In situ catalytic reforming of plastic pyrolysis vapors using MSW incineration ashes

2021 ◽  
Vol 276 ◽  
pp. 116681
Author(s):  
Ashiq Ahamed ◽  
Lili Liang ◽  
Wei Ping Chan ◽  
Preston Choon Kiat Tan ◽  
Nicklaus Tze Xuan Yip ◽  
...  
Author(s):  
Alena Nikolaevna Seliverstova ◽  
Denis Valerievich Nemchinov ◽  
Elena Fedorovna Raykova

Fail-safety taken as a factor of completeness of using the resources of the production facility is important for characterizing the technological process. In most modern automated process control systems the above factor is implemented by means of the emergency protection system which allows to avoid the progressing emergency. However, such measures significantly increase the downtime of process equipment, since the possibility of developing pre-emergency and emergency situations when combining several permissible and close to emergency values of parameters is not taken into account. To solve the problem of reducing machinery downtime, a method for determining the object state indicator has been proposed. It takes into account all variants of the influence of technological parameters on each other as well as their combinations leading to the emergency progress. As well, the proposed solution helps to set the proximity of the operating mode of the production equipment to the threshold emergency, which greatly reduces the risk of emergency in situ, thereby reducing equipment downtime and economic losses. The method of determining the indicator of the state of the object is considered on the example of the stabilization block of hydrogenate catalytic reforming unit.


2021 ◽  
Vol 613 ◽  
pp. 118018 ◽  
Author(s):  
Xue-Yu Ren ◽  
Jing-Pei Cao ◽  
Shi-Xuan Zhao ◽  
Xiao-Yan Zhao ◽  
Xiao-Bo Feng ◽  
...  

Fuel ◽  
2007 ◽  
Vol 86 (12-13) ◽  
pp. 1983-1993 ◽  
Author(s):  
K. Karlfeldt ◽  
B.-M. Steenari

1984 ◽  
Vol 75 ◽  
pp. 743-759 ◽  
Author(s):  
Kerry T. Nock

ABSTRACTA mission to rendezvous with the rings of Saturn is studied with regard to science rationale and instrumentation and engineering feasibility and design. Future detailedin situexploration of the rings of Saturn will require spacecraft systems with enormous propulsive capability. NASA is currently studying the critical technologies for just such a system, called Nuclear Electric Propulsion (NEP). Electric propulsion is the only technology which can effectively provide the required total impulse for this demanding mission. Furthermore, the power source must be nuclear because the solar energy reaching Saturn is only 1% of that at the Earth. An important aspect of this mission is the ability of the low thrust propulsion system to continuously boost the spacecraft above the ring plane as it spirals in toward Saturn, thus enabling scientific measurements of ring particles from only a few kilometers.


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