scholarly journals Development of sago drying with environmentally friendly techniques

2021 ◽  
Vol 886 (1) ◽  
pp. 012044
Author(s):  
Yulismayanti ◽  
Abdul Waris ◽  
Junaedi Muhidong

Abstract One of the drying machines that is commonly used by in industry is a rack-type dryer. However, the rack-type drying machine has generally fairly low efficiency. A rack-type dryer has been designed which was equipped with a hybrid mechanism, but is its performance not yet known when it is controlled by an expert control system. The purpose of this research was to produce an expert control system that can be applied to a rack-type dryer with a hybrid system mechanism which can improve the performance of the dryer. The research includes the development of expert rules applied to the control system and a series of tests was carried out using 10 kg of fresh sago starch. The test results show that the drying air temperature did not show any overshoot and short settling time, drying temperature is relatively stable and there was no steady state error. The drying rate of fresh sago starch can be increased by using the hybrid system. The use of electric power with the hybrid system was lower (5.78 kWh) compared to that of non-hybrid (6.88 kWh) or a reduction of about 16% compared to the non-hybrid system. Thermal efficiency of the rack-type dryer with the expert control system was about 36%.

1989 ◽  
Vol 19 (5) ◽  
pp. 1101-1105 ◽  
Author(s):  
M.S. Mahmoud ◽  
S.Z. Eid ◽  
A.A. Abou-Elsoud

2014 ◽  
Vol 940 ◽  
pp. 306-310
Author(s):  
Xiao Jin Wang ◽  
Xin Li ◽  
Xiao Ling Peng ◽  
Qi Feng Fang

Aiming at the abnormal landing of the aircraft which caused by the invalidation of the undercarriage, a safe auxiliary system for aircraft’s forced landing is proposed. Firstly, the article introduces the basic compositions and the main functions of each part in the system, and proposes the undercarriage robot based on the aircraft arresting system and also the underground rail system based on the steam-driven catapult principle is put forward. Secondly, the detail introductions on the system’s operating principles for aiding the forced landing of aircraft are given separately from starting, docking, decelerating and separation. At last, an expert control system based on knowledge base is proposed for realizing the calculation of docking position, velocity matching and the optimal decelerating scheme.


Sign in / Sign up

Export Citation Format

Share Document