Performance assessment of thermal protection coatings of hazardous material tankers in the presence of defects

2017 ◽  
Vol 105 ◽  
pp. 393-409 ◽  
Author(s):  
Giordano Emrys Scarponi ◽  
Gabriele Landucci ◽  
Alessandro Tugnoli ◽  
Valerio Cozzani ◽  
Albrecht Michael Birk
2018 ◽  
Vol 91 (1) ◽  
pp. 26-39
Author(s):  
O. M. Alifanov ◽  
S. A. Budnik ◽  
A. V. Morzhukhina ◽  
A. V. Nenarokomov ◽  
A. V. Netelev ◽  
...  

Author(s):  
V.V. Leonov ◽  
V.S. Zarubin ◽  
M.A. Ayrapetyan

In the case of full implementation of the programs of studying and developing the Moon, announced in recent years (“Luna”, Artemis, Chang’e), significant increase in cargo turnover between the Moon and the Earth is expected. Therefore the research and development of appropriate spacecrafts and their structural elements is believed to be promising, especially thermal protection coatings ensuring spacecraft safety during movement (descent) in the dense atmosphere layers. A special characteristic of the trajectory of the spacecraft returning from the Moon’s orbit is the closeness of the speed of its entry into the Earth’s atmosphere to the parabolic one. This circumstance significantly complicates solving the problem of creating thermal protection for such a vehicle, because of higher convective and radiative heat flows compared to those acting on orbital landers. The analysis showed that when implementing the trajectory of the return of spacecraft with multiple re-entries into the Earth’s atmosphere, a trajectory can be selected (at least for cargo flights) so that the intensity of heat exchange on the surface of the coating does not exceed the permissible level. In this case, use of modern and advanced anisotropic heat-protective composite materials can reduce the spacecraft surface temperature to a level that does not cause destruction of the thermal protection coating.


Author(s):  
Zheyong Bian ◽  
Nathalie Carchi ◽  
Xiang Liu

Abstract Railroad tank car transportation is the most efficient way to transport large amounts of hazardous material. More than 2 million tank-car loads of hazardous materials (hazmat) are transported annually by rail in the United States. Recently, the boom in the production of petroleum crude oil and natural gases from shale has dramatically increased the rail transport volume of flammable energy resources. However, accidents do occur, and the transportation of flammable hazardous material can result in disastrous consequences. The fire can heat up a tank car, rapidly increasing the inside pressure and causing the tank car to either rupture or explode. Railroad companies are developing or seeking advanced thermal protection systems to prevent tank car explosion or prolong the burst time to win a sufficient rescue time. It is of great importance to understand the existing thermal protection systems used in hazmat tank cars and to identify key priorities that the government and industry consider for improving tank car thermal protection performance, providing guidance for future thermal protection material development. Thus, this paper reviews the literature on the effects and analysis of different tank car thermal protection systems, identifying the effectiveness of different thermal protection components, properties of thermal protection materials, and testing methodologies. Different combinations of insulators and jackets are tested in order to observe the effects of the fire on the tank car. The tank car is tested while carrying hazardous material like liquefied petroleum gas, propane, and ethylene oxide, etc. This investigation analyzes the differences of thermal protection systems in prolonging the life span of a tank car engulfed in flames. A tank car can use either material like fiberglass, ceramic fiber blankets, perlite powder, or urethane foam to better insulate and thermally protect the tank car. An insulator is shown to prolong the life span of a tank car since bare tank cars tend to heat up rapidly when exposed to flames. The thermal protection system of a tank car is built of insulators, jackets, and supporting material for the insulator. The supporting material and jacket combination with the insulator also prevent the tank car from heating up rapidly. There are two primary testing methods, pool fire, and torch fire. Each type of fire has different outcomes and limits in which the tank car can withstand. When testing the heating of a tank car, thermocouples were placed throughout a tank car and recorded to check what areas were heated the most during the experiment. Some factors that had been accounted for in the previous studies were the wind speed and the direction of the wind, which affected the overall experiment, mostly torch fire experiments.


2021 ◽  
pp. 27-31
Author(s):  
Al’-Bdeyri M.Sh. ◽  
N.A. Dubrovina ◽  
S.V. Sergeev

The possibility for creating of high-hard protective wear-resistant and thermal protection coatings by the galvanic plasma method on the AlSi12Cu aluminum alloy in order to improve the operating characteristics of the pistons of internal combustion engine is shown. The effect of technological modes and electrolyte composition on the structure and composition of the resulting coating is established.


2020 ◽  
pp. 88-96
Author(s):  
Alexandr Maramygin ◽  

The material summed up in this article is recommended for engineers of aerospace industry, as well as can be of inter-est for the production personnel. The article covers the production of “scale-like” outer thermal protection coatings on the basis of syntactic materials with tumescent characteristics used in the production of special purpose equipment. The research per-formed sums up the results of the practical implementation of the technology adaptative method in the conditions of the real outer thermal protection coatings production. This work describes a typical technological process of “scale-like” outer thermal protection coating production from the panels based on syntactic material, including the stages of separate panels production with the help of shape-generating molding tools and forming of thermal protection coating by laying and molding-on of separate panels on the pressure restraint layer of the aircraft. The author proves the effectiveness of technology adaptative method us-age on the example of modification processes of pattern polymer composition being the basis of syntactic material. The re-search describes the solutions for the production cycle optimization via improvement of technological properties of the materials used. The work also contains the results of the researches, including spectral and thermochemical analyses of polymer compo-sitions modified by polyisocyanates, and describes the research techniques of their properties. Quasi-eutectic compositions of aliphatic and aromatic amines are received, which, being used as curative of reactive epoxiurethane polymers produced on the basis of epoxy-diane oligomers and polyisocyanates, enable to divide the polymerization process into two stages. The method described in the article provides the elimination of panel defects on the stage of molding-on due to implementation of mode separation in polymerization processes, which contributes towards the quality and reliability of thermal protection coating.


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