials with unknown emissivity is studied. A method for determining the surface temperature using a standard sample of average spectral normal emissivity in the wavelength range of 1,65–1,80 μm and an industrially produced Metis M322 pyrometer operating in the same wavelength range. The surface temperature of studied samples of the composite material and platinum was determined experimentally from the temperature of a standard sample located on the studied surfaces. The relative error in determining the surface temperature of the studied materials, introduced by the proposed method, was calculated taking into account the temperatures of the platinum and the composite material, determined from the temperature of the standard sample located on the studied surfaces, and from the temperature of the studied surfaces in the absence of the standard sample. The relative errors thus obtained did not exceed 1,7 % for the composite material and 0,5% for the platinum at surface temperatures of about 973 K. It was also found that: the inaccuracy of a priori data on the emissivity of the standard sample in the range (–0,01; 0,01) relative to the average emissivity increases the relative error in determining the temperature of the composite material by 0,68 %, and the installation of a standard sample on the studied materials leads to temperature changes on the periphery of the surface not exceeding 0,47 % for composite material and 0,05 % for platinum.


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